ISBN: 978-1-61782-948-2

49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition 2011

Orlando, Florida, USA 4-7 January 2011

Volume 1 of 20

The contents of this work are copyrighted and additional reproduction in whole or in part are expressly prohibited without the prior written permission of the Publisher or copyright holder. The resale of the entire proceeding as received from CURRAN is permitted. For reprint permission, please contact AIAA’s Business Manager, Technical Papers. Contact by phone at 703-264-7500; fax at 703-264-7551 or by mail at 1801 Alexander Bell Drive, Reston, VA 20191, USA.

Printed from e-media with permission by:

Curran Associates, Inc. 57 Morehouse Lane

Red Hook, NY 12571

Some format issues inherent in the e-media version may also appear in this print version.

TABLE OF CONTENTS

VOLUME 1

DRYDEN LECTURE: FUEL OPTIONS FOR NEXT GENERATION CHEMICAL PROPULSION................................................... 1C. Law

MULTI-VARIATE DESIGNED EXPERIMENTS FOR DEVELOPMENT OF A WING WEIGHT SURROGATE MODEL ............................................................................................................................................................................................................. 31

John Doty

TECHNOLOGY ASSESSMENT OF NASA ENVIRONMENTALLY RESPONSIBLE AVIATION ADVANCED VEHICLE CONCEPTS................................................................................................................................................................................... 40

J. Schutte, H. Jimenez, D. Mavris

IMPACT OF DESIGNED EXPERIMENTS ON EFFICIENCY, ACCURACY, AND HYPOTHETICAL TEST COSTS USING A LIGHT AIRCRAFT WING MODEL ............................................................................................................................ 51

S. Szaruga, J. Doty

DEVELOPING THE AERODYNAMICS MODULE FOR THE INTEGRATED MULTIDISCIPLINARY OPTIMIZATION OBJECT SYSTEM .......................................................................................................................................................... 62

Steven Doyle, Katherine Alston, Tyler Winter

AERODYNAMIC OPTIMIZATION ON THE CONCEPTUAL DESIGN STAGE ............................................................................... 80Doe Young Hur, Min-Ho Kwak, Su-Hwan Yoon, Dongho Lee

AERODYNAMIC CHARACTERIZATION OF A MODERN LAUNCH VEHICLE ............................................................................ 90Robert Hall, Scott Holland, John Blevins

GENERATION OF THE ARES I-X FLIGHT TEST VEHICLE AERODYNAMIC DATA BOOK AND COMPARISON TO FLIGHT .......................................................................................................................................................................104

Steven Bauer, Steven Krist, William Compton

AERODYNAMIC ANALYSES AND DATABASE DEVELOPMENT FOR LIFT-OFF/TRANSITION AND FIRST STAGE ASCENT OF THE ARES I A106 VEHICLE ..................................................................................................................127

B. Pamadi, J. Pei, P. Covell, N. Favaregh, C. Gumbert, J. Hanke

OVERVIEW OF EXPERIMENTAL INVESTIGATIONS FOR ARES I LAUNCH VEHICLE DEVELOPMENT ........................149W. Tomek, G. Erickson, J. Pinier, J. Hanke

AERODYNAMIC CHARACTERIZATION AND SIMULATION OF A SOLID ROCKET BOOSTER DURING REENTRY FLIGHT ......................................................................................................................................................................................165

D. Purinton, J. Blevins, V. Pritchett, D. Haynes, M. Carpenter

OVERVIEW OF ARES-I CFD ASCENT AERODYNAMIC DATA DEVELOPMENT AND ANALYSIS BASED ON USM3D .....................................................................................................................................................................................................181

K. Abdol-Hamid, F. Ghaffari, E. Parlette

BEST PRACTICES FOR AERO-DATABASE CFD SIMULATIONS OF ARES V ASCENT ...........................................................219C. Kiris, J. Housman, M. Gusman, D. Schauerhamer, K. Deere, A. Elmiligui, K. Abdol-Hamid, E. Parlette, M. Andrews, J. Blevins

VALIDATING LES FOR JET AEROACOUSTICS .................................................................................................................................240J. Bridges

ON SOME ISSUES IN LARGE-EDDY SIMULATIONS FOR CHEVRON NOZZLE JET FLOWS (INVITED PAPER)............................................................................................................................................................................................................250

Ali Uzun, M. Yousuff Hussaini

MECHANISMS OF JET NOISE REDUCTION AND THEIR IMPACT ON LARGE-EDDY SIMULATIONS (INVITED) ......................................................................................................................................................................................................276

D. Bodony, J. Kim, J. Freund

HYBRID RANS-LES MODELLING OF CHEVRON NOZZLES WITH PREDICTION OF FAR FIELD SOUND.......................285H. Xia, S. Karabasov, P. Tucker, A. Dowling, T. Hynes, O. Graham, K. Depuru

HIGH SPEED AND HIGH REYNOLDS NUMBER JET CONTROL USING ARC FILAMENT PLASMA ACTUATORS FOR NOISE MITIGATION AND FOR FLOW AND NOISE DIAGNOSTICS..........................................................301

M. Samimy, M. Kearney-Fisher, J. Kim, A. Sinha

SIMULATION-BASED ANALYSIS OF THE NEAR FIELD IN A SUPERSONIC JET CONTROLLED BY PLASMA ACTUATORS ...............................................................................................................................................................................320

D. Gaitonde

UNSTEADY ADJOINT METHOD FOR THE OPTIMAL CONTROL OF ADVECTION AND BURGER'S EQUATIONS USING HIGH-ORDER SPECTRAL DIFFERENCE METHOD ...................................................................................339

Kui Ou, Antony Jameson

REYNOLDS-AVERAGED NAVIER-STOKES SIMULATION OF A 2-D CIRCULATION CONTROL WIND TUNNEL EXPERIMENT .............................................................................................................................................................................357

Brian Allan, Gregory Jones, John Lin

A NONLINEAR SENSITIVITY SOLVER FOR AERODYNAMIC SHAPE OPTIMIZATION AND RAPID DESIGN SPACE EXPLORATION..............................................................................................................................................................373

Travis Drayna, Graham Candler, Heath Johnson

SUPERCRITICAL WING DESIGN AND OPTIMIZATION FOR TRANSONIC CIVIL AIRPLANE ............................................387Y. Zhang, H. Chen, M. Zhang, M. Zhang, T. Liu, W. Zhang, S. Fu

SIMULATION OF SEPARATION OF STORES PARTIALLY FILLED WITH FLUIDS .................................................................396Rainald Lohner

EVALUATION OF FLOW SOLVER ACCURACY USING FIVE SIMPLE UNSTEADY VALIDATION CASES........................413Bradford Green, Ryan Czerwiec, Christopher Cureton, Chad Lillian, Sergey Kernazhitskiy, Tim Eymann, Jason Torres, Keith Bergeron, Robert Decker

GOAL ORIENTED MESH ADAPTATION USING TOTAL DERIVATIVE OF AERODYNAMIC FUNCTIONS WITH RESPECT TO MESH COORDINATES ........................................................................................................................................443

Jacques Peter, Pierre Trontin, Maxime Nguyen-Dinh

REVIEW OF MICRO VORTEX GENERATORS IN HIGH-SPEED FLOW .......................................................................................468Frank Lu, Qin Li, Yusi Shih, Adam Pierce, Chaoqun Liu

INTERACTION OF MICROVORTEX GENERATOR FLOW WITH RAMP-INDUCED SHOCK/BOUNDARY-LAYER INTERACTIONS ............................................................................................................................................................................484

A. Pierce, Q. Li, Y. Shih, F. Lu, C. Liu

INSTABILITY PROCESS IN SYNTHETIC JETS ...................................................................................................................................494L. Oren, J. Cha, E. Gutmark, S. Khosla

ROTORCRAFT FUSELAGE DRAG REDUCTION USING COMBUSTION POWERED ACTUATORS .....................................507G. Woo, A. Glezer, J. Bain, T. Crittenden, L. Sankar

DISTORTION MANAGEMENT IN A BLI INLET DIFFUSER USING SYNTHETIC-JET HYBRID FLOW CONTROL ......................................................................................................................................................................................................520

A. Gissen, B. Vukasinovic, M. McMillan, A. Glezer

CONTROL OF SELF-EXCITED ROLL OSCILLATIONS OF LOW-ASPECT-RATIO WINGS USING ACOUSTIC EXCITATION ..........................................................................................................................................................................534

Tianxiang Hu, Zhijin Wang, Ismet Gursul

CONTROL OF FLOW OVER A RECTANGULAR CAVITY USING A ROD IN CROSS FLOW: FURTHER EVALUATION OF KEY MECHANISMS .................................................................................................................................................549

K. Chaudhari, G. Raman

KOOPMAN SPECTRAL ANALYSIS OF SEPARATED FLOW OVER AFINITE-THICKNESS FLAT PLATE WITH ELLIPTICAL LEADING EDGE.....................................................................................................................................................562

J. Tu, C. Rowley, E. Aram, R. Mittal

FLOW FIELD EFFECTS OF CONTROL ON SUPERSONIC OPEN CAVITIES...............................................................................576Taylor Lusk, Jonathan Dudley, Lawrence Ukeiley, Louis Cattafesta

TRANSITION TO SELF-EXCITED OSCILLATIONS IN LOW DENSITY TRANSVERSE JET SHEAR LAYERS ..........................................................................................................................................................................................................592

Daniel Getsinger, Cory Hendrickson, Ann Karagozian

EFFECTS OF OBLIQUE UNSTABLE MODES ON THE DEVELOPMENT OF A TURBULENT MIXING LAYER AT HIGH CONVECTIVE MACH NUMBERS ..........................................................................................................................609

Daisuke Watanabe, Kensuke Akita, Hiroshi Maekawa

HIGH-SPEED SCHLIEREN IMAGING THROUGH A TWO-DIMENSIONAL WEAKLY-COMPRESSIBLE SHEAR LAYER .............................................................................................................................................................................................621

Z. Ponder, E. Jumper

INVESTIGATION OF THE THREE DIMENSIONAL FLOW STRUCTURESIN A PLANAR OFFSET ATTACHING JET .........................................................................................................................................................................................640

N. Gao, D. Ewing

HIGH-ORDER METHODS INCLUDING DISCONTINUOUS GALERKIN BY RECONSTRUCTIONS ON TRIANGULAR MESHES .............................................................................................................................................................................655

H. Huynh

EFFICIENT SOLUTION TECHNIQUES FOR HIGH-ORDER METHODS ON 3-D ANISOTROPIC HYBRID MESHES..........................................................................................................................................................................................................683

T. Haga, H. Gao, Z. Wang

HIGH-ORDER METHODS FOR DIFFUSION EQUATION WITH ENERGY STABLE FLUX RECONSTRUCTION SCHEME .................................................................................................................................................................701

K. Ou, P. Vincent, A. Jameson

A STABLE SPECTRAL DIFFERENCE METHOD FOR TRIANGLES ...............................................................................................720A. Balan, G. May, J. Schöberl

AN ARTIFICIAL COMPRESSIBILITY METHOD FOR THE SPECTRAL DIFFERENCE SOLUTION OF UNSTEADY INCOMPRESSIBLE NAVIER-STOKES EQUATIONS ON MULTIPLE GRIDS .......................................................741

C. Liang, A. Chan, X. Liu, A. Jameson

A HIGH RESOLUTION SPECTRAL METHOD FOR THE COMPRESSIBLE NAVIER-STOKES EQUATIONS......................754Caleb Barnes, George Huang, Joseph Shang

SOLVING TIME DEPENDENT DIFFUSION EQUATIONS ON ARBITRARY GRIDS USING A HIGH-ORDER SPACE-TIME DISCONTINUOUS GALERKIN CELL VERTEX SCHEME.......................................................................................767

S. Tu, G. Skelton, Q. Pang

ON PARALLEL PERFORMANCE OF A DISCONTINUOUS GALERKIN COMPRESSIBLE FLOW SOLVER BASED ON DIFFERENT NUMERICAL FLUXES ..................................................................................................................................781

A. Ali, H. Luo, A. Hassan, K. Syed, M. Ishaq

THREE DIMENSIONAL EFFECTS ON THE FREQUENCY RESPONSE CURVE FOR THE INLINE VIBRATING CYLINDER.............................................................................................................................................................................797

A. Mehmood, I. Akhtar, M. Ghommem, M. Hajj, A. Nayfeh

UNSTEADY FLOW PREDICTIONS AROUND TANDEM CYLINDERS WITH SUB-CRITICAL SPACING .............................812R. Satti, Y. Li, R. Shock, S. Noelting

HIGH ANGLE OF ATTACK HELICOPTER BLADE-VORTEX INTERACTION;NUMERICAL STUDIES USING LES .....................................................................................................................................................................................................823

M. Ilie, P. Coronado, C. Velez, G. Zha

MODIFICATION TO THE K-ω TURBULENCE MODEL FOR VORTICALLY DOMINATED FLOWS ....................................832Lawrence Dechant

NUMERICAL INVESTIGATIONS OF VORTEX-CYLINDER MECHANISM OF INTERACTION USING LES AND URANS...................................................................................................................................................................................................851

P. Coronado, M. Ilie, G. Zha

REDUCED ORDER MODELING OF A TURBULENT TWO DIMENSIONAL CYLINDER WAKE WITH FILTERED POD AND ARTIFICIAL NEURAL NETWORKS ..............................................................................................................863

Akin Paksoy, Buryan Apacoglu, Selin Aradag

ATTENUATION OF GAS TURBINE COMBUSTOR PRESSURE OSCILLATIONS USING SYMMETRY BREAKING ....................................................................................................................................................................................................877

J. Cohen, G. Hagen, A. Banaszuk, S. Becz, P. Mehta

IMPROVEMENT OF THE GAS TURBINE PLASMA ASSISTED COMBUSTOR CHARACTERISTICS ...................................886S. Serbin, A. Mostipanenko, I. Matveev, A. Topina

EFFECT OF SWIRL NUMBER AND FUEL TYPE UPON THE FLASHBACK IN SWIRL COMBUSTORS ...............................892M. Abdulsada, N. Syred, A. Griffiths, P. Bowen

VOLUME 2

THE ROLE OF LOCAL BASE CAVITIES IN AN AUGMENTOR BLUFFBODY FLAMEHOLDER............................................908

W. Kim, G. Mungal

DISTRIBUTED COMBUSTION WITH SWIRL FOR GAS TURBINE APPLICATION ...................................................................931A. Khalil, V. Arghode, A. Gupta

LES INVESTIGATION AND SENSITIVITY ANALYSIS OF THE FLOW DYNAMICS IN A GAS TURBINE SWIRL COMBUSTOR .................................................................................................................................................................................941

P. Iudiciani, C. Duwig, S. Hosseini, R. Szasz, L. Fuchs, E. Gutmark

IMPROVED CORRELATION FOR BLOWOUT OF BLUFF BODY STABILIZED FLAMES .......................................................958B. Huelskamp, B. Kiel, A. Lynch, S. Kostka, P. Gokulakrishnan, M. Klassen

UNSTART OF A SUPERSONIC MODEL INLET/ISOLATOR FLOW INDUCED BY MASS INJECTION..................................981Hyungrok Do, Seong-Kyun Im, Mark Mungal, Mark Cappelli

AN EXPERIMENTAL INVESTIGATION OF CORNER BLEED APPLIED TO A NORMAL SHOCK-WAVE/BOUNDARY-LAYER INTERACTION AND DIFFUSER .........................................................................................................992

Neil Titchener, Paul Bruce, Holger Babinsky

CHARACTERIZATION OF MICRO-VORTEX GENERATORS IN SUPERSONIC FLOWS .......................................................1000W. Nolan, H. Babinsky

NUMERICAL AND EXPERIMENTAL STUDIES ON THE SEPARATIONTOPOLOGY OF THE MVG CONTROLLED FLOW AT M=2.5............................................................................................................................................................1017

Q. Li, Y. Yan, P. Lu, A. Pierce, C. Liu, F. Lu

CHARACTERIZATION OF SUPERSONIC COMBUSTER INLET FLOWS USING DIODE LASER ABSORPTION SPECTROSCOPY ............................................................................................................................................................1033

Sven Wittig, Sean O'Byrne

APPLICATION OF COMPOUND COMPRESSIBLE FLOW TO A BOUNDARY LAYER IN A HYPERSONIC THREE-DIMENSIONAL INLET ..............................................................................................................................................................1044

G. Bussey, M. Lewis

NONLINEAR GUIDANCE AND CONSENSUS FOR UNMANNED VEHICLES WITH TIME VARYING CONNECTION TOPOLOGIES.................................................................................................................................................................1055

M. Ahmed, K. Subbarao

ANALYSIS OF TIME OPTIMAL 3D PATHS FOR AN AUTONOMOUS AIRCRAFT WITH A PIECEWISE CONSTANT ACCELERATION ................................................................................................................................................................1067

Y. Bestaoui, E. Kahale

COOPERATIVE CONTROL OF SWARMS OF UNMANNED AERIAL VEHICLES .....................................................................1081E. De Vries, K. Subbarao

ROUTE FINDING FOR AN AUTONOMOUS AIRCRAFT ..................................................................................................................1104S. Dicheva, Y. Bestaoui

ATTRACTIVE MANIFOLD-BASED NONCERTAINTY-EQUIVALENT ADAPTIVE CONTROL OF AIRCRAFT ...................................................................................................................................................................................................1117

K. Lee, S. Singh

BRIDGE MONITORING BY A LIGHTER THAN AIR ROBOT.........................................................................................................1134Yasmina Bestaoui

AN EXPERIMENTAL AND COMPUTATIONAL INVESTIGATION OF N-DODECANE IGNITION AND CHEMICAL KINETICS .............................................................................................................................................................................1150

D. Karwat, M. Wooldridge, C. Westbrook, S. Wagnon, J. Lai

IGNITION DELAY STUDY OF MOIST SYNGAS/OXIDIZER AND HYDROGEN/OXIDIZER MIXTURES USING A RAPID COMPRESSION MACHINE ......................................................................................................................................1166

A. Das, C. Sung

AUTOIGNITION OF BINARY FUEL BLENDS OF N-BUTANOL AND N-HEPTANE IN A RAPID COMPRESSION MACHINE .....................................................................................................................................................................1175

Yu Zhang, Kamal Kumar, Chih-Jen Sung

KINETIC MODELING OF THE H2/O2 REACTION IN HIGH-PRESSURE FLAMES ...................................................................1183Michael Burke, Yiguang Ju, Frederick Dryer, Marcos Chaos, Stephen Klippenstein

KINETIC MECHANISM FOR LOW PRESSURE OXYGEN / METHANEIGNITION AND COMBUSTION ............................1192N. Slavinskaya, O. Haidn

HOT COMBUSTION TORCH JET IGNITION DELAY TIME FOR ETHYLENE-AIR MIXTURES ..........................................1205I. Perera, S. Wijeyakulasuriya, R. Nalim

INVESTIGATION OF THE EFFECT OF NITRIC OXIDE ON THE AUTOIGNITION OF JP-8 AT LOW PRESSURE VITIATED CONDITIONS ...................................................................................................................................................1216

C. Fuller, P. Gokulakrishnan, M. Klassen, R. Roby, B. Kiel

ATOMIZATION PATTERNS AND BREAKUP CHARACTERISTICS OF LIQUID SHEETS FORMED BY TWO IMPINGING JETS............................................................................................................................................................................1230

D. Ma, X. Chen, P. Khare, V. Yang

EFFECT OF BACKPRESSURE ON INTERNAL FLOW DYNAMICS AND SPRAY CHARACTERISTICS OF LIQUID SWIRL INJECTOR .....................................................................................................................................................................1244

X. Chen, Y. Liu, V. Yang

HIGH-FIDELITY SIMULATION OF ATOMIZATION AND EVAPORATION IN A LIQUID JET IN CROSS-FLOW ............................................................................................................................................................................................................1261

X. Li, M. Soteriou, M. Arienti, M. Sussman

INFLUENCE OF COMPUTATIONAL DROP REPRESENTATION IN LESOF A DROPLET-LADEN MIXING LAYER ..........................................................................................................................................................................................................1280

Senthilkumaran Radhakrishnan, Josette Bellan

STEADY AND UNSTEADY RANS SIMULATIONS OF CRYOGENIC ROCKET COMBUSTORS ............................................1296M. Lempke, P. Gerlinger, M. Aigner, M. Rachner

IGNITION AND FLAME PROPAGATION ALONG PLANAR MONODISPERSE DROPLET STREAMS................................1309Jan Boyde, Patrick Le Clercq, Massimiliano Di Domenico, Thomas Mosbach, Gregor Gebel, Michael Rachner, Manfred Aigner

SWIRLING FLOWS AND LATERAL JET INJECTION FOR IMPROVED MIXING AND COMBUSTION .............................1324D. Lilley

40 YEARS WITH SWIRL, VORTEX, CYCLONIC FLOWS, AND COMBUSTION ........................................................................1340Nicholas Syred

ENGINEERING ASPECTS OF COMPLEX GAS TURBINE COMBUSTION MIXERS PART II: HIGH T3 ..............................1362Hukam Mongia

ENGINEERING ASPECTS OF COMPLEX GAS TURBINE COMBUSTION MIXERS PART I: HIGH ΔT...............................1372Hukam Mongia

ROLE OF SWIRL IN FLAME STABILIZATION .................................................................................................................................1388J. Driscoll, J. Temme

FDF SIMULATION OF SWIRLING REACTING FLOWS ON UNSTRUCTURED MESHES ......................................................1399N. Ansari, G. Goldin, P. Pisciuneri, M. Nik, P. Strakey, P. Givi

APPLICATION OF THE SLOW INVARIANT MANIFOLD CORRECTION FOR DIFFUSION .................................................1416Joshua Mengers, Joseph Powers

INTERMITTENCY AND PREMIXED TURBULENT REACTING FLOWS ....................................................................................1431Peter Hamlington, Alexei Poludnenko, Elaine Oran

SOOT MODELING IN A TURBULENT UNCONFINED C2H4/AIR JET FLAME..........................................................................1444Thomas Blacha, Massimiliano Di Domenico, Markus Köhler, Peter Gerlinger, Manfred Aigner

MODELING THE PROPAGATION OF PREMIXED FLAMES IN THE CONTEXT OF HYDRODYNAMIC THEORY .......................................................................................................................................................................................................1454

F. Creta, M. Matalon

MULTI-SCALE MODELING OF COAL GASIFICATION PROCESSES IN A WELL-STIRRED REACTOR WITH DETAILED CHEMISTRY .............................................................................................................................................................1464

L. Qiao, J. Xu, J. Gore

A SIMPLE MODEL OF MULTIPLE SPRAY FLAMES AND THEIR INTERACTION .................................................................1478Liron Hamelnick, Jerrold Greenberg

SPARK IGNITION AND EXPANSION OF A TURBULENTNON-PREMIXED BLUFF-BODY METHANE FLAME USING LARGEEDDY SIMULATIONS ...................................................................................................................................1493

Antonios Triantafyllidis, Epaminondas Mastorakos

THE IN-SITU RESOURCE UTILIZATION PROJECT UNDER THE NEW EXPLORATION ENTERPRISE ..........................1503W. Larson, G. Sanders

COMPARISON OF LUNAR AND MARS IN-SITU RESOURCE UTILIZATION FOR FUTURE ROBOTIC AND HUMAN MISSIONS ..........................................................................................................................................................................1510

G. Sanders

MANAGEMENT PROCESSES AND PROCEDURES FOR A SUCCESSFUL ANALOGUE DEPLOYMENT............................1525S. Schmidt, D. Boucher, M. McTaggart

DESIGN AND TESTING A SEPARABLE TANDEM ARTICULATING ROVER............................................................................1536P. Visscher, C. Bell, B. Jones

DEVELOPING PLANETARY ROVER TRACTION SYSTEMS .........................................................................................................1557P. Visscher, B. Jones, P. Radziszewski

PERFORMANCE EVALUATION OF THE RESOLVE EBRC MODULE IN FIELD TESTS 2005-2010 .....................................1579M. Viel, D. Boucher, J. Atwell, D. Roberts

EXCAVATION SYSTEM FOR LUNAR RESOURCE MANAGEMENT BASED ON SCREW CONVEYING AUGER TECHNOLOGY ...........................................................................................................................................................................1600

M. Radulescu, B. Landon, K. Moditis, T. Friedlaender, P. Radziszewski

SAVING ENERGY IN HOSPITALS WITH CCHP ................................................................................................................................1625Satoru Okamoto

EFFICIENCY OPTIMIZATION OF A STANDING-WAVE THERMOACOUSTIC HEAT ENGINE ..........................................1635Mazen Eldeeb, Mahmoud Fouad, Essam Khalil

GEOMETRICAL OPTIMIZATION OF THERMOACOUSTIC HEAT ENGINES ..........................................................................1646Abdelmaged Ibrahim, Nadim Arafa, Essam Khalil

HORIZONTAL AXIS TIDAL STREAM TURBINE ANALYSIS USING NUMERICAL SIMULATION .....................................1653J. Lee, D. Kim, S. Rhee

INVESTIGATION OF GAS-SOLID FLUIDIZED BED DYNAMICS WITH SPHERICAL AND NON-SPHERICAL PARTICLES.........................................................................................................................................................................1665

M. Rahman, M. Ruvalcaba, N. Love, A. Choudhuri

COUPLING STRATEGIES FOR HIGH-SPEED AEROHEATING PROBLEMS ............................................................................1673M. Howard, S. Bova

ARCJET TESTINGS OF SILICA AEROGEL TOWARD MARS AEROFLYBYSAMPLE COLLECTION MISSION .......................................................................................................................................................................................................1690

Toshiyuki Suzuki, Takashi Ozawa, Makoto Tabata, Kazuhisa Fujita, Hideyuki Kawai, Kyoko Okudaira

A STREAMLINE-UPWIND PETROV-GALERKIN FINITE ELEMENT SCHEME FOR NON-IONIZED HYPERSONIC FLOWS IN THERMOCHEMICAL NONEQUILIBRIUM ........................................................................................1701

Benjamin Kirk, Steven Bova, Ryan Bond

CONTRIBUTION OF CO2 IR RADIATION TO MARTIAN ENTRIES RADIATIVE WALL FLUXES ......................................1726Mario Lino Da Silva, James Beck

EVALUATION OF HYPERVELOCITY CARBON DIOXIDE BLUNT BODY EXPERIMENTS IN AN EXPANSION TUBE FACILITY ................................................................................................................................................................1742

Manu Sharma, Andy Swantek, William Flaherty, Joanna Austin, Sriram Doraiswamy, Graham Candler

MODELING OF THE CRACK GROWTH IN THE AVCOAT HEAT SHIELD ...............................................................................1768E. Titov, R. Kumar, D. Levin, B. Anderson

INTERACTIONS OF SINGLE-NOZZLE SUPERSONIC PROPULSIVE DECELERATION JETS ON MARS ENTRY AEROSHELLS ..............................................................................................................................................................................1787

Hicham Alkandry, Iain Boyd, Erin Reed, Joshua Codoni, James McDaniel

A CHALLENGE OF MODELING THERMO-MECHANICAL RESPONSE OF SILICA-PHENOLIC COMPOSITES UNDER HIGH HEATING RATES................................................................................................................................1800

Y. Matsuura, K. Hirai, T. Kamita, Y. Sato, T. Takatoya, H. Igawa

VOLUME 3

OPTICAL TRACKING AND SPECTROSCOPIC MEASUREMENT OF HAYABUSA CAPSULE REENTRY FIREBALL....................................................................................................................................................................................................1819

K. Fujita, H. Takayanagi, T. Suzuki, T. Yanagisawa, H. Kurosaki, M. Yamamoto, Y. Ishihara, S. Abe

IMPROVED PREDICTIONS OF PICA RECESSION IN ARC JET SHEAR TESTS .......................................................................1831D. Driver, M. Maclean

ELECTRONIC EXCITATION MODELING FOR INDUCTIVELY COUPLED PLASMA FLOWS.............................................1847T. Ozawa, T. Suzuki, H. Osawa, H. Takayanagi, K. Fujita

CFD IMPLEMENTATION OF A NOVEL CARBON-PHENOLIC-IN-AIR CHEMISTRY MODEL FOR ATMOSPHERIC RE-ENTRY ....................................................................................................................................................................1865

Alexandre Martin, Iain Boyd

DEVELOPMENT AND VERIFICATION OF THE CHARRING ABLATING THERMAL PROTECTION IMPLICIT SYSTEM SOLVER ..................................................................................................................................................................1883

A. Amar, N. Calvert, B. Kirk

PYROLYSIS GAS FLOW IN THERMALLY ABLATING MEDIA USING TIME-IMPLICIT DISCONTINUOUS GALERKIN METHODS.............................................................................................................................................................................1919

A. Bhatia, S. Roy, R. Gosse

DEVELOPMENT AND VALIDATION OF GENERALIZED LIFTING LINE BASED CODE FOR WIND TURBINE AERODYNAMICS ...................................................................................................................................................................1934

Francesco Grasso, Arne Van Garrel, Gerard Schepers

THE DEVELOPMENT OF CACTUS, A WIND AND MARINE TURBINE PERFORMANCE SIMULATION CODE.............................................................................................................................................................................................................1952

Jonathan Murray, Matthew Barone

A SUPERPOSITION THEORY FOR EFFICIENT COMPUTATION OF APPROXIMATE LIFT DISTRIBUTIONS ON HAWT ROTOR BLADES ..................................................................................................................................1973

Aditya Balu, Ashok Gopalarathnam, Fuh-Gwo Yuan

VALIDATION OF POTENTIAL FLOW AERODYNAMICS FOR HORIZONTAL-AXIS WIND TURBINES IN STEADY CONDITIONS USING THE MEXICO PROJECT EXPERIMENTAL DATA .................................................................1982

S. Cline, M. McWilliam, S. Lawton, C. Crawford

AN INVESTIGATION OF WT_PERF CONVERGENCE ISSUES ......................................................................................................1993D. Maniaci

VALIDATION OF THE BEDDOES-LEISHMAN DYNAMIC STALL MODEL FOR HORIZONTAL AXIS WIND TURBINES USING MEXICO DATA ...........................................................................................................................................2006

R. Santos Pereira, G. Schepers, M. Pavel

INBOARD STALL AND SEPARATION MITIGATION TECHNIQUES ON WIND TURBINE ROTORS ..................................2018Raymond Chow, C. Van Dam

COUPLED CFD/MULTIBODY ANALYSIS OF NREL UNSTEADY AERODYNAMIC EXPERIMENT PHASE VI ROTOR ....................................................................................................................................................................................................2029

Pierangelo Masarati, Jayanarayanan Sitaraman

INVESTIGATION OF VORTEX STRUCTURE NEAR THE SURFACE OF DBD-ACTUATOR ..................................................2044V. Golub, E. Son, A. Saveliev, V. Sechenov, D. Tereshonok

LIGHT EMISSION, DISCHARGE CAPACITANCE AND THRUST PRODUCTION OF DBD PLASMA ACTUATORS ...............................................................................................................................................................................................2055

Jochen Kriegseis, Benjamin Möller, Sven Grundmann, Cameron Tropea

DBD SURFACE CHARGE MEASUREMENTS AND MITIGATION IN MOVING AIR ................................................................2064Sohail Zaidi, Matthew Edwards, Dmitry Opatis, Richard Miles

PHENOMENOLOGICAL MODEL OF THE BODY FORCE INDUCED BY SURFACE DIELECTRIC BARRIER DISCHARGE ............................................................................................................................................................................2076

V. Soloviev, V. Krivtsov

MODELING OF AERODYNAMIC FORCING INDUCED BY SURFACE DIELECTRIC BARRIER DISCHARGE ................................................................................................................................................................................................2090

A. Fedorov, V. Krivtsov, V. Soloviev, V. Soudakov

A MORE EFFICIENT CONCEPTUAL DESIGN PROCESS USING THE RAGE GEOMETRY MODELER.............................2103Dejapong Suwarantana, David Rodriguez

COUPLING PARAMETRIC AIRCRAFT LOFTING TO CFD & CSM GRID GENERATION FOR CONCEPTUAL DESIGN............................................................................................................................................................................2113

A. Rizzi, J. Oppelstrup, M. Zhang, M. Tomac

CONCEPTUAL DESIGN MODELING IN THE RDS-PROFESSIONAL AIRCRAFT DESIGN SOFTWARE ............................2131Dan Raymer

GEOMETRY DESIGN ASSISTANT FOR AIRPLANE PRELIMINARY DESIGN ..........................................................................2142Willem Anemaat, Balaji Kaushik

WING SECTION THICKNESS AND CAMBER ALLOCATION FOR CONCEPTUAL AND PRELIMINARY AIRCRAFT DESIGN...................................................................................................................................................................................2160

Arvin Shajanian, Timothy Takahashi, Brian German, Matthew Daskilewicz, Shane Donovan

CONCEPTUAL DESIGN METHOD FOR SOLAR POWERED AIRCRAFTS .................................................................................2185Mehdi Hajian Maleki

ANALYSIS OF EMPTY WEIGHT OF GENERAL AVIATION PISTON ENGINE AIRCRAFT ...................................................2195K. Ibrahim

NUMERICAL ANALYSIS OF DYNAMICALLY LOADED ADVANCED STIFFENED AEROSPACE COMPOSITE STRUCTURES WITH BONDED/FASTENED JOINTS...............................................................................................2207

S. Binnamangala, J. Bayandor

AERODYNAMIC PERFORMANCE STUDY OF A MODERN BLENDED-WING-BODY AIRCRAFT UNDER SEVERE WEATHER SITUATIONS ........................................................................................................................................................2218

W. Tung, B. Song

ARES I AND ARES I-X STAGE SEPARATION AERODYNAMIC TESTING .................................................................................2228Jeremy Pinier, Charles Niskey

VALIDATION OF OVERFLOW FOR COMPUTING PLUME EFFECTS DURING THE AREAS I STAGE SEPARATION PROCESS ..........................................................................................................................................................................2245

G. Klopfer, J. Kless, H. Lee, J. Onufer, S. Pandya, W. Chan

AERODYNAMIC ANALYSES AND DATABASE DEVELOPMENT FOR ARES I VEHICLE FIRST STAGE SEPARATION ..............................................................................................................................................................................................2268

Bandu Pamadi, Jing Pei, Jeremy Pinier, Goetz Klopfer, Scott Holland, Peter Covell

COMPUTATIONAL ANALYSIS OF ARES I ROLL CONTROL SYSTEM JET INTERACTIONS ON ROLLING MOMENT .................................................................................................................................................................................2285

Karen Deere, S. Paul Pao, Khaled Abdol-Hamid

THE CRUCIAL ROLE OF ERROR CORRELATION FOR UNCERTAINTY MODELING OF CFD-BASED AERODYNAMICS INCREMENTS ..........................................................................................................................................................2309

Michael Hemsch, Eric Walker

AN ASSESSMENT OF ARES I-X AEROACOUSTIC MEASUREMENTS WITH COMPARISONS TO PRE-FLIGHT WIND TUNNEL TEST RESULTS............................................................................................................................................2322

D. Reed, M. Mayle, D. Nance

COMBUSTION RATES AND TEMPERATURES OF REACTIVE MATERIALS PARTICLES ...................................................2336C. Badiola, S. Zhang, R. Gill, E. Dreizin

TERNARY REACTIVE NANOCOMPOSITE POWDERS ...................................................................................................................2345Y. Aly, D. Stamatis, C. Badiola, E. Dreizin

THERMAL INITIATION OF CONSOLIDATED NANOCOMPOSITE THERMITE POWDERS ................................................2355Demitrios Stamatis, Edward Dreizin

AN APPROXIMATE EXPRESSION FOR BASE PRESSURE FLUCTUATION SPECTRA FOR BLUFF BODIES .........................................................................................................................................................................................................2366

Lawrence Dechant, Justin Smith

ASYMPTOTIC SOLUTIONS FOR GASEOUS FLOW IN A THREE-DIMENSIONAL RECTANGULAR MICROCHANNEL ......................................................................................................................................................................................2382

K. Al Khasawneh, H. Liu, C. Cai

A GRID BASED SURFACE TRACKING ALGORITHM FOR EFFICIENTLY COMPUTING LAGRANGIAN COHERENT STRUCTURES IN 3D UNSTEADY FLOWS ...................................................................................................................2393

Douglas Lipinski, Kamran Mohseni

CONSTRAINED AND UNCONSTRAINED AERODYNAMIC QUADRATIC PROGRAMMING OPTIMIZATION USING HIGH ORDER FINITE VOLUME METHOD AND ADJOINT SENSITIVITY COMPUTATION .........................................................................................................................................................................................2403

Mohammad Azab, Carl Ollivier-Gooch

AN INITIAL VALUE PROBLEM APPROACH TO INVESTIGATE BIGLOBAL STABILITY PROBLEMS ............................2425Christoph Brehm, Hermann Fasel

FLOW STRUCTURES OF GASEOUS JETS INJECTED INTO WATER FOR UNDERWATER PROPULSION......................2446J. Tang, C. Tseng, N. Wang, W. Shyy

NEAR-FIELD TRAJECTORY OF CIRCULAR LIQUID JETS INJECTED INTO SUBSONIC GASEOUS CROSSFLOW...............................................................................................................................................................................................2462

Seyedmohsen Najafi Marzbali, Ali Dolatabadi

THE BEHAVIOR OF BUBBLE AND WATER JET INDUCED BY UNDERWATER EXPLOSION IN A RECTANGULAR TUBE.............................................................................................................................................................................2472

Taketoshi Koita, Yujian Zhu, Mingyu Sun

INTERACTION OF A PLANAR SHOCK WITH A DENSE FIELD OF PARTICLES IN A MULTIPHASE SHOCK TUBE ..............................................................................................................................................................................................2482

J. Wagner, S. Beresh, S. Kearney, W. Trott, C. Jaime, B. Pruett, M. Baer

NUMERICAL SIMULATIONS OF MULTIPHASE FLOW IN SUPERSONIC MICRO-NOZZLES .............................................2495Benjamin Greenfield, William Louisos, Darren Hitt

COMPARISON OF RANS, DES AND DDES RESULTS FOR ONERA M-6 WING AT TRANSONIC FLOW SPEED USING AN IN-HOUSE PARALLEL CODE ..............................................................................................................................2511

Naveed Durrani, Ning Qin

AN OVERSET UNSTRUCTURED MESH DISCONTINUOUS GALERKIN APPROACH FOR AERODYNAMIC PROBLEMS .................................................................................................................................................................2524

Cristian Nastase, Dimitri Mavriplis, Jay Sitaraman

DYNAMIC MESH DEFORMATION FOR ADAPTIVE GRID RESOLUTION ENHANCEMENT WITH STAGGERED SPECTRAL DIFFERENCE AND FINITE VOLUME MESH ....................................................................................2536

Kui Ou, Antony Jameson

A HYBRIDIZED DISCONTINUOUS PETROV-GALERKIN METHOD FOR COMPRESIBLE FLOWS...................................2552David Moro, Ngoc Cuong Nguyen, Jaime Peraire, Jay Gopalakrishnan

KINETIC ENERGY CONSERVING DISCONTINUOUS GALERKIN SCHEME............................................................................2570Yves Allaneau, Antony Jameson

A CLASS OF RECONSTRUCTED DISCONTINUOUS GALERKIN METHODS FOR COMPRESSIBLE FLOWS ON ARBITRARY GRIDS ...........................................................................................................................................................2583

H. Luo, Y. Xia, R. Norgaliev, C. Cai

A DISCONTINUOUS GALERKIN DISCRETIZATION WITH MULTIWAVELET-BASED GRID ADADPTATION FOR COMPRESSIBLE FLOWS ................................................................................................................................2601

F. Iacono, G. May, S. Müller, R. Schäfer

SPRAY CHARACTERISTICS OF A PRESSURE SWIRL NOZZLE UNDER AN ATMOSPHERIC CONDITION DUE TO FLASH BOILING ........................................................................................................................................................................2623

Wonho Kim, Woongsup Yoon

NUMERICAL STUDY OF DETONATION-TURBULENCE INTERACTION ..................................................................................2637Luca Massa, Monika Chauhan, Frank Lu

AN EXPERIMENTAL STUDY OF ELECTROSTATIC SPRAYS OF BIO-BUTANOL AT LOW FLOW RATES .....................2664Maria Agathou, Dimitrios Kyritsis

EVALUATION OF FLAME-PROLONGATION OF ILDM AND FLAMELET TABULATED CHEMISTRY APPROACHES FOR LAMINAR FLAMES ............................................................................................................................................2677

Pradeep Jha, Clinton Groth

RANS MODELS FOR SCALAR TRANSPORT IN ABLATING COMPRESSIBLE BOUNDARY LAYERS ...............................2696K. Braman, K. Koo, V. Raman, R. Upadhyay, O. Ozekoye

LARGE-EDDY SIMULATION OF SUPERSONIC, TURBULENT MIXING LAYERS DOWNSTREAM OF A SPLITTER PLATE ......................................................................................................................................................................................2710

Arjun Sharma, Rathakrishnan Bhaskaran, Sanjiva Lele

VOLUME 4

TEMPORAL DIRECT NUMERICAL SIMULATIONS OF OBLIQUE BREAKDOWN FOR A CONE AT MACH 3.5 ...................................................................................................................................................................................................................2735

Andreas Laible, Hermann Fasel

INVESTIGATIONS OF INFLUENCE OF FREE STREAM TURBULENCE AND ACOUSTIC DISTURBANCES ON THE LAMINAR-TURBULENT TRANSITION ON LV6 AIRFOIL AND SWEPT WING MODE ..........................................2768

S. Chernyshev, A. Ivanov, A. Kiselev, V. Kuzminsky, D. Sboev, S. Zhigulev

ERROR AND WORK ESTIMATES FOR HIGH-ORDER ELEMENTS ............................................................................................2786Rainald Lohner

GOAL-ORIENTED ERROR ESTIMATION AND HP-ADAPTIVE MESH REFINEMENT FOR AERODYNAMIC FLOWS .........................................................................................................................................................................2794

Tobias Leicht, Ralf Hartmann

A NUMERICAL STUDY OF ADJOINT-BASED MESH ADAPTATION FOR COMPRESSIBLE FLOW SIMULATION ..............................................................................................................................................................................................2810

Jochen Schuetz, Georg May

EFFICIENT RESIDUAL-BASED MESH ADAPTATION FOR 1D AND 2D CFD APPLICATIONS.............................................2827Aniruddha Choudhary, Christopher Roy

EVALUATION OF EXTRAPOLATION-BASED DISCRETIZATION ERROR AND UNCERTAINTY ESTIMATORS .............................................................................................................................................................................................2843

Tyrone Phillips, Christopher Roy

THEORETICAL, COMPUTATIONAL AND EXPERIMENTAL STUDIES OF A FLAT PLATE UNDERGOING HIGH-AMPLITUDE PITCHING MOTION............................................................................................................................................2861

Kiran Ramesh, Ashok Gopalarathnam, Jack Edwards, Michael Ol, Kenneth Granlund

AERODYNAMICS OF A SUCCESSFUL PERCHING MANEUVER .................................................................................................2873Tyler Krone, Yeon Baik, Jonathan Rausch, Luis Bernal

THREE-DIMENSIONAL FLOW STRUCTURE ON A HEAVING LOW-ASPECT-RATIO WING..............................................2886Miguel Visbal

UNSTEADY FORCE GENERATION AND VORTEX DYNAMICS OF PITCHING AND PLUNGING FLAT PLATES AT LOW REYNOLDS NUMBER.............................................................................................................................................2910

Y. Baik, L. Bernal, W. Shyy, M. Ol

LATTICE BOLTZMANN SIMULATIONS OF PLUNGE AND PITCH OF A 3-D CHORD-WISE FLEXIBLE WING IN A LOW REYNOLDS NUMBER FLOW.................................................................................................................................2945

Dewei Qi, Yingming Liu

CONTROL VOLUME ANALYSIS OF BOUNDARY LAYER INGESTING PROPULSION SYSTEMS WITH OR WITHOUT SHOCK WAVE AHEAD OF THE INLET...................................................................................................................2971

Hyun Kim, James Felder

SUPERCONDUCTING ELECTRIC DISTRIBUTED PROPULSION STRUCTURAL INTEGRATION AND DESIGN IN A SPLIT-WING REGIONAL AIRLINER..........................................................................................................................2982

A. Gibson, D. Hall, M. Waters, B. Schiltgen, T. Foster, K. Papathakis

SPLIT-WING PROPULSOR DESIGN AND ANALYSIS FOR ELECTRIC DISTRIBUTED PROPULSION ..............................2997B. Schiltgen, M. Green, D. Hall, A. Gibson, T. Foster, M. Waters

WEIGHTS AND EFFICIENCIES OF ELECTRIC COMPONENTS OF A TURBOELECTRIC AIRCRAFT PROPULSION SYSTEM ............................................................................................................................................................................3025

Gerald Brown

THE BENEFITS OF VARIABLE AREA FAN NOZZLES ON TURBOFAN ENGINES ..................................................................3043U. Michel

THE DEVELOPMENT OF A HIGH SPEED CENTRIFUGAL COMPRESSOR RESEARCH FACILITY ..................................3060R. Fleming, F. Lou, N. Key

FULLY COUPLED FLUID-STRUCTURAL INTERACTION OF A TRANSONIC ROTOR AT NEAR-STALL CONDITIONS USING DETACHED EDDY SIMULATION.................................................................................................................3072

Xiangying Chen, Hongsik Im, Ge-Cheng Zha

A FAST INFLUENCE COEFFICIENT METHOD FOR LINEARIZED FLUTTER AND FORCED-RESPONSE ANALYSIS ....................................................................................................................................................................................................3093

Kwen Hsu, Daniel Hoyniak

INLET BUZZ AND COMBUSTION OSCILLATION IN A LIQUID-FUELED RAMJET ENGINE .............................................3104Seong-Jin Kim, Hyo-Won Yeom, Hong-Gye Sung, Vigor Yang

AN ILES ANALYSIS OF TRANSVERSE JET INJECTION INTO SUPERSONIC CROSS-FLOW WITH SYNTHETIC TURBULENT BOUNDARY LAYER ...............................................................................................................................3124

Z. Rana, B. Thornber, D. Drikakis

STRUCTURES OF AERATED-LIQUID JETS INJECTED FROM VARIOUS NOZZLE CONTOURS .......................................3142K. Lin, C. Rajnicek, J. McCall, B. Fischer, C. Carter, K. Fezzaa

IMPROVED SIMULATION OF INFLOW DISTORTION FOR DIRECT-CONNECT SCRAMJET STUDIES ..........................3166Mark Hagenmaier, Dean Eklund, Ryan Milligan

MEASUREMENT OF FLAME CHARACTERISTICS OF A LOW SWIRL BURNER AT HIGH PRESSURES AND VELOCITIES......................................................................................................................................................................................3181

Karthik Periagaram, David Noble, Jerry Seitzman, Tim Lieuwen, Scott Martin, Enrique Portillo

BLOWOFF DYNAMICS OF ASYMMETRICALLY-FUELED BLUFFBODY FLAMES................................................................3190Steven Tuttle, Swetaprovo Chaudhuri, Kristin Kopp-Vaughan, Trevor Jenson, Baki Cetegen, Michael Renfro, Jeffrey Cohen

MODE SELECTION IN FLAME-VORTEX DRIVEN COMBUSTION INSTABILITIES ..............................................................3210R. Speth, S. Hong, S. Shanbogue, A. Ghoniem

VISUALIZATION OF SHEAR LAYER DYNAMICS IN A TRANSVERSELY EXCITED, ANNULAR PREMIXING NOZZLE...............................................................................................................................................................................3227

J. O`connor, T. Lieuwen, M. Kolb

EXPERIMENTAL AND NUMERICAL INVESTIGATION OF TURBULENT, LEAN, HIGH-STRAINED, CONFINED, JET FLAMES........................................................................................................................................................................3242

Massimiliano Di Domenico, Christian Beck, Oliver Lammel, Werner Krebs, B. Noll

SPONTANEOUS RAMAN SCATTERING MEASUREMENTS AND CFD SIMULATIONS OF MAJOR SPECIES AND TEMPERATURE IN A TURBULENT DILUTE HYDROGEN DIFFUSION FLAME..........................................3253

Joseph Ranalli, Peter Strakey

BURNER PLATFORM FOR SUB-ATMOSPHERIC PRESSURE FLAME STUDIES .....................................................................3263T. Ombrello, C. Carter, V. Katta

LAMINAR FLAME SPEEDS AND EXTINCTION STRETCH RATES OF SELECTED AROMATIC HYDROCARBONS......................................................................................................................................................................................3276

X. Hui, A. Das, K. Kumar, C. Sung

HIGH PRESSURE BURNING RATES AND MODEL COMPARISONS FOR HIGH-HYDROGEN CO, CH4, C2H4, AND C2H6 MIXTURES.....................................................................................................................................................................3283

J. Santner, M. Burke, F. Dryer, Y. Ju

SOOT CONCENTRATION AND TEMPERATURE MEASUREMENTS IN CO-FLOW LAMINAR PROPANE-AIR DIFFUSION FLAMES AT PRESSURES UP TO 7 BAR ..............................................................................................................3292

H. Gohari Darabkhani, J. Oakey, Y. Zhang

EFFECT OF HELIUM DILUTION ON FLAME STABILITY AND LAMINAR FLAME SPEEDS OF HYDROCARBON FUEL BLENDS AT ELEVATED PRESSURES.....................................................................................................3306

M. Krejci, A. Vissotski, W. Lowry, E. Petersen, W. Metcalfe, S. Burke, H. Curran, G. Bourque

VARIANCE REDUCTION TECHNIQUES FOR MONTE CARLO SOLUTION OF RADIATIVE TRANSFER IN HYPERSONIC FLOWS: HYBRID P1–MONTE CARLO ................................................................................................................3316

Andrew Feldick, Ankit Bansal, Michael Modest

RADIATIVE HEATING OF MARTIAN SPACE VEHICLE AT CRUCIAL POINTS OF TRAJECTORY ..................................3325Daniil Andrienko, Sergey Surzhikov

SPECTRAL MODELING OF RADIATIVE HEAT TRANSFER IN CARBONACEOUS ATMOSPHERES USING NEW K-DISTRIBUTION MODELS ...........................................................................................................................................3339

A. Bansal, M. Modest

VISCOUS SHOCK LAYER CALCULATION OF STAGNATION-REGION HEATING ENVIRONMENT IN NEPTUNE AEROCAPTURE .....................................................................................................................................................................3356

Chul Park

VARIANCE REDUCTION TECHNIQUES FOR MONTE CARLO SOLUTION OF RADIATIVE TRANSFER IN HYPERSONIC FLOWS: IMPORTANCE SAMPLING ...................................................................................................................3363

Andrew Feldick, Michael Modest

SIMULATION OF RADIATING FLOWS IN IMPULSIVE FACILITIES .........................................................................................3371R. Morgan, T. McIntyre, U. Sheikh

RADIATIVE AND CONVECTIOVE HEATING OF ORION SPACE VEHICLES AT EARTH ORBITAL ENTRIES.......................................................................................................................................................................................................3382

S. Surzhikov, J. Shang

UNCERTAINTY QUANTIFICATION IN HYPERSONIC REENTRY FLOWS DUE TO ALEATORY AND EPISTEMIC UNCERTAINTIES ...............................................................................................................................................................3404

Benjamin Bettis, Serhat Hosder

HIGH THERMAL CONDUCTIVE COMPOSITE CONTAINING A NETWORK OF VAPOR GROWN CARBON FIBER AND CARBON NANOTUBE IN ALUMINUM MATRIX .....................................................................................3425

Katsuhiko Sasaki, Kohei Fukuchi, Kazuaki Katagiri, Terumitsu Imanishi, Akiyuki Shimizu, Atsushi Kakitsuji

MODELING OF AIR FLOW IN DENSE-POPULATED AIR CONDITIONED SPACES................................................................3434Essam Khalil

INSULATION MATERIALS DEVELOPMENT FOR POTENTIAL VENUS SURFACE MISSIONS...........................................3442M. Pauken, L. Li, D. Almasco, L. Del Castillo, M. Van Luvender, J. Beatty, M. Knopp, J. Polk

INVERSE ESTIMATION OF FRONT SURFACE TEMPERATURE OF A PLATE WITH LASER HEATING AND CONVECTION-RADIATION COOLING .....................................................................................................................................3450

Jianhua Zhou, Yuwen Zhang, J. Chen, Z. Feng

LESSONS LEARNED FROM RECENT BLADE FAILURES: PRIMARY CAUSES AND RISK-REDUCING TECHNOLOGIES .......................................................................................................................................................................................3466

D. Griffin, M. Malkin

AEROELASTIC PROPERTIES OF BACKWARD SWEPT BLADES................................................................................................3475Morten Hansen

EXPERIMENTAL BEND-TWIST COUPLING PROPERTIES OF THREE UNIDIRECTIONAL FIBER-REINFORCED COMPOSITE MATERIALS ..........................................................................................................................................3494

Justin Walsh, David Walrath

ANALYSIS OF FATIGUE LOADS OF WIND TURBINE BLADES SUBJECT TO COLD WEATHER CONDITIONS USING A FINITE ELEMENT MODEL ........................................................................................................................3501

P. Lillo, C. Crawford

ANALYSIS OF WIND SPEED MEASUREMENTS USING CONTINUOUS WAVE LIDAR FOR WIND TURBINE CONTROL.................................................................................................................................................................................3510

Eric Simley, Lucy Pao, Rod Frehlich, Bonnie Jonkman, Neil Kelley

IMPROVING YAW ALIGNMENT USING SPINNER BASED LIDAR..............................................................................................3526Knud Kragh, Morten Hansen, Torben Mikkelsen

AIRCRAFT DESIGN FOR REDUCED CLIMATE IMPACT ..............................................................................................................3539Emily Schwartz, Ilan Kroo

PERFORMANCE AND NOISE TRADE-OFFS ON A CIVIL AIRLINER WITH OVER-THE-WING ENGINES ......................3559S. Powell, A. Sóbester, P. Joseph

DESIGN AND OPTIMIZATION OF FUTURE AIRCRAFT FOR ASSESSING THE FUEL BURN TRENDS OF COMMERCIAL AVIATION .....................................................................................................................................................................3576

T. Economon, S. Copeland, J. Alonso, M. Zeinali, D. Rutherford

NOISE ASSESSMENT OF THE DOUBLE-BUBBLE AIRCRAFT CONFIGURATION..................................................................3596Elena De La Rosa Blanco, James Hileman

DETERMINATION OF LEAD AZIDE ARRHENIUS KINETICS CONSTANTS.............................................................................3605C. Bulian, H. Lee, L. Thompson

MODELING THE ENERGY RELEASE AND BURN RATE CHARACTERISTICS OF ZPP BASED INITIATORS ................................................................................................................................................................................................3616

B. Poulsen, K. Rink

COMPUTATIONAL ANALYSIS OF SOLID OXIDE FUEL CELL WITH FUNCTIONALLY GRADED ELECTRODES .............................................................................................................................................................................................3624

Chao Wang, George Huang, Ryan Miller

INTRODUCTION OF PARACHUTE AERODYNAMICS INTO AN UNDERGRADUATE AERODYNAMICS COURSE........................................................................................................................................................................................................3634

Eugene Niemi, Christopher Niezrecki, Kenneth Desabrais

VOLUME 5

A MODERN COMPRESSIBLE FLOW LABORATORY EXPERIENCE FOR UNDERGRADUATES ........................................3645

Frank Lu, Sikander Ali, Eric Braun, Luca Maddalena

INQUIRY BASED ENGINEERING LABS PREDICT STUDENT SUCCESS....................................................................................3657E. Moscovitch, C. Huff, K. Boykin, S. Olcmen, S. Wood, A. Haque, C. Lawson, J. Bonn

CCSU MOONBUGGY-2 SENIOR CAPSTONE DESIGN PROJECT, AS A ROAD MAP TO THE SUCCESSFUL ENGINEERING CAREER AND EFFECTIVE ASSESSMENT ................................................................................3663

Viatcheslav Naoumov, Nidal Al-Masoud, Jeffrey Cloutier

NUMERICAL SIMULATIONS AND PERFORMANCE COMPARISON OF AIR-BLAST AND PRESSURE JET ATOMIZERS................................................................................................................................................................................................3673

Y. Bhatt, D. Arora, R. Shaw, V. Golubev

PROPER ORTHOGONAL DECOMPOSITION ON A SUBSONIC JET EXHAUSTED FROM AN AXISYMMETRIC NOZZLE AND CHEVRON NOZZLES WITH VARYING PENETRATION...................................................3692

Bhupatindra Malla, Daniel Cuppoletti, Jeff Kastner, Ephraim Gutmark

ANALYSIS OF MODIFIED COMPRESSIBILITY CORRECTIONS FOR TURBULENCE MODELS ........................................3704Nico Gross, Gregory Blaisdell, Anastasios Lyrintzis

GRID REFINEMENT STRATEGIES FOR LARGE EDDY SIMULATION OF ROUND JETS.....................................................3723Gregory Rodebaugh, Lester Su

PARALLEL ADAPTIVE MESH RENMENT SCHEME WITH PRESUMED CONDITIONAL MOMENT AND FPI TABULATED CHEMISTRY FOR TURBULENT NON-PREMIXED COMBUSTION............................................................3734

P. Jha, C. Groth

AN EMPIRICAL REDUCED ORDER MODEL OF THE MACH 0.6 TURBULENT AXISYMMETRIC JET.............................3751Jeremy Pinier, Mark Glauser

INSTABILITY AND TRANSITION RESEARCH IN A MACH-6 QUIET TUNNEL........................................................................3762A. Chou, B. Wheaton, C. Ward, P. Gilbert, L. Steen, S. Schneider

OFF-BODY BOUNDARY-LAYER MEASUREMENT TECHNIQUES DEVELOPMENT FOR SUPERSONIC LOW-DISTURBANCE FLOWS ................................................................................................................................................................3787

Lewis Owens, Michael Kegerise, Stephen Wilkinson

STREAMWISE VORTICITY, LAMINAR SEPARATION AND TRANSITION IN FLOWS OVER TURBOMACHINERY BLADES ...............................................................................................................................................................3809

J. Gostelow, W. McMullan, G. Walker

NUMERICAL STUDY OF MECHANISM OF U-SHAPED VORTEX FORMATION......................................................................3821Ping Lu, Chaoqun Liu, Qin Li

NUMERICAL STUDY OF MECHANISM OF SMALL VORTEX GENERATION IN BOUNDARY LAYER TRANSITION ...............................................................................................................................................................................................3834

Ping Lu, Chaoqun Liu

LARGE EDDY SIMULATIONS OF CHANNEL FLOW WITH FLUID INJECTION THROUGH A POROUS WALL ............................................................................................................................................................................................................3853

M. Dupuy, E. Radenac, Y. Fabignon, F. Plourde

MODELING FOR CFD IN AERO-MECHANICAL DESIGN ..............................................................................................................3867Clark Briggs

SIMULATION OF FLOW OVER SUBOFF BARE HULL MODEL ...................................................................................................3878A. Gross, A. Kremheller, H. Fasel

COMPUTATIONAL INVESTIGATION OF HEAVY FUEL FEASIILITY IN A GASOLINE DIRECT INJECTION SPARK IGNITION ENGINE ..............................................................................................................................................3900

S. Moda, H. Dong, H. Wan, J. Hoke

INTEGRATION OF COMPUTATIONAL FLUID DYNAMICS WITH DYNAMIC SYSTEMS MODELING TO SIMULATE CONTROL OF AUTONOMOUS VEHICLES ..................................................................................................................3910

Michael Martin

STUDIES ON FLUIDIC INJECTION THRUST VECTORING IN AEROSPIKE NOZZLES.........................................................3917K. Hanumanthrao, S. Ragothaman, B. Arun Kumar, M. Giri Prasad, V. Sanal Kumar

SHOCK-BUBBLE INTERACTION SIMULATIONS USING A NEW TWO-PHASE DISCONTINUOUS GALERKIN METHOD ...............................................................................................................................................................................3928

Leandro Gryngarten, Suresh Menon

HIGH-ORDER MULTI-DIMENSIONAL LIMITING FOR TURBULENT FLOWS AND COMBUSTION .................................3949Peter Gerlinger

LIMITERS FOR DISCONTINUOUS GALERKIN DISCRETIZATIONS FOR MIXED TYPE MESHES WITH P-TYPE ADAPTIVITY ...............................................................................................................................................................................3982

Konstantinos Kontzialis, John Ekaterinaris

HIGH-ORDER CESE METHODS FOR THE EULER EQUATIONS .................................................................................................4000David Bilyeu, Yung-Yu Chen, S.-T. John Yu

ASSESSMENT OF PROPULSION SYSTEM CONFIGURATION AND FUEL COMPOSITION ON HYBRID WING BODY FUEL EFFICIENCY ..........................................................................................................................................................4014

S. Sato, P. Mody, D. Hall, E. De La Rosa Blanco, J. Hileman

AN EXAMINATION OF THE EFFECT OF BOUNDARY LAYER INGESTION ON TURBOELECTRIC DISTRIBUTED PROPULSION SYSTEMS .............................................................................................................................................4031

J. Felder, H. Kim, G. Brown, J. Chu

AERODYNAMIC SIMULATION OF FLOWS IN A HIGHLY LOADED TURBINE ......................................................................4057Federico Aguilar, Roger L. Davis, John P. Clark

FLOW ANALYSIS OF A HIGHLY LOADED LOW-PRESSURE TURBINE ...................................................................................4068Christine McClelland, Roger Davis, John Clark

TIME-ACCURATE CFD ANALYSIS ON THE EFFECTS OF UPSTREAM STATOR LOADING AND BLADE ROW INTERACTIONS ON STATOR SUCTION SIDE BOUNDARY LAYER BEHAVIOR .........................................................4080

Kenneth Clark, Steven Gorrell

FORCED VIBRATION OF A TURBINE CASCADE UNDER LOW AND HIGH ENGINE ORDER EXCITATION PREDICTED BY TRANSFORMATION TECHNIQUES...........................................................................................4092

I. Lee, S. Shin, T. Kim

THE INFLUENCE OF TURBULENCE-CHEMISTRY INTERACTION MODELLING FOR SUPERSONIC COMBUSTION ............................................................................................................................................................................................4111

Peter Cocks, William Dawes, Stewart Cant

INVESTIGATION OF SEGMENTED BLEED MODEL IN SUPERSONIC TURBULENT BOUNDARY LAYER .....................4123S. Manavasi, A. Morell, A. Hamed

NUMERICAL STUDY ON TURBULENT STRUCTURE OF TRANSVERSE JET INTO A SUPERSONIC FLOW ............................................................................................................................................................................................................4141

Junya Watanabe, Toshinori Kouchi, Kenichi Takita, Goro Masuya

MIXING CHARACTERISTICS OF ACTIVE MICROJET-BASED ACTUATORS IN A SUPERSONIC BACKWARD-FACING STEP FLOW ......................................................................................................................................................4155

K. Ahmed, M. Ali, F. Alvi

MULTI-DISCIPLINARY DECONTAMINATION ASSESSMENT OF AN INTERNAL ELECTRONICS BAY..........................4168Rick Graves, Hugh Griffis

A METHOD TO CORRELATE AMBIENT WIND TO FABRIC FACE VELOCITY AND PERMEABILITY............................4191T. Ghee, K. Murphy

AN NPSS MODEL OF A PROPOSED ALTITUDE TEST FACILITY................................................................................................4206B. Huffman, T. Lavelle, A. Owen

ENERGY TRANSFER EFFECTS DURING CHEMICALLY ACTIVATED DECOMPOSITION OF LARGER AROMATIC COMPOUNDS ......................................................................................................................................................................4213

B. Lefort, W. Tsang

A SHOCK TUBE EXPERIMENTAL STUDY AND KINETIC MODELING OF M-XYLENE IGNITION DELAY....................4225Saumitra Saxena, Giacomo Flora, Moshan Kahandawala, Sukh Sidhu

AUTOIGNITION, FLAME PROPAGATION, AND EXTINCTION OF BINARY FUEL BLENDS OF N-DECANE/ETHYLENE AND N-DECANE/METHANE..........................................................................................................................4243

Kamal Kumar, Xin Hui, Apurba Das, Chih-Jen Sung

AUTOIGNITION OF BUTANOL ISOMERS AT LOW TO INTERMEDIATE TEMPERATURE AND ELEVATED PRESSURE ............................................................................................................................................................................4252

Bryan Weber, Kamal Kumar, Chih-Jen Sung

EXTINCTION LIMITS OF C1-C4 HYDROCARBON AND AIR NONPREMIXED FLAMES RELEVANT FOR HYPERSONIC APPLICATIONS ..............................................................................................................................................................4260

Brendyn Sarnacki, Harsha Chelliah

RADICAL INDEX ON EXTINCTION LIMITS OF DIFFUSION FLAMES FOR LARGE HYDROCARBON FUELS ...........................................................................................................................................................................................................4267

Sang Hee Won, Stephen Dooley, Frederick Dryer, Yiguang Ju

IGNITION AND NEAR-WALL BURNING IN TRANSVERSE HYDROGEN JETS IN SUPERSONIC CROSSFLOW...............................................................................................................................................................................................4277

Mirko Gamba, M. Godfrey Mungal, Ronald Hanson

DEVELOPMENT OF A MODEL SCRAMJET COMBUSTOR ...........................................................................................................4292V. Miller, M. Gamba, M. Mungal, R. Hanson

STRATIFIED JET FLAMES IN A HEATED (1364K) CROSS-FLOW WITH AUTO-IGNITION .................................................4302Daniel Micka, James Driscoll

A MULTIVARIATE QUADRATURE BASED MOMENT METHOD FOR SUPERSONIC COMBUSTION MODELING..................................................................................................................................................................................................4314

Pratik Donde, Heeseok Koo, Venkat Raman

LARGE EDDY SIMULATION OF SUPERSONIC COMBUSTION IN A CAVITY-STRUT FLAMEHOLDER .........................4322C. Ghodke, J. Choi, S. Srinivasan, S. Menon

INTERACTIONS OF DETONATIONS WITH RAMPS ........................................................................................................................4341C. Stevens, V. Gamezo, P. King, F. Schauer, J. Hoke

LES OF H2O2 COAXIAL JET FLAMES IN A MULTIPLE-INJECTOR COMBUSTOR ................................................................4350Shingo Matsuyama, Junji Shinjo, Satoru Ogawa, Yasuhiro Mizobuchi

SUPERCRITICAL LOX/METHANE COMBUSTION OF A SHEAR COAXIAL INJECTOR.......................................................4363Hongfa Huo, Vigor Yang

COMBUSTION INSTABILITY COUPLING MECHANISMS BETWEEN ACOUSTICS AND LOX/CH4 SPRAY FLAMES........................................................................................................................................................................................................4376

Mark Sliphorst, Gröning Stefan, Bernhard Knapp, Michael Oschwald

EFFECTS OF HYDROGEN ADDITION ON COMBUSTION STABILITY OF AN UNSTABLE METHANE ROCKET COMBUSTOR ...........................................................................................................................................................................4391

S. Rosen, M. Pfeil, Y. Yu, W. Anderson

NUMERICAL STUDY OF THE FLAME AIMING FOR THE EVALUATION OF COMBUSTION INSTABILITY AT THE ATMOSPHERIC PRESSURE ........................................................................................................................4401

Dan Hori, Shingo Matsuyama, Taro Shimizu, Seiji Yoshida, Shigeru Tachibana, Yasuhiro Mizobuchi

A BROADBAND MULTI-HOP NETWORK FOR EARTH-MARS COMMUNICATION USING MULTI-PURPOSE INTERPLANETARY RELAY SATELLITES AND LINEAR-CIRCULAR COMMUTATING CHAIN TOPOLOGY .................................................................................................................................................................................................4404

S. Haque

CONSTRUCTION OF LOGISTICS NETWORK FOR FUTURE SUSTAINABLE MANNED MARS EXPLORATION TO REDUCE LOGISTICS RISK ...............................................................................................................................4432

Yasuhiro Akiyama, Yoshifumi Inatani

CONCEPTUAL DESIGN OF A LUNAR LANDING MISSION USING KOREA SPACE LAUNCH VEHICLE 2 ......................4439Y. Moon, T. Jang, C. Park, S. Kwon

CONCEPTUAL DESIGN OF A SMALL LUNAR RETURN VEHICLE.............................................................................................4451Sungkwon Jo, Chul Park, Sejin Kwon

HERRO MARS: DESIGN STUDY FOR A HIGHLY-ROBOTIC HUMAN MISSION TO MARS.................................................4456S. Oleson, G. Landis, M. McGuire, G. Schmidt

HUMAN TELEROBOTIC EXPLORATION OF VENUS: A FLEXIBLE PATH DESIGN STUDY ...............................................4470G. Landis, R. Dyson, M. McGuire, S. Oleson, G. Schmidt, J. Grantier, L. Burke, I. Dux, M. Bur, J. Fincannon, K. Bury, M. Mongalier, G. Williams, J. Warner, T. Packard, A. Colozza, M. Martini, J. Fittje, P. Schmitz, J. Gyekenyesi, D. McCurdy

HIGH RESOLUTION MICRO-OPTICAL WALL SHEAR STRESS SENSOR .................................................................................4487Ulas Ayaz, Tindaro Ioppolo, Volkan Otugen

SIMULATION OF UNSTEADY NANO-PARTICLE HEAT TRANSFER IN A ONE-DIMENSIONAL SLOT ............................4496Michael Martin, Karl Yee

MATHEMATICAL MODELING OF VARIABLE CONDUCTANCE HEAT PIPES FOR STEADY STATE AND TRANSIENT OPERATION .......................................................................................................................................................................4507

T. Hoang, R. Baldauff, D. Mahony

LOOP HEAT PIPE WITH THERMAL CONTROL VALVE FOR VARIABLE THERMAL CONDUCTANCE LINK OF LUNAR LANDERS AND ROVERS ........................................................................................................................................4513

J. Hartenstine, W. Anderson, K. Walker, M. Brown

DUAL HEAT PULSE, DUAL LAYER THERMAL PROTECTION SYSTEM SIZING ANALYSIS AND TRADE STUDIES FOR HUMAN MARS ENTRY DESCENT AND LANDING ...............................................................................................4526

Mary McGuire

FLEXIBLE ABLATIVE THERMAL PROTECTION SIZING ON INFLATABLE AERODYNAMIC DECELERATOR FOR HUMAN MARS ENTRY DESCENT AND LANDING .................................................................................4541

M. McGuire, J. Arnold, A. Covington, I. Dupzyk

HEAT TRANSFER MEASUREMENT AND MODELING IN RIGID HIGH-TEMPERATURE REUSABLE SURFACE INSULATION TILES ..............................................................................................................................................................4550

Kamran Daryabeigi, Jeffrey Knutson, George Cunnington

VOLUME 6

ENHANCEMENT OF AERODYNAMIC HEATING REDUCTION IN HIGH ENTHALPY FLOWS WITH OPPOSING JET ...........................................................................................................................................................................................4564

T. Imoto, H. Okabe, Y. Tani, S. Aso

EXPERIMENTAL AND COMPUTATIONAL ANALYSIS OF A WIND TURBINE AIRFOIL WITH ACTIVE MICROTABS................................................................................................................................................................................................4576

Aubryn Cooperman, Raymond Chow, Scott Johnson, C. Van Dam

MODELING THE TEMPORAL RESPONSE OF A MICROTAB IN AN AEROELASTIC MODEL OF A WIND TURBINE ......................................................................................................................................................................................................4583

Peter Baek, Mac Gaunaa

A STUDY OF FLATBACK AIRFOILS IN DYNAMIC MOTION .......................................................................................................4593C. Mertes, M. Singh, J. Strike, M. Hind, A. Babbitt, J. Baker, J. Naughton, J. Sitaraman

DYNAMIC CHARACTERIZATION OF WIND TURBINE BLADE SECTION ...............................................................................4607Ashli Babbitt, John Strike, Christopher Mertes, Michael Hind, Manjinder Singh, Jonathan Naughton

ON THE SKIN FRICTION DRAG REDUCTION IN LARGE WIND TURBINES USING SHARP V-GROOVED RIBLETS .......................................................................................................................................................................................................4620

Leonardo Chamorro, Roger Arndt, Fotis Sotiropoulos

LEADING-EDGE ROUGHNESS EFFECTS ON 633-418 AIRFOIL PERFORMANCE ...................................................................4627E. White, D. Kutz, J. Freels, J. Hidore, R. Grife, Y. Sun, D. Chao

SUMMARY OF THE TANDEM CYLINDER SOLUTIONS FROM THE BENCHMARK PROBLEMS FOR AIRFRAME NOISE COMPUTATIONS-I WORKSHOP ......................................................................................................................4640

David Lockard

EXPERIMENTAL STUDIES ON A RUDIMENTARY FOUR WHEEL LANDING GEAR ............................................................4662Lakshmi Venkatakrishnan, N. Karthikeyan, Kevin Mejia

ANALYSIS OF EXPERIMENTAL AND NUMERICAL STUDIES OF THE RUDIMENTARY LANDING GEAR ....................4679Philippe Spalart, Kevin Mejia

VEHICLE SKETCH PAD (VSP) STRUCTURAL LAYOUT TOOL ...................................................................................................4694Armand Chaput, Erdem Akay, Sergio Rizo-Patron

CONVERSION OF COMPONENT-BASED POINT DEFINITION TO VSP MODEL AND HIGHER-ORDER MESHING .....................................................................................................................................................................................................4708

Irian Ordaz

MODIFICATION OF VEHICLE SKETCH PAD FOR THE HYBRID WING BODY CONCEPT .................................................4714M. Link, A. Ko, P. Gelhausen, A. Tumbull

HYBRID WING BODY PLANFORM DESIGN WITH VEHICLE SKETCH PAD ...........................................................................4727Douglas Wells, Erik Olson

RECENT ADVANCES IN HIGH-ENERGY, HIGH-REPETITION RATE DIAGNOSTICS FOR PLIF, RAYLEIGH, AND RAMAN SCATTERING IMAGING IN TURBULENT REACTING FLOWS .................................................4735

Jeffrey Sutton, Walter Lempert

REQUIREMENTS, CAPABILITIES AND ACCURACY OF TIME-RESOLVED PIV IN TURBULENT REACTING FLOWS ...................................................................................................................................................................................4750

Mirko Gamba, Noel Clemens

PERFORMANCE CRITERIA - THE MISSING LINK IN ASSESSMENT CHAIN FOR CONTINUOUS PROGRAM IMPROVEMENT ..................................................................................................................................................................4782

Swami Karunamoorthy

APPLICATIONS OF HIGH-ORDER WEIGHTED COMPACT NONLINEAR SCHEME FOR COMPLEX TRANSONIC FLOWS.................................................................................................................................................................................4788

Xiaogang Deng, Guangxue Wang, Guohua Tu, Meiliang Mao

DEVELOPMENT AND VALIDATION OF A HIGH-ORDER SHOCK-FITTING NON-EQUILIBRIUM FLOW SOLVER ........................................................................................................................................................................................................4799

X. Wang, X. Zhong

A BANDWIDTH AND ORDER OPTIMIZED WENO INTERPOLATION SCHEME FOR COMPRESSIBLE TURBULENT FLOWS................................................................................................................................................................................4823

Nathan Mullenix, Datta Gaitonde

HIGH-ORDER SOLUTION-ADAPTIVE CENTRAL ESSENTIALLY NON-OSCILLATORY (CENO) METHOD FOR VISCOUS FLOWS .............................................................................................................................................................................4841

Lucian Ivan, Clinton Groth

IMPROVEMENT OF MIXING FUNCTION FOR MODIFIED UPWINDING COMPACT SCHEME .........................................4871Huankun Fu, Ping Lu, Chaoqun Liu

HIGH-ORDER NONLINEAR SCHEMES FOR VISCOUS TERMS AND THE APPLICATION TO COMPLEX CONFIGURATION PROBLEMS .............................................................................................................................................................4880

H. Liu, X. Deng, M. Mao, G. Wang

STABILITY OF BOUNDARY LAYERS IN BINARY MIXTURES OF OXYGEN AND NITROGEN...........................................4892Erman Ulker, Jill Klentzman, Anatoli Tumin

RECEPTIVITY OF HYPERSONIC BOUNDARY LAYERS TO ACOUSTIC AND VORTICAL DISTURBANCES.........................................................................................................................................................................................4913

Ponnampalam Balakumar, Michael Kegerise

PRESSURE FLUCTUATIONS BENEATH TURBULENT SPOTS AND INSTABILITY WAVE PACKETS IN A HYPERSONIC BOUNDARY LAYER ......................................................................................................................................................4945

Katya Casper, Steven Beresh, Steven Schneider

INSTABILITY OF HYPERSONIC BOUNDARY LAYER ON A WALL WITH RESONATING MICRO-CAVITIES .....................................................................................................................................................................................................4966

Alexander Fedorov, Guillaume Brès, Matthew Inkman, Tim Colonius

TRANSITION INITIATED BY A LOCALIZED DISTURBANCE IN A HYPERSONIC FLAT-PLATE BOUNDARY LAYER ..................................................................................................................................................................................4980

Jayahar Sivasubramanian, Hermann Fasel

NUMERICAL SIMULATIONS ON MODE S GROWTH OVER FELTMETAL AND REGULAR POROUS COATINGS OF A MACH 5.92 FLOW .....................................................................................................................................................5004

X. Wang, X. Zhong

NONLINEAR STRUCTURAL RESPONSE IN FLEXIBLE FLAPPING WINGS WITH DIFFERENT DENSITY RATIO ...........................................................................................................................................................................................................5031

Min Xu, Mingjun Wei, Tao Yang, Thomas Burton, Young Lee

COMPUTATIONAL INVESTIGATION OF FLOW OVER INFLATABLE AIRFOILS AT MULTIPLE REYNOLDS NUMBERS.............................................................................................................................................................................5040

D. Takahashi, R. Lebeau

COMPUTATIONAL FLUID-BODY INTERACTION OF HINGE CONNECTED FLAPPING PLATE IN HOVER..........................................................................................................................................................................................................5051

H. Wan, H. Dong, G. Huang

INVESTIGATION OF PROGRESSIVE STRUCTURAL FAILURE DUE TO SOFT BODY IMPACT USING MESHLESS LAGRANGIAN AND COUPLED LAGRANGIAN-EULERIAN SCHEMES...............................................................5061

C. Chandra, T. Wong, J. Bayandor

THE CARBUNCLE CFD PROBLEM.......................................................................................................................................................5071Robert Maccormack

ACTIVE FLUX SCHEMES ........................................................................................................................................................................5084Timothy Eymann, Philip Roe

E-CUSP SCHEME FOR THE EQUATIONS OF MAGNETOTHYDRODYNAMICS WITH HIGH ORDER WENO SCHEME .........................................................................................................................................................................................5095

Yiqing Shen, Gecheng Zha, Manuel Huerta

AN UPWIND SOLVER FOR THE NATIONAL COMBUSTION CODE............................................................................................5112Peter Sockol

PROGRESSES IN GAS-KINETIC UPWIND EULER/NAVIER-STOKES SOLVERS.....................................................................5130Lei Tang

APPLICATION OF GAS-KINETIC BGK SCHEME IN THREE-DIMENSIONAL FLOW ............................................................5152Qibing Li, Song Fu

HOT FLOW TESTING OF DUAL BELL NOZZLES ............................................................................................................................5161C. Genin, R. Stark

AERODYNAMIC INTERFERENCE REDUCTION METHOD FOR TWO-STAGE LAUNCH VEHICLES SUPERSONIC SEPARATION ...................................................................................................................................................................5169

Taro Uematsu, Shigeru Aso, Yasuhiro Tani

EXPERIMENTAL STUDY ON ROCKET NOZZLE SIDE LOAD REDUCTION ............................................................................5181Ralf Stark, Chloé Génin

ANALYSIS OF SHOCK STRUCTURES ABOUT A ROCKET MOTOR THRUST CONTROL UNIT USING CFD ................................................................................................................................................................................................................5187

David Gonzalez

ORBIT INSERTION DYNAMICS OF A PICO-SATELLITE WITH RESPECT TO COUPLED SOLID-LIQUID DYNAMICS ..................................................................................................................................................................................................5202

Andre Baeten, Joachim Juettner

SUPERCRITICAL FLUID BEHAVIOR IN A COOLING CHANNEL ...............................................................................................5218David Taieb, Guillaume Ribert, Vigor Yang

LEADING EDGE VORTEX DEVELOPMENT ON A WAVING WING AT REYNOLDS NUMBERS BETWEEN 10,000 AND 60,000 .......................................................................................................................................................................................5229

Anya Jones, Holger Babinsky

HIGH-FIDELITY SIMULATIONS OF TRANSITIONAL AIRFOIL INTERACTING WITH UPSTREAM VORTICAL STRUCTURE.........................................................................................................................................................................5244

V. Golubev, L. Nguyen, M. Visbal

AN INVESTIGATION OF THE EFFECT OF FREESTREAM TURBULENCE ON THE LAMINAR SEPARATION BUBBLE ON AN SD7003 AIRFOIL ..............................................................................................................................5264

David Olson, Alan Katz, Ahmed Naguib, Manoochehr Koochesfahani, Donald Rizzetta, Miguel Visbal

VORTEX FORMATION AND SATURATION FOR LOW-ASPECT-RATIO ROTATING FLAT PLATES AT LOW REYNOLDS NUMBER ....................................................................................................................................................................5273

Adam Devoria, Priyanka Mahajan, Matthew Ringuette

MULTIDIMENSIONAL MODELING OF GAS MIXING IN TRANSIENT TRANSLATING CONFINED TURBULENT JETS.....................................................................................................................................................................................5308

Sameera Wijeyakulasuriya, Razi Nalim

SIMULATION OF PLASMA-SPARK-ENHANCED MIXING IN JET IN SUPERSONIC CROSSFLOW ...................................5325E. Tylczak, D. Peterson, G. Candler

CFD AIDED DEVELOPMENT OF AN EXPERIMENTAL SETUP TO INVESTIGATE INTERNAL SUPERSONIC COMBUSTION .................................................................................................................................................................5343

Felix Schranner, Mirko Gamba, M. Godfrey Mungal, Nikolaus Adams, Gianluca Iaccarino

MODELING HYPERSONIC PROPULSION USING FINITE ELEMENT CFD ...............................................................................5361Nicholas Moffitt, Cody Pinkerman, Andrew Arena

THE ROLE OF THE BAROCLINIC TERM IN SUPERSONIC FUEL/AIR MIXING ENHANCEMENT....................................5379L. Romagnosi, A. Ingenito, D. Cecere, E. Giacomazzi, C. Bruno

SCRAMJET ISOLATOR SHOCK TRAIN LOCATION TECHNIQUES ...........................................................................................5388John Hutzel, Douglas Decker, Richard Cobb, Paul King, Michael Veth, Jeffrey Donbar

NUMERICAL ANALYSIS OF A DIRECT CONNECT SUPERSONIC COMBUSTOR...................................................................5409F. Malo-Molina, H. Ebrahimi, D. Gaitonde

CFD ANALYSIS OF AN INLET-ISOLATOR COMBINATION FOR DUAL MODE SCRAMJET APPLICATIONS ..........................................................................................................................................................................................5427

F. Ferguson, M. Dhanasar, J. Grant, L. Uitenham, I. Blankson

NUMERICAL INVESTIGATIONS OF NOX-FORMATION IN SCRAMJET COMBUSTORS USING WALL AND STRUT INJECTORS .........................................................................................................................................................................5441

Markus Kindler, Peter Gerlinger, Manfred Aigner

CELEBRATING CENTENARY OF POWERED FLIGHT IN AUSTRALIA ....................................................................................5453S. Patsikatheodorou, G. Till, C. Bil

THE HISTORY OF AVIATION EDUCATION AND TRAINING .......................................................................................................5460J. Barata, F. Neves

BIRTH OF U.S. NAVAL AERONAUTICAL ENGINEERING AND PHENOMENAL RISE TO EXCELLENCE ......................5466David Haas, Eric Silberg, Judah Milgram

VOLUME 7

ESCAPING EARTH: HUMAN SPACEFLIGHT AS RELIGION ........................................................................................................5482

Roger Launius

ENVISIONING THE EARTH: CONCEPTIONS OF THIS PLANET FROM THE FLAT EARTH TO GAIA.............................5491Roger Launius

COMPUTATIONAL MODELING AND EXPERIMENTAL OBSERVATION OF COMPOSITIONAL STRATIFICATION IN PREMIXED FLAMES .......................................................................................................................................5498

D. Schmidt, D. Kyritsis, T. Kang

EFFECTS OF PRESSURE AND GRAVITY IN LAMINAR COFLOW ETHYLENE DIFFUSION FLAMES .............................5506Marc Charest, Clinton Groth, Ömer Gülder

LEAN BLOWOUT LIMITS FOR JP-8 SURROGATES AND THEIR PARENT COMPONENTS.................................................5527Viswanath Katta, Tei Newman-Lehman, Kal Seshadri, William Roquemore

MODELING OF SOOT SIZE DISTRIBUTIONS IN PARTIALLY PREMIXED C2H4/AIR FLAMES.........................................5538Thomas Blacha, Massimiliano Di Domenico, Nadezhda Slavinskaya, Peter Gerlinger, Manfred Aigner

COMPUTATION OF LAMINAR PREMIXED FLAMES USING REDUCED KINETICS BASED ON CONSTITUENTS AND SPECIES .............................................................................................................................................................5550

Kenneth Harstad, Josette Bellan

SIMULATIONS OF COMPOSITE SOLID PROPELLANT COMBUSTION USING ADAPTIVE MESH REFINEMENT .............................................................................................................................................................................................5564

Jung Choi, Mehtap Cakmak, Suresh Menon

RELATIVE DISPERSION OF CATALYTIC NANOPARTICLE ADDITIVES AND AP PARTICLES IN COMPOSITE SOLID PROPELLANT AND THE EFFECT ON BURNING RATE ..........................................................................5577

K. Kreitz, E. Petersen, D. Reid, S. Seal

OPTIMIZED DUAL-EXPANDER AEROSPIKE NOZZLE UPPER STAGE ROCKET ENGINE .................................................5585Joshua Hall, Carl Hartsfield, Joseph Simmons, Richard Branam

PERFORMANCE MODELING OF A PARAFFIN WAX / NITROUS OXIDE HYBRID ROCKET MOTOR .............................5614Bernard Genevieve, Michael Brooks, Jean Pitot De La Beaujardiere, Lance Roberts

DUAL PARTICLE LOADING FOR SOLID ROCKET INSTABILITY SYMPTOM SUPPRESSION...........................................5626David Greatrix

THE DEVIL’S IN THE TAILS – RELIABILITY PREDICTION METHODOLOGIES FOR THE ORION HEAT SHIELD .........................................................................................................................................................................................................5640

Jeremy Vander Kam, Austin Howard, Peter Gage, John Schiermeier

SYSTEM READINESS AND RISK ASSESSMENT FOR ADVANCED VEHICLE CONCEPTS – DISCUSSION OF FUNDAMENTAL CONCEPTS ...........................................................................................................................................................5652

Hernando Jimenez, Jeffery Schutte, Dimitri Mavris

A COMPUTATIONAL PREDICTION OF THE PERMEATION LEAK RATE PERFORMANCE OF A CANDIDATE SPACE SEAL ......................................................................................................................................................................5670

Nicholas Garafolo, Scott Sawyer

ADHESION OF AN ELASTOMER SEAL TO METAL AND ITS MITIGATION WITH ATOMIC OXYGEN PRETREATMENT ......................................................................................................................................................................................5685

M. Panickar, J. Wasowski, C. Daniels

COMPARTMENT VENTING ON THE ORION CREW MODULE DURING ATMOSPHERIC RE-ENTRY ............................5692Ries Smith

LIDAR-AIDED INERTIAL NAVIGATION WITH EXTENDED KALMAN FILTERING FOR PINPOINT LANDING OVER ROUGH TERRAIN.....................................................................................................................................................5705

D. Busnardo, M. Aitken, R. Tolson, D. Pierrottet, F. Amzajerdian

UNDERSTANDING PULSARS TO CREATE A FUTURE SPACE PROPULSOR ...........................................................................5721Paul Murad

RAMIFICATIONS OF EINSTEIN'S FIELD EQUATIONS FOR CREATING ADVANCED PROPULSION SCHEMES.....................................................................................................................................................................................................5730

Paul Murad

DEVELOPMENT AND TESTING OF AN AUTONOMOUS REGOLITH EXCAVATION AND DELIVERY SYSTEM ........................................................................................................................................................................................................5741

D. Boucher, T. Atwell, R. Theiss, R. Armstrong, S. Benigni

FUEL CELL INTEGRATION TO A MOBILITY PLATFORM ..........................................................................................................5751J. Richard, R. Gopal, D. Boucher, R. Theiss

SOLAR THERMAL SYSTEM FOR LUNAR ISRU APPLICATIONS: DEVELOPMENT AND FIELD OPERATION AT MAUNA KEA, HI ........................................................................................................................................................5759

Takashi Nakamura, Benjamine Smith

2010 FIELD DEMONSTRATION OF THE SOLAR CARBOTHERMAL REGOLITH REDUCTION PROCESS TO PRODUCE OXYGEN ...........................................................................................................................................................................5775

Robert Gustafson, Brant White, Michael Fidler

PROSPECTING FOR SPACE EXPLORATION ....................................................................................................................................5792L. Sigurdson, D. Boucher, R. Taylor, R. Armstrong, A. Deslauriers, E. Caillibot

LUNAR SOIL PARTICLE SEPARATOR................................................................................................................................................5801Mark Berggren, Robert Zubrin, Peter Jonscher, James Kilgore

PARTICLE SIZE, POROSITY AND TEMPERATURE EFFECTS ON CHAR CONVERSION ....................................................5819Islam Ahmed, Ashwani Gupta

REDUCTION OF CHAR USING STEAM AND O2/AIR ENRICHMENT .........................................................................................5835Henry Molintas, Ashwani Gupta

DESIGN AND CONSTRUCTION OF AN OPTICALLY-ACCESSIBLE COAL GASIFIER FOR CO2 REDUCTION USING EXCESS H2............................................................................................................................................................5853

I. Sircar, R. Gejji, A. Sane, D. Blunck, S. Meyer, J. Gore

EXAMINATION OF EMISSION SPECTRA FROM HYDROGEN SULFIDE FLAMES ................................................................5866H. Selim, A. Al Shoaibi, A. Gupta

DISPERSION OF A CLOUD OF PARTICLES BY A MOVING SHOCK: EFFECTS OF SHAPE, ANGLE OF INCIDENCE AND ASPECT RATIO ........................................................................................................................................................5887

Thomas Dittmann, Gustaaf Jacobs, Wai-Sun Don

TURBULENT SWIRLING FURNACE FLOWS: HISTORY AND DEVELOPMENT .....................................................................5904Essam Khalil

EFFECT OF FREE SURFACE HEAT TRANSFER ON THERMOCAPILLARY CONVECTION IN FLOATING ZONE LIQUID BRIDGE ............................................................................................................................................................................5922

I. Ahmed, J. Masud, M. Nigar

NUMERICAL STUDIES OF 3-D FLOW REGIMES IN A TOROIDAL THERMOSYPHON.........................................................5944El Hassan Ridouane, Darren Hitt, Christopher Danforth

VIBRATIONAL AND ROTATIONAL EXCITATION AND DISSOCIATION OF CO2 REEXAMINED .....................................5960Richard Jaffe

STATE-RESOLVED VIBRATIONAL RELAXATION MODELING FOR STRONGLY NONEQUILIBRIUM FLOWS ..........................................................................................................................................................................................................5974

I. Boyd, E. Josyula

UNIFIED GAS-KINETIC SCHEME FOR ALL KNUDSEN NUMBER FLOWS ..............................................................................5984Kun Xu, Juan-Chen Huang

ENERGY BIN BASED COUPLING MODEL FOR HIGH ENTHALPY FLOWS USING PRIOR RECOMBINATION DISTRIBUTION......................................................................................................................................................5999

Sriram Doraiswamy, Daniel Kelley, Graham Candler

COMPARATIVE ANALYSIS OF COUPLED RADIATION-GASDYANAMIC SOLUTION METHODOLOGY.......................6010Christopher Martin, Robert Greendyke

RADIATIVE GAS DYNAMICS OF MARTIAN SPACE VEHICLES .................................................................................................6039Sergey Surzhikov, Pierre Omaly

NONEQUILIBRIUM RADIATIVE GASDYNAMICS OF SEGMENTAL-CONICAL SPACE VEHICLE OF LARGE SIZE ................................................................................................................................................................................................6067

A. Djadkin, A. Beloshitsky, M. Shuvalov, S. Surzhikov

METASTABLE EQUILIBRIUM OF A DYNAMIC ELECTRICAL SYSTEM IN TERMS OF ENTROPY GENERATION RATE.................................................................................................................................................................................6096

J. Doty, K. Yerkes

ADVANCES IN WIND TURBINE SITE ASSESSMENT.......................................................................................................................6106D. Malcolm, K. Lybarger, G. Randall

TURBULENCE PATTERNS AROUND A LARGE WIND FARM ......................................................................................................6112Leonardo Chamorro, Roger Arndt, Fotis Sotiropoulos

PREDICTION OF WIND TURBINE PERFORMANCE AND WAKE LOSSES USING ANALYSIS METHODS OF INCREMENTAL COMPLEXITY ......................................................................................................................................................6120

Christopher Gundling, Beatrice Roget, Jayanarayanan Sitaraman

INVESTIGATION OF TURBINE RESPONSE TO VARIOUS WIND INFLOW MODELS............................................................6144Raj Rai, Manjinder Saini, Jonathan Naughton

EXPERIMENTAL STUDY ON THE WIND TURBINE WAKE MEANDERING WITH THE HELP OF A NON-ROTATION SIMPLIFIED MODEL AND OF A ROTATING MODEL..............................................................................................6155

Sandrine Aubrun, Stéphane Loyer, Guillaume Espana, Paul Hayden, Philip Hancock

2-D NUMERICAL ANALYSIS OF A VAWT WIND FARM FOR DIFFERENT CONFIGURATIONS ........................................6161Naveed Durrani, Ning Qin, Harris Hameed, Shahab Khushnood

GENERATION OF PARAMETRIC EQUIVALENT-AREA TARGETS FOR DESIGN OF LOW-BOOM SUPERSONIC CONCEPTS .......................................................................................................................................................................6172

Wu Li, Elwood Shields

EVALUATING MARKET AND ENVIRONMENTAL IMPACTS OF AN N+3 SUPERSONIC AIRCRAFT ...............................6181Isaac Tetzloff, William Crossley

INTEGRATION OF OFF-TRACK SONIC BOOM ANALYSIS IN CONCEPTUAL DESIGN OF SUPERSONIC AIRCRAFT ...................................................................................................................................................................................................6195

Irian Ordaz, Wu Li

INTEGRATION OF MULTIFIDELITY MULTIDISCIPLINARY COMPUTER CODES FOR DESIGN AND ANALYSIS OF SUPERSONIC AIRCRAFT ............................................................................................................................................6206

Karl Geiselhart, Lori Ozoroski, James Fenbert, Elwood Shields, Wu Li

STRUCTURED PROGRAMMING EDUCATION REQUIREMENTS FOR AEROSPACE ENGINEERING .............................6218Earnest Arrington

THREE-DIMENSIONAL ACTIVE FLOW CONTROL DRAG REDUCTION STUDIES OVER A BLUFF BODY USING A COUPLED LATTICE BOLTZMANN-NAVIER-STOKES METHODOLOGY ...............................................................6247

Nandita Yeshala, Lakshmi Sankar

NUMERICAL SIMULATION INVESTIGATING CONTROL OF FLOW OVER A FLAT-WINDOW TURRET ......................6260Philip Morgan, Miguel Visbal

HIGH-ACCURACY SIMULATIONS OF SYNTHETIC JETS FOR LOW-RE FLOW CONTROL...............................................6284H. Nakhla, A. Bourlier, L. Nguyen, S. Bhatt, J. Brodnick, V. Golubev

A SIMPLE SCHEME TO LIMIT REFINEMENT ZONES FOR SUPERSONIC FLOWS ...............................................................6296Rainald Lohner, Adrien Loseille

SPEED OF SOUND AND REAL GAS SOLUTION ALGORITHM FOR SUPERCRITICAL FLOWS .........................................6305S. Moon, J. Shin, J. Choi

A PDE-BASED MESH UPDATE METHOD FOR MOVING AND DEFORMING HIGH REYNOLDS NUMBER MESHES........................................................................................................................................................................................................6318

Richard Smith

DEVELOPMENT OF AN AERO-OPTICS SOFTWARE LIBRARY AND INTEGRATION INTO STRUCTURED OVERSET AND UNSTRUCTURED CFD SOLVERS...............................................................................................6334

W. Coirier, J. Stutts

A NEW CHANGING-TOPOLOGY ALE SCHEME FOR MOVING MESH UNSTEADY SIMULATIONS................................6353Geraldine Olivier, Frederic Alauzet

LOW REYNOLDS NUMBER EXPERIMENTS ON AN IMPULSIVELY STARTED FLAT PLATE AT HIGH INCIDENCE .................................................................................................................................................................................................6378

Charles Pitt Ford, Holger Babinsky

VOLUME 8

LOW-DIMENSIONAL STATE-SPACE REPRESENTATIONS FOR CLASSICAL UNSTEADY AERODYNAMIC MODELS ......................................................................................................................................................................6396

Steven Brunton, Clarence Rowley

TRANSIENT FORCE ON A ROTATING AR 2 SEMI-SPAN FLAT PLATE ....................................................................................6408John Puttmann, Aaron Altman

MULTI-SCALE TURBULENCE MODEL IN SIMULATION OF SUPERSONIC CROSSFLOW .................................................6420E. Hassan, H. Aono, J. Boles, D. Davis, W. Shyy

MODELING STRUCTURAL UNCERTAINTIES IN REYNOLDS-AVERAGED COMPUTATIONS OF SHOCK/BOUNDARY LAYER INTERACTIONS ..................................................................................................................................6437

Michael Emory, Rene Pecnik, Gianluca Iaccarino

NUMERICAL INVESTIGATION OF SHOCK-WAVE/ISOTROPIC TURBULENCE INTERACTION ......................................6453Nathan Grube, Ellen Taylor, Pino Martin

EXPERIMENTAL INVESTIGATIONS OF A HYPERSONIC SHOCK TURBULENT BOUNDARY LAYER INTERACTION ...........................................................................................................................................................................................6476

Anne-Marie Schreyer, Dipankar Sahoo, Alexander Smits

WALL MODELING IN LARGE-EDDY SIMULATION: PREDICTING ACCURATE SKIN FRICTION AT VERY HIGH REYNOLDS NUMBER.......................................................................................................................................................6488

S. Kawai, J. Larsson

DETACHED EDDY SIMULATION OF SHOCK TURBULENT BOUNDARY LAYER INTERACTION OVER A PROTRUSION .............................................................................................................................................................................................6508

Mohammad Badr, Klaus Hoffmann

PASSIVE CONTROL OF HIGH-SPEED SEPARATED FLOWS USING SPLITTER PLATES ....................................................6530Todd Reedy, Greg Elliott, J. Craig Dutton, Yeol Lee

FLOWFIELD CHARACTERISTICS OF OBLIQUE SHOCKS GENERATED USING MICROJET ARRAYS ..........................6540M. Ali, K. Ahmed, Rajan Kumar, Farrukh Alvi

EXPERIMENTAL INVESTIGATIONS ON STABILITY OF VORTEX FLOW OVER SLENDER DELTA WING WITH DORSAL FIN ......................................................................................................................................................................6555

Xuanshi Meng, Jinsheng Cai, Zhide Qiao, Shijun Luo, Feng Liu

FLOW SEPARATION CONTROL OVER AN AIRFOIL WITH NANOSECOND PULSE DRIVEN DBD PLASMA ACTUATORS .............................................................................................................................................................................6571

C. Rethmel, J. Little, K. Takashima, A. Sinha, I. Adamovich, M. Samimy

TRANSITORY CONTROL OF DYNAMIC STALL ON A MOVING AIRFOIL ..............................................................................6588G. Woo, A. Glezer

AN HP-ADAPTIVE DISCONTINUOUS GALERKIN SOLVER FOR AERODYNAMIC FLOWS ON MIXED-ELEMENT MESHES ..................................................................................................................................................................................6601

Nicholas Burgess, Dimitri Mavriplis

OUTPUT-BASED SPACE-TIME MESH ADAPTATION FOR UNSTEADY AERODYNAMICS..................................................6619Yuxing Luo, Krzysztof Fidkowski

A RESIDUAL-BASED PROCEDURE FOR HP-ADAPTATION ON 2-D HYBRID MESHES ........................................................6640Haiyang Gao, Z. J. Wang

AUTOMATED QUADRATURE-FREE DISCONTINUOUS GALERKIN METHOD APPLIED TO VISCOUS FLOWS ..........................................................................................................................................................................................................6653

Marshall Galbraith, Paul Orkwis, John Benek

BUTTERFLIES IN SPACE ........................................................................................................................................................................6685N. Moreno, G. Vogt, W. Thomson

STUDENT DROP TOWER COMPETITIONS: DROPPING IN A MICROGRAVITY ENVIRONMENT (DIME) AND WHAT IF NO GRAVITY? (WING) ................................................................................................................................................6689

Nancy Hall, Dennis Stocker, Richard Delombard

CONJUGATE ROTOR-STATOR INTERACTION PROCEDURE FOR FILM-COOLED TURBINE SECTIONS ....................6697Joshua Gottlieb, Roger Davis, John Clark

CONJUGATE HEAT TRANSFER SIMULATION OF COOLED TURBINE BLADES USING UNSTRUCTURED-MESH CFD SOLVER...............................................................................................................................................6709

Tetsuya Yoshiara, Daisuke Sasaki, Kazuhiro Nakahashi

THREE-DIMENSIONAL FILM-COOLED VANE CFD SIMULATIONS AND PRELIMINARY COMPARISON TO EXPERIMENTS ....................................................................................................................................................................................6719

J. Johnson, P. King, J. Clark, R. Anthony, P. Koch, M. Ooten, E. Kasik, R. Ni

IN-SITU STRAIN MEASUREMENTS OF EB-PVD THERMAL BARRIER COATINGS USING SYNCHROTRON X-RAY DIFFRACTION UNDER THERMO-MECHANICAL LOADING ........................................................6732

R. Diaz, M. Mossaddad, A. Bozan, S. Raghavan, J. Almer, J. Okasinski, H. Palaez-Perez, P. Imbrie

CONCEPTUAL DESIGN OF SHORT-RANGE TWO-STAGE SCRAMJET VEHICLE .................................................................6739I. Yang, C. Park, S. Choi, S. Yang

EFFECT OF THERMALLY INDUCED DEFORMATION IN UVA SUPERSONIC COMBUSTION FACILITY ......................6749A. Gupte, W. Engblom, C. Goyne, R. Rockwell

LASER-INDUCED PLASMA IGNITION EXPERIMENTS IN A SCRAMJET INLET ...................................................................6765Stefan Brieschenk, Sean O'Byrne, Harald Kleine

THE STABILIZED OBLIQUE DETONATION WAVE AND UNSTEADY WAVE STRUCTURE AROUND HYPER-VELOCITY SPHERICAL PROJECTILE ................................................................................................................................6778

Shinichi Maeda, Ryuichi Inada, Jiro Kasahara, Akiko Matsuo, Ikko Funaki

ANALYSIS OF HYDROGEN INJECTION INTO THE COMBUSTOR OF HYSHOT-II SCRAMJET ENGINE USING ILES .................................................................................................................................................................................................6786

Z. Rana, B. Thornber, D. Drikakis

COMMUNICATION THROUGH HYPERSONIC OR RE-ENTRY PLASMAS................................................................................6806C. Davis, P. Peterson, S. Bilen

DRGEP-BASED MECHANISM REDUCTION STRATEGIES: GRAPH SEARCH ALGORITHMS AND SKELETAL PRIMARY REFERENCE FUEL MECHANISMS ...........................................................................................................6818

Kyle Niemeyer, Chih-Jen Sung

HIGHER-ORDER CORRELATION OF KINETIC PARAMETERS FROM GLOBAL SENSITIVITY ANALYSIS WITH CONSIDERATION OF EXTINCTION PHENOMENA OF NON-PREMIXED FLAMES .............................6831

Gaetano Esposito, Harsha Chelliah

CORRELATIONS FOR THE LAMINAR FLAME SPEED, ADIABATIC FLAME TEMPERATURE AND IGNITION DELAY TIME FOR METHANE, ETHANOL AND N-DECANE ....................................................................................6839

Jan Michael Boyde, Andreas Fiolitakis, Massimiliano Di Domenico, Manfred Aigner

RECONCILE DISCREPANCIES OF CURRENT SYNGAS KINETICS MODELS BY CONSIDERING TURBULENCE EFFECTS ON IGNITION DELAY AT GAS-TURBINE RELEVANT OPERATING CONDITIONS ..............................................................................................................................................................................................6855

Matthias Ihme

THE ALGORITHM FOR AUTOMATIC CONSTRUCTION OF A GLOBAL REACTION MODEL ...........................................6871A. Zizin, N. Slavinskaya, U. Riedel, M. Aigner

OPTIMAL BAYESIAN EXPERIMENTAL DESIGN FOR COMBUSTION KINETICS .................................................................6882Xun Huan, Youssef Marzouk

STATIC STABILITY MARGIN SENSING IN A LEAN DIRECT INJECTION(LDI) COMBUSTOR AT ELEVATED PRESSURE ............................................................................................................................................................................6898

R. Bompelly, J. Seitzman

MICROJET INJECTION STRATEGIES FOR MITIGATING DYNAMICS IN A LEAN PREMIXED SWIRL-STABILIZED COMBUSTOR ....................................................................................................................................................................6912

Zachary Labry, Santosh Shanbhogue, Ahmed Ghoniem

A STUDY OF LEAN DIRECT-INJECTION FLAMES THROUGH SIMULTANEOUS PIV AND OH* CHEMILUMINESCENCE .........................................................................................................................................................................6926

R. Villalva Gomez, E. Gutmark

CHARACTERIZATION OF INSTABILITIES IN A LOW-SWIRL INJECTOR WITH EXHAUST GAS RECIRCULATION......................................................................................................................................................................................6936

Donald Ferguson, Joseph Ranalli

MEASUREMENT OF FLAME FREQUENCY RESPONSE FUNCTIONS IN A LOW-SWIRL FLAME UNDER EXHAUST GAS RECIRCULATION CONDITIONS.............................................................................................................................6945

Joseph Ranalli, Donald Ferguson

LES OF A CH4/AIR MESOCOMBUSTOR AT 3 ATM:EDC AND LAMINAR-RATE MODELS..................................................6952Angelo Minotti, Claudio Bruno

ELECTROSPRAY THRUSTER FOR CUBESAT ..................................................................................................................................6966S. Ober, R. Branam, R. Huffman, N. Demmons, R. Martin

µ-HALL EFFECT THRUSTER CHARACTERIZATION.....................................................................................................................6975J. De La Harpe, R. Branam, R. Huffman, S. Paintal, R. Tedrake

HIGH THRUST DENSITY PROPELLANTS IN HALL THRUSTERS...............................................................................................6990A. Hillier, R. Branam, R. Huffman, J. Szabo, S. Paintal

EXPLOSIONS, EXPULSION RATE, DISPERSION AND IGNITION OF RELEASED FUELS: A REVIEW .............................7005David Lilley

FDS: APPLICATION OF THE FIRE DYNAMICS SIMULATOR CODE TO A THREE-ROOM STRUCTURE WITH EXPERIMENTAL FIRES AND 60 SMOKE DETECTORS .....................................................................................................7032

V. Kulkarni, D. Lilley

ASSESSING EXPLOSION HAZARDS IN GAS TURBINE ENCLOSURES ......................................................................................7053O. Heynes, K. Clutter

FDS: GRID REFINEMENT STUDIES WITH THE FIRE DYNAMICS SIMULATOR CODE FOR ONE-ROOM STRUCTURAL FIRES WITH A VARIETY OF BURNING ITEMS ...................................................................................................7065

D. Mandloi, D. Lilley

BRANZFIRE: APPLICATION TO REALISTIC BURNING ITEMS IN A ROOM FIRE WITH SMOKE DETECTORS AND SPRINKLER ACTIVATION TIMES ....................................................................................................................7087

A. Raavi, D. Lilley

MULTIQUANTUM STATE-TO-STATE TRANSITIONS IN HYPERSONIC BLUNT BODY FLOWS ........................................7110Eswar Josyula, Abdelaziz Aliat, Prakash Vedula

EFFECT OF ESCAPE FACTOR TO A HYPERSONIC NONEQUILIBRIUM FLOW IMPLEMENTED IN DSMC-PHOTON MONTE CARLO RADIATION .................................................................................................................................7126

Ilyoup Sohn, Zheng Li, Deborah Levin

DEVELOPMENT OF A HYBRID DSMC/NAVIER-STOKES SOLVER WITH APPLICATION TO THE STS-119 BOUNDARY LAYER TRANSITION FLIGHT EXPERIMENTS .................................................................................................7149

K. Stephani, D. Goldstein, P. Varghese

SENSITIVITY ANALYSIS FOR DSMC SIMULATIONS OF HIGH-TEMPERATURE AIR CHEMISTRY ...............................7170J. Strand, D. Goldstein

CHALLENGES OF MODELING OF ELECTRONIC STATE SPECIFIC PROCESSES FOR HYPERSONIC REENTRY FLOWS IN DSMC...................................................................................................................................................................7188

Z. Li, T. Ozawa, I. Sohn, D. Levin

PURDUE STUDENT EXPERIMENT AND EDUCATION IN VARIOUS LOW-GRAVITY FLIGHT METHODS .....................7214Steven Collicott

INVISCID ANALYSIS OF HORIZONTAL-AXIS WIND TURBINES USING DISTRIBUTED VORTICITY ELEMENTS ..................................................................................................................................................................................................7226

Blair Basom, Mark Maughmer

A CORRECTED BLADE ELEMENT MOMENTUM METHOD FOR SIMULATING WIND TURBINES IN YAWED FLOW............................................................................................................................................................................................7247

M. McWilliam, S. Lawton, S. Cline, C. Crawford

A DETAILED AERODYNAMIC DESIGN AND ANALYSIS OF A 2-D VERTICAL AXIS WIND TURBINE USING SLIDING MESH IN CFD ..............................................................................................................................................................7257

Naveed Durrani, Haris Hameed, Hammad Rahman, Sajid Chaudhry

INDICIAL RESPONSE FUNCTION FOR FINITE-THICKNESS AIRFOILS, A SEMI-EMPIRICAL APPROACH..................................................................................................................................................................................................7273

Mac Gaunaa, Leonardo Bergami, Joachim Heinz

PREDICTION OF STEADY AERODYNAMIC PERFORMANCE OF ROTORS WITH WINGLETS USING SIMPLE PRESCRIBED WAKE METHODS ..........................................................................................................................................7284

Mac Gaunaa, Niels Sorensen, Mads Dossing

VOLUME 9

WIND TURBINE PERFORMANCE ANALYSIS UNDER UNCERTAINTY.....................................................................................7296

G. Petrone, C. De Nicola, D. Quagliarella, J. Witteveen, G. Iaccarino

DESIGN OF AN AIR AMBULANCE AIRCRAFT FOR THE AUSTRALIAN ENVIRONMENT ..................................................7314Allison Adorni-Braccesi, Cees Bil

TECHNICAL CONSTRAINTS FOR A LOW-COST FEMTO-SATELLITE LAUNCHER .............................................................7328R. Jove-Casulleras, J. Tristancho, C. Vera-Flores

CONCEPTUAL SIZING OF REGIONAL TRANSPORT AIRCRAFT FOR INDIA.........................................................................7346Darwin Rajpal, Rajkumar Pant

A “TOLERANT” WING DESIGN FOR UCAV ......................................................................................................................................7354R. Nangia, M. Palmer

DESIGN, FABRICATION, AND TESTING OF AN INSECT-SIZED MAV WING FLAPPING MECHANISM .........................7367M. Anderson, N. Sladek, R. Cobb

A SOFTWARE SUITE FOR CONCEPTUAL DESIGN OF FLAPPING WING MAVS ...................................................................7378Etan Karni, Michael Johnson, Brandon Stiltner, Kevin Fogleman, Paul Gelhausen, David Willis, Rick Lind, Mayuresh Patil

FIGURE-8 FLAPPING MICRO AIR VEHICLE ....................................................................................................................................7389Jaderic Dawson, P. Huang

AERODYNAMIC SENSING AS FEEDBACK FOR ORNITHOPTER FLIGHT CONTROL .........................................................7401Derrick Yeo, Ella Atkins, Wei Shyy

DESIGN AND ANALYSIS OF A BIO-INSPIRED WARPING TAIL FOR MAV APPLICATIONS...............................................7416Z. Votaw, Z. Gaston, A. Brezina, H. Dong, A. Benthara

NORTH AMERICAN AEROSPACE PROJECT-ADAPTABLE DESIGN/BUILD PROJECTS FOR AEROSPACE EDUCATION ......................................................................................................................................................................7428

E. Crawley, R. Niewoehner, P. Gray, J. Koster

AEROSPACE ENGINEERING IN THE CLASSROOM: THE PROJECT LEAD THE WAY MODEL........................................7436G. Holt, D. Hughes

A NEW REALIZABLE SUBGRID-SCALE STRESS MODEL FOR LARGE EDDY SIMULATION OF NEUTRAL ATMOSPHERIC BOUNDARY LAYER..............................................................................................................................7445

Harish Gopalan, Stefan Heinz

NUMERICAL INVESTIGATION OF DIFFERENT WIND TURBINE AIRFOILS..........................................................................7455Andreas Gross, Hermann Fasel

DRAG REDUCTION USING RIBLET FILM APPLIED TO AIRFOILS FOR WIND TURBINES ...............................................7470Agrim Sareen, Robert Deters, Steven Henry, Michael Selig

EFFECT OF TURBULENCE LOADING ON A 2-D AEROFOIL........................................................................................................7489M. Mahmoodilari, K. Kontis, P. Stansby

POWER GENERATION FROM WIND TURBINES IN A SOLAR CHIMNEY................................................................................7500T. Foote, R. Agarwal

SECONDARY INSTABILITY OF ROUGHNESS WAKES AND OPTIMAL DISTURBANCES....................................................7513Nick Denissen, Edward White

NUMERICAL INVESTIGATIONS OF THE INFLUENCE OF DISTRIBUTED ROUGHNESS ON BLASIUS BOUNDARY LAYER STABILITY ...........................................................................................................................................................7533

Christoph Brehm, Clay Koevary, Tim Dackermann, Hermann Fasel

DIRECT NUMERICAL SIMULATIONS OF FLOW PAST RANDOM DISTRIBUTED ROUGHNESS ......................................7555S. Drews, R. Downs, C. Doolittle, D. Goldstein, E. White

HYPERSONIC TRANSITION TO TURBULENCE TRIGGERED BY ISOLATED ROUGHNESS ELEMENTS .......................7569Seokkwan Yoon, Michael Barnhardt, Emre Sozer, Graham Candler

ROUGHNESS-INDUCED TRANSITION IN HIGH SPEED FLOWS .................................................................................................7581Prahladh Iyer, Suman Muppidi, Krishnan Mahesh

NUMERICAL SIMULATIONS OF HYPERSONIC BOUNDARY-LAYER INSTABILITY WITH LOCALIZED ROUGHNESS ...............................................................................................................................................................................................7597

Olaf Marxen, Gianluca Iaccarino, Eric Shaqfeh

HIGH FIDELITY SIMULATIONS OF FLAPPING WINGS DESIGNED FOR ENERGETICALLY OPTIMAL FLIGHT.........................................................................................................................................................................................................7613

P. Persson, D. Willis

AERODYNAMIC FORCES ON FLEXIBLE FLAPPING WINGS ......................................................................................................7627Erik Sallstrom, Lawrence Ukeiley, Pin Wu, Peter Ifju

HIGH-FIDELITY AEROELASTIC COMPUTATIONS OF A FLAPPING WING WITH SPANWISE FLEXIBILITY ..............................................................................................................................................................................................7643

Raymond Gordnier, Satish Chimakurthi, Carlos Cesnik, Peter Attar

PIV STUDY OF FLOW FIELDS IN THE NEAR-WAKE REGION OF A FLAPPING WING MICRO AIR VEHICLE ......................................................................................................................................................................................................7669

H. Ren, Y. Wu, G. Huang, J. Evans

ON THE DETERMINATION OF PROPULSIVE CHARACTERISTICS OF A FLAPPING AIRFOIL WITH ADVANCED ALE METHOD.....................................................................................................................................................................7681

Jean-François Cori, Stéphane Étienne, Dominique Pelletier

GRID AND TIME STEP REQUIREMENTS TO ACCURATELY AND EFFICIENTLY RESOLVE FLOW AROUND A RIGID FLAPPING AIRFOIL USING OVERFLOW .......................................................................................................7697

J. Leffell, T. Pulliam

PARAMETRIC ANALYSIS OF EXPENDABLE TYPE SINGLE-SPOOL TURBOJET ENGINE WITH A SHORT AFTERBURNER...........................................................................................................................................................................7714

B. Haider, N. Davidovic, N. Durrani

PRELIMINARY DESIGN OF A SHORT AFTERBURNER FOR SINGLE-SPOOL EXPENDABLE TURBOJET ENGINE ........................................................................................................................................................................................................7728

B. Haider, N. Davidovic, N. Durrani

NUMERICAL INVESTIGATION OF AN AIR-AIR EJECTOR WITH DIFFUSER FOR USE IN GAS TURBINE EXHAUST SYSTEMS .................................................................................................................................................................................7739

David Cerantola, James Crawford, A. Birk

TIME-ACCURATE FLOW FIELD AND ROTOR SPEED MEASUREMENTS OF A PULSED DETONATION DRIVEN TURBINE .....................................................................................................................................................................................7749

K. Rouser, P. King, F. Schauer, R. Sondergaard, L. Goss, J. Hoke

AN IMPROVED METHODOLOGY FOR GAS TURBINE TECHNOLOGY PORTFOLIO PLANNING, INCLUDING TECHNOLOGY SYNERGY MATRICES AND REAL OPTIONS ANALYSIS ........................................................7765

Farooq Akram, Matthew Prior, Dimitri Mavris

HEAT TRANSFER EXPERIMENTS ON A PULSED DETONATION DRIVEN RADIAL TURBINE EXHAUST .....................7778Nicholas Longo, Paul King, Frederick Schauer, Rolf Sondergaard, John Hoke

THE ROTATING DETONATION-WAVE ENGINE CONCEPT: A BRIEF STATUS REPORT ...................................................7791K. Kailasanath

NUMERICAL STUDY OF THE EFFECTS OF ENGINE SIZE ON ROTATING DETONATION ENGINES .............................7799Douglas Schwer, Kailas Kailasanath

NUMERICAL STUDY ON DETONATION CHARACTERISTICS USING A BIO-FUEL ..............................................................7812T. Shimada, A. Hayashi, E. Yamada, N. Tsuboi

ANALYSIS OF DEFLAGRATIVE COMBUSTION IN A WAVE-ROTOR CONSTANT-VOLUME COMBUSTOR ..............................................................................................................................................................................................7823

Tarek Elharis, Sameera Wijeyakulasuriya, M. Nalim, Yu Matsutomi

NUMERICAL ANALYSIS OF A PULSE DETONATION CROSS FLOW HEAT LOAD EXPERIMENT ...................................7837Daniel Paxson, Andrew Naples, John Hoke, Fred Schauer

DETONATION PROPAGATION THROUGH DUCTS IN A PULSED DETONATION ENGINE.................................................7849Jeffrey Nielsen, Chris Stevens, Paul King, Fred Schauer, John Hoke

DETONATION INITIATION BY A GRADIENT MECHANISM IN PROPANE–OXYGEN AND PROPANE–AIR MIXTURES ..........................................................................................................................................................................................7862

Aleksandr Rakitin, Ilia Popov, Andrei Starikovskii

A COMPARISON OF FLUIDIC AND PHYSICAL OBSTACLES FOR DEFLAGRATION-TO-DETONATION TRANSITION ...............................................................................................................................................................................................7867

B. Knox, D. Forliti, C. Stevens, J. Hoke, F. Schauer

BALL VALVE PULSED DETONATION ENGINE................................................................................................................................7876E. Anderson, C. Stevens, J. Hoke, F. Schauer

DEPENDENCE OF THE BLUFF BODY WAKE STRUCTURE ON FLAME TEMPERATURE RATIO ....................................7884B. Emerson, J. Lundrigan, J. O'Connor, D. Noble, T. Lieuwen

THE INFLUENCE OF STOICHIOMETRY AND FLAME-HOLDER SHAPE ON FLAME DYNAMICS AND ACOUSTICS .................................................................................................................................................................................................7898

Barry Kiel, Amy Lynch, Stanislav Kostka, Bethany Huelskamp, Reza Kashani, Nick Parr

CHARACTERIZATION OF BLUFF-BODY-FLAME VORTEX SHEDDING USING PROPER ORTHOGONAL DECOMPOSITION .....................................................................................................................................................................................7916

S. Kostka, S. Roy, B. Huelskamp, A. Lynch, B. Kiel, J. Gord

DYNAMICS OF A TRANSVERSELY FORCED, BLUFF BODY STABILIZED FLAME...............................................................7923B. Emerson, U. Mondragon, C. Brown, V. Acharya, D. Shin, V. McDonell, T. Lieuwen

INTERFERENCE EFFECTS IN CONTROLLING FLAME RESPONSE TO HARMONIC FLOW PERTURBATIONS......................................................................................................................................................................................7937

D. Shin, M. Romani, T. Lieuwen

BUILDUP AND OPERATION OF A ROTATING DETONATION ENGINE ....................................................................................7948Levi Thomas, Frederick Schauer, John Hoke, Andrew Naples

COMBUSTION OF ALUMINUM, ALUMINUM HYDRIDE, AND ICE MIXTURES......................................................................7958Dilip S. Sundaram, Vigor Yang, Terrence Connell, Grant Risha, Richard Yetter, Gregory Young

AN EXPERIMENTAL INVESTIGATION OF THE AUTOIGNITION CHARACTERISTICS OF CAMELINA-BASED HYDROPROCESSED RENEWABLE JET FUEL ...................................................................................................................7968

Casey Allen, Elisa Toulson, Tonghun Lee

BURNING RATES OF NANO-ALUMINUM/ FC-2175/ NICKEL OXIDE COMPOSITES AS A FUNCTION OF DOPING, PRESSURE AND MAGNETIC FIELD ..................................................................................................................................7976

P. Seshadri, B. Mason, S. Son, L. Groven, A. Gash

THERMO-MECHANICAL BEHAVIOR OF NICKEL-COATED NANO-ALUMINUM PARTICLES .........................................7987D. Sundaram, V. Yang, P. Puri

MODELING CONSTELLATION VIRTUAL MISSIONS USING THE VDOTTM PROCESS MANAGEMENT TOOL.............................................................................................................................................................................................................8000

R. Herdy, D. O'Neil, I. Sturken, M. Nix, D. Yanez

HYDROGEN REDUCTION OF LUNAR REGOLITH SIMULANTS FOR OXYGEN PRODUCTION ........................................8009Uday Hegde, Ramaswamy Balasubramaniam, Suleyman Gokoglu, Kathleen Rogers, Michael Reddington, Lara Oryshchyn

MEASUREMENT OF APPARENT THERMAL CONDUCTIVITY OF JSC-1A UNDER AMBIENT PRESSURE.....................8019Zeng-Guang Yuan, Julie Kleinhenz

INVESTIGATION OF HEAT RECUPERATION IN A CONCENTRIC HYDROGEN REDUCTION REACTOR .....................8031Diane Linne, Julie Kleinhenz, Uday Hegde, Daniel Gotti

PRESSURE CONTROLLED HEAT PIPE SOLAR RECEIVER FOR REGOLITH OXYGEN PRODUCTION WITH MULTIPLE REACTORS ...............................................................................................................................................................8046

J. Hartenstine, K. Walker, C. Tarau, W. Anderson

MICROWAVE PROCESSING OF PLANETARY SURFACES FOR THE EXTRACTION OF VOLATILES ............................8060Edwin Etheridge, William Kaukler

COMBUSTIBLE MIXTURES OF LUNAR REGOLITH WITH ALUMINUM AND MAGNESIUM: THERMODYNAMIC ANALYSIS AND COMBUSTION EXPERIMENTS .......................................................................................8073

Christopher White, Francisco Alvarez, Evgeny Shafirovich

SOME USEFUL STRATEGIES FOR UNSTRUCTURED EDGE-BASED SOLVERS ON SHARED MEMORY MACHINES ..................................................................................................................................................................................................8084

R. Aubry, G. Houzeaux, M. Vazquez

A SCIENTIFIC SOFTWARE VERIFICATION LIBRARY BASED ON THE METHOD OF MANUFACTURED SOLUTIONS .................................................................................................................................................................................................8110

David Marshall

DESIGN OF VEHICLE MANAGEMENT SOFTWARE FOR HIGH ALTITUDE AIRSHIP BASED ON VXWORKS ...................................................................................................................................................................................................8123

Guangtai Jiang, Ming Zhu, Zewei Zheng

EVOLUTION MAP MODEL FOR ORGANIZING INFORMATION AT AIRCRAFT CONCEPTUAL DESIGN PHASE ...........................................................................................................................................................................................................8130

Hu Liu, Yong Liang Tian, Ming Qiang Luo, Peng Lu, Zhe Wu

COMBUSTION CHARACTERISTICS OF SPRAY FLAMES OF SOY METHYL ESTER AND DIESEL BLENDS ........................................................................................................................................................................................................8140

C. Aldana, S. Gollahalli, R. Parthasarathy

PERFORMANCE AND EMISSION CHARACTERISTICS OF ALCOHOL/JET A BLENDS IN A SMALL-SCALE GAS TURBINE ENGINE .............................................................................................................................................................8151

Carlos Mendez, Ramkumar Parthasarathy, Subramanyam Gollahalli

AN EXPERIMENTAL INVESTIGATION OF COMBUSTION INDUCED VORTEX BREAKDOWN FLASHBACK IN A SWIRL STABILIZED BURNER............................................................................................................................8163

B. Dam, G. Corona, M. Hayder, A. Choudhuri

AN INVESTIGATION OF LEAN LIMITS OF HYDROGEN FLAME AT MESO-SCALE.............................................................8177Mahbub Ahmed, Ahsan Choudhuri, Vivek Shirsat, Mosfequr Rahman

ON THE MODELING OF FLOW REGIMES DOWNSTREAM OF FLAME HOLDERS IN COMBUSTION CHAMBERS .................................................................................................................................................................................................8184

Essam Khalil

HYDROGEN ADDITION EFFECTS ON METHANE-AIR COLORLESS DISTRIBUTED COMBUSTION FLAMES........................................................................................................................................................................................................8193

V. Arghode, A. Gupta

VOLUME 10

PROBABILISTIC MODELS AND UNCERTAINTY QUANTIFICATION FOR THE IONIZATION REACTION RATE OF ATOMIC NITROGEN..............................................................................................................................................................8207

Kenji Miki, Marco Panesi, Ernesto Prudencio, S. Prudhomme

DEVELOPMENT OF A PARTICLE-PARTICLE HYBRID SCHEME BASED ON ESBGK AND DSMC METHODS TO SIMULATE MULTI-SCALE TRANSITIONAL FLOWS .........................................................................................8225

Rakesh Kumar, Evgeny Titov, Deborah Levin

EXPERIMENTAL CHARACTERIZATION OF THE LENS EXPANSION TUNNEL FACILITY INCLUDING BLUNT BODY SURFACE HEATING......................................................................................................................................................8267

A. Dufrene, M. Maclean, R. Parker, M. Holden

MOLECULAR DYNAMICS ANALYSIS OF SURFACE CATALYSIS IN HIGH-TEMPERATURE GAS...................................8276Shinya Kudo, Yohei Suzuki, Naofumi Ohnishi

EVALUATING THE EFFECT ON COMPONENT COOLING AND THERMALLY GENERATED STRESS CAUSED BY VARIATION OF INTERNAL HEAT TRANSFER COEFFICIENTS THROUGH AN UNCERTAINTY QUANTIFICATION .....................................................................................................................................................8292

Jan Marsh, Jayanta Kapat

NUMERICAL AND EXPERIMENTAL STUDY OF FILM COOLING EFFECTIVENESS AND TOTAL PRESSURE LOSS FOR A REALISTIC CASCADE WITH AN ANNULAR ENDWALL ................................................................8305

T. Casey, C. Nguyen, J. Kullberg, M. Ricklick, J. Kapat

A NOVEL CARTESIAN IMPLEMENTATION OF THE DIRECT SIMULATION MONTE CARLO METHOD ......................8319J. Burt, E. Josyula, I. Boyd

A PARALLEL DSMC IMPLEMENTATION INCLUDING ADAPATIVE MESH REFINEMENT AND CUT-CELL ALGORITHMS ................................................................................................................................................................................8341

Da Gao, Thomas Schwartzentruber

RESONANT VIBRATIONS RESULTING FROM THE RE-ENGINEERING OF A CONSTANT-SPEED 2-BLADED TURBINE TO A VARIABLE-SPEED 3-BLADED TURBINE ............................................................................................8350

Paul Fleming, Alan Wright, Lee Fingersh, Jan-Willem Van Wingerden

SPACE-TIME LOADINGS ON WIND TURBINE BLADES DRIVEN BY ATMOSPHERIC BOUNDARY LAYER TURBULENCE .............................................................................................................................................................................8364

A. Lavely, G. Vijayakumar, M. Kinzel, J. Brasseur, E. Paterson

DESIGN, FABRICATION, ASSEMBLY AND INITIAL TESTING OF A SMART ROTOR ..........................................................8388D. Berg, J. Berg, J. White, B. Resor, M. Rumsey

PASSIVE CAMBER CHANGE FOR WINDTURBINE LOAD ALLEVIATION ...............................................................................8399B. Lambie, M. Jain, C. Tropea, G. Spelsberg-Korspeter

PERFORMANCE CHARACTERIZATION OF CYCLIC BLADE PITCH VARIATION ON A VERTICAL AXIS WIND TURBINE..........................................................................................................................................................................................8408

David Erickson, Jason Wallace, Jaime Peraire

NON PLANAR SPAN LOADS FOR MINIMUM INDUCED DRAG ...................................................................................................8431T. Takahashi, S. Donovan

A BOTTOM-UP APPROACH TO VEHICLE CONFIGURATION SPACE EXPLORATION AROUND UNCONVENTIONAL TECHNOLOGIES ...............................................................................................................................................8445

Davis Balaba, Dimitri Mavris

A TANK HEATING MODEL FOR AIRCRAFT FUEL THERMAL SYSTEMS WITH RECIRCULATION ...............................8474Brian German

PRELIMINARY AERODYNAMIC SHAPE OPTIMIZATION OF A BLENDED-WING-BODY AIRCRAFT CONFIGURATION .....................................................................................................................................................................................8483

Nimeesha Kuntawala, Jason Hicken, David Zingg

AN EMPIRICAL APPROACH TOWARDS THE RAPID DERIVATION OF VEHICLE SCALING LAWS IN CONCEPTUAL DESIGN............................................................................................................................................................................8498

Davis Balaba, Dimitri Mavris

ALUMINUM COMBUSTION IN ALUMINIZED EXPLOSIVES: AEROBIC AND ANAEROBIC REACTION ........................8510H. Krier, J. Peuker, N. Glumac

REFLECTED SHOCK BIFURCATION IN A SQUARE CHANNEL ..................................................................................................8516Alexei Khokhlov, Joanna Austin, Charles Bacon, Shashi Aithal, Katherine Riley

SHOCK WAVE INTERACTION WITH MICROSTRUCTURES AND HETEROGENEOUS MEDIA.........................................8526Anil Kapahi, Shivkumar Sambasivam, Uday Kumar

THREE-DIMENSIONAL PARALLEL COMPRESSIBLE MULTI-MATERIAL FLOWS..............................................................8547A. Kapahi, J. Mousel, S. Sambasivam, U. Kumar

DIRECT NUMERICAL SIMULATIONS OF TURBULENT FLOW INTERACTIONS WITH STRONG SHOCKS USING SHOCK-FITTING METHOD ....................................................................................................................................8577

Pradeep Rawat, Xiaolin Zhong

SIMULATIONS OF HIGH SPEED TURBULENT JETS IN CROSSFLOWS....................................................................................8627Xiaochuan Chai, Krishnan Mahesh

A CONSERVATIVE MESHLESS SCHEME: GENERAL ORDER FORMULATION AND APPLICATION TO EULER EQUATIONS .................................................................................................................................................................................8640

E. Chiu, Q. Wang, A. Jameson

MESH QUALITY EFFECTS ON THE ACCURACY OF CFD SOLUTIONS ON UNSTRUCTURED MESHES ........................8659Aaron Katz, Venkateswaran Sankaran

HARMONIC BALANCE METHODOLOGY FOR MESHLESS PARTICLE-BASED METHODS ...............................................8683Ramji Kamakoti, Liping Xue, Patrick Hu, Peter Attar, Prakash Vedula

A MESHLESS FINITE DIFFERENCE SCHEME FOR COMPRESSIBLE POTENTIAL FLOWS ...............................................8699Alejandro Ramos, Robert McDonald

CONSTRAINED HERMITE TLS FOR MESH-FREE DERIVATIVE ESTIMATION NEAR AND ON BOUNDARIES .............................................................................................................................................................................................8715

Robert McDonald, Alejandro Ramos

INITIAL INVESTIGATION OF A MESHLESS INTERFACE METHOD USING RADIAL BASIS FUNCTIONS.....................8730William Costin, Christian Allen

ANALYSIS AND CORRECTION OF ERRORS GENERATED BY SLOWLY MOVING SHOCKS.............................................8745E. Johnsen, S. Lele, J. Larsson

CONDITIONAL SAMPLING AND EXPERIMENT DESIGN FOR QUANTIFYING MANUFACTURING ERROR OF TRANSONIC AIRFOIL........................................................................................................................................................8757

Q. Wang, H. Chen, R. Hu, P. Constantine

DEVELOPMENT AND IMPLEMENTATION OF A PROBABILISTIC DESIGN APPROACH TO MODEL THE VARIATION OF INTERNAL HEAT TRANSFER COEFFICIENTS AS PART OF AN UNCERTAINTY QUANTIFICATION ....................................................................................................................................................................................8774

Jan Marsh, Jayanta Kapat

UNCERTAINTY QUANTIFICATION FOR LAMINAR-TURBULENT TRANSITION PREDICTION IN RANS TURBOMACHINERY APPLICATIONS.................................................................................................................................................8787

R. Pecnik, J. Witteveen, G. Iaccarino

HELICOPTER BVI NOISE REDUCTION USING SYNTHETIC JETS: NUMERICAL STUDIES USING LES ........................8801C. Velez, P. Coronado, H. Al-Kuran, A. Deperta, M. Ilie

DES STUDY OF BASE AND BASE-BLEED FLOWS WITH DYNAMIC FORMULATION OF DES CONSTANT ...................8813Jae-Ryul Shin, Jeongyeol Choi

A REYNOLDS STRESS RELAXATION TURBULENCE MODEL APPLIED TO A WINGTIP VORTEX FLOW....................8823Matthew Churchfield, Gregory Blaisdell

VERIFICATION OF A FREE SURFACE ADAPTIVE FINITE ELEMENT SOLUTION ALGORITHM ....................................8848Lise Charlot, Stéphane Étienne, Dominique Pelletier

A DISCRETE VORTEX METHOD INVESTIGATION OF CANONICAL PITCH RAMP-HOLD CASE....................................8861P. Hammer, A. Altman, F. Eastep

GRASP: A NEW OBJECT-ORIENTED SERIAL DSMC SIMULATION PACKAGE .....................................................................8877H. Liu, C. Cai, S. Makala

LOW-DIMENSIONAL TOOL FOR PREDICTING FORCE COEFFICIENTS ON A CIRCULAR CYLINDER ........................8887Mehdi Ghommem, Imran Akhtar, Arshad Mehmood, Muhammad Hajj

UNSTEADY COMPRESSIBLE FLOW ON A NACA 0021 AIRFOIL.................................................................................................8895C. Jensen, K. Gompertz, D. Peng, T. Juliano, P. Kumar, J. Gregory, J. Bons

WIND EFFECT ON VIBRATION AND SCATTERING BEHAVIOR OF JAPANESE SLATE .....................................................8912Satoru Okamoto

UNSTEADY FLOW ANALYSIS IN A FIRED BRIGGS-STRATTON INTERNAL COMBUSTION ENGINE ............................8920M. Drabo, J. Davis, S. Olcmen, M. Ashford, P. Seers

LAGRANGIAN CONCENTRATION DIFFERENTIAL EQUATIONS FOR INTERPHASE MASS TRANSFER AND UNSTEADY FLOW ...........................................................................................................................................................................8937

Jason Mickey, Eric Loth

MAXIMUM DEVIATION IN UNSTEADY FLOWS WITH EXPERIMENTAL COMPARISONS ................................................8964K. Bergeron, N. Carter, O. Boelens, R. Cummings, R. Decker

NUMERICAL SIMULATION OF VORTEX RING INTERACTIONS WITH SOLID WALL .......................................................8974Debojyoti Ghosh, James Baeder

NUMERICAL, EXPERIMENTAL AND THEORETICAL STUDIES ON MECHANISM OF K-H INSTABILITY AND RING GENERATION BEHIND SUPERSONIC MVG.................................................................................................................8987

Y. Yan, Q. Li, C. Liu, F. La

MACH NUMBER EFFECTS ON VORTEX BREAKDOWN IN SUBSONIC FLOW OVER A DELTA WING ...........................8999Hiroaki Fukumoto, Yoshihiro Ishikawa, Taku Nonomura, Kozo Fujii

INTERACTION OF TIP VORTICES GENERATED BY TWO BLADED ROTOR COMPOSED OF DIFFERENT PITCH ANGLES IN A HOVER ........................................................................................................................................9013

Y. Han, B. Park, Y. Sohn

COMPUTATIONAL ANALYSIS OF A WINGTIP VORTEX IN THE NEAR-FIELD USING LBM-VLES APPROACH..................................................................................................................................................................................................9025

Rajani Satti, Yanbing Li, Richard Shock, Brad Duncan

RESPONSE OF A HYPERSONIC TURBULENT BOUNDARY LAYER TO LOCAL AND GLOBAL MECHANICAL DISTORTIONS ...............................................................................................................................................................9037

Scott Peltier, Ray Humble, Rodney Bowersox

DETERMINING THE EFFECT OF DIMPLES ON DRAG IN A TURBULENT CHANNEL FLOW ............................................9050C. Tay

TURBULENT BOUNDARY LAYERS OVER COARSE SCALE RESOLUTION APPROXIMATIONS OF A ROUGH FORWARD-FACING STEP ......................................................................................................................................................9062

H. Ren, Y. Wu

HIGH-ORDER LES SIMULATIONS USING IMPLICIT-EXPLICIT RUNGE-KUTTA SCHEMES ............................................9088Per-Olof Persson

A DIAGONALLY IMPLICIT RUNGE-KUTTA METHOD FOR THE DISCONTINUOUS GALERKIN SOLUTIONS OF THE NAVIER-STOKES EQUATIONS .....................................................................................................................9098

H. Segawa, H. Luo, R. Nourgaliev

VOLUME 11

APPLICATION OF HIGH-ORDER ENERGY STABLE FLUX RECONSTRUCTION SCHEMES TO THE EULER EQUATIONS .................................................................................................................................................................................9121

Patrice Castonguay, Peter Vincent, Antony Jameson

GPU-ACCELERATED SPARSE MATRIX-VECTOR PRODUCT FOR A HYBRIDIZABLE DISCONTINUOUS GALERKIN METHOD ...............................................................................................................................................................................9152

Xevi Roca, Ngoc Cuong Nguyen, Jaime Peraire

DIODE LASER ABSORPTION SPECTROSCOPY MEASUREMENTS IN A GASEOUS HYDROGEN / OXYGEN ROCKET ....................................................................................................................................................................................9164

Justin Locke, Sibtosh Pal, Roger Woodward, Robert Santoro

IN SITU CO2 CONCENTRATION MEASUREMENT INSIDE A COMBUSTION CHAMBER USING INFRARED LASER ABSORPTION TECHNIQUE ...............................................................................................................................9184

Nobuyuki Kawahara, Eiji Tomita

INFRARED IMAGING, COMPUTATIONS, AND TOMOGRAPHY OF BLUFF BODY STABILIZED LAMINAR DIFFUSION FLAMES............................................................................................................................................................9195

B. Rankin, D. Blunck, V. Katta, S. Stouffer, J. Gore

INVESTIGATING THE PERFORMANCE OF NOVEL ENERGETIC MATERIALS USING OPTICAL DIAGNOSTICS ............................................................................................................................................................................................9207

B. Halls, C. Moody, J. Miller, M. Slipchenko, T. Meyer, J. Stauffer, S. Roy, W. Lewis, C. Bunker, R. Gord

TIME RESOLVED PARTICLE IMAGE VELOCIMETRY INVESTIGATIONS WITHIN A SECTIONAL ULTRA COMPACT COMBUSTOR .........................................................................................................................................................9217

K. Lebay, M. Polanka, M. Reeder, R. Branam

THERMAL STABILITY TESTING OF A FISCHER-TROPSCH FUEL AND VARIOUS BLENDS WITH JET A ....................9229J. Klettlinger, C. Yen, A. Surgenor

PRELIMINARY CHARACTERIZATION OF BIO-FUELS USING A SMALL SCALE GAS TURBINE ENGINE....................9241J. Baranski, J. Hoke, P. Litke, F. Schauer

THE PERFORMANCE AND EMISSIONS EFFECTS OF UTILIZING HEAVY FUELS AND BIODIESEL IN A SMALL SPARK IGNITION INTERNAL COMBUSTION ENGINE ..................................................................................................9251

J. Groenewegen, P. Litke, C. Wilson, S. Sidhu, J. Hoke

IGNITION DELAY TIMES OF A RANGE OF ALTERNATE JET-FUELS AND SURROGATE FUEL CANDIDATE HYDROCARBONS UNDER FUEL-LEAN CONDITIONS: A SHOCK TUBE STUDY ..........................................9261

J. Balagurunathan, Giacomo Flora, Saumitra Saxena, Moshan Kahandawala, Matthew Dewitt, Sukh Sidhu, Edwin Corporan

MEASUREMENTS OF EXTINCTION LIMITS OF METHYL DECANOATE DIFFUSION FLAMES AND A KINETIC STUDY ........................................................................................................................................................................................9273

Pascal Dievart, Sang Hee Won, Mruthunjaya Uddi, Stephen Dooley, Frederick Dryer, Yiguang Ju

CHEMICAL KINETIC STUDY OF THE ALTERNATIVE TRANSPORT FUEL, TERTIARY-BUTANOL ...............................9286J. Lefkowitz, J. Heyne, S. Won, S. Dooley, H. Kim, F. Haas, S. Jahangirian, F. Dryer, Y. Ju

COMPARISON OF DIRECT SOLAR ENERGY TO RESISTANCE HEATING FOR CARBOTHERMAL REDUCTION OF REGOLITH ..................................................................................................................................................................9298

Anthony Muscatello, Robert Gustafson

MULTIPHYSICS MODELING FOR DIMENSIONAL ANALYSIS OF A SELF-HEATED MOLTEN REGOLITH ELECTROLYSIS REACTOR FOR OXYGEN AND METALS PRODUCTION FROM SPACE RESOURCES................................................................................................................................................................................................9308

J. Dominguez, L. Sibille

CALCIUM REDUCTION AS A PROCESS FOR OXYGEN PRODUCTION FROM LUNAR REGOLITH.................................9316Geoffrey Landis

GREEN AEROSPACE FUELS FROM NON-PETROLEUM SOURCES ...........................................................................................9322A. Hepp, M. Kulis, A. De La Ree, R. Zubrin, M. Beggren, J. Hensel, M. Kimble

ENABLING LONG-DURATION LUNAR EQUATORIAL OPERATIONS WITH THERMAL WADI INFRASTRUCTURE...................................................................................................................................................................................9343

Heather Jones, John Thornton, Ramaswamy Balasubramaniam, Suleyman Gokoglu, Kurt Sacksteder, William Whittaker

THERMAL ENERGY PROCESS HEAT FOR LUNAR ISRU: TECHNICAL CHALLENGES AND TECHNOLOGY OPPORTUNITIES.........................................................................................................................................................9356

P. Gordon, A. Colozza, A. Hepp, R. Heller, R. Gustafson, T. Stern, T. Nakamura

SIMULATION OF AN INTEGRATED LEAN-DIRECT INJECTION COMBUSTOR AND A STAGE OF STATOR-ROTOR TURBINE ....................................................................................................................................................................9378

Changju Wey, Nan-Suey Liu

ON THE COMPUTATIONS OF FILM COOLING IN GAS TURBINE BLADES ............................................................................9393A. Adawy, S. Morkos, E. Khalil

COMPUTATIONAL STUDY OF HEAT TRANSFER DISTRIBUTION IN A SQUARE CHANNEL WITH RIB TURBULATORS AND BLEED HOLES ..................................................................................................................................................9402

Ryoichi Amano, Jose Martinez Lucci, Sourabh Kumar, Krishna Guntur

TOWARDS EFFICIENT CFD-SIMULATIONS OF ENGINE LIKE TURBINE GUIDE VANE FILM COOLING ....................9412A. Bradley, H. Nadali Najafabadi, M. Karlsson, J. Wren, E. Utriainen, M. Kinell

CFD SIMULATIONS USING REDUCED MODELS FOR FILM COOLING DESIGN ...................................................................9432H. Nadali Najafabadi, A. Bradley, J. Wren, M. Karlsson, E. Utriainen, M. Kinell

INVESTIGATION ON THE CHARACTERISTICS OF PLUME INDUCED FLOW SEPARATION AND WALL HEAT TRANFER ........................................................................................................................................................................................9444

J. Kim, J. Lee, J. Choi, K. Kim

ANALYSIS OF FILM COOLING AND HEAT TRANSFER IN ROCKET THRUST CHAMBER AND NOZZLE .....................9456Alexander Miranda, Mohammad Naraghi

COMPARISON OF PLIF AND CFD RESULTS FOR THE ORION CEV RCS JETS ......................................................................9470C. Ivey, P. Danehy, B. Bathel, A. Dyakonov, J. Inman, S. Jones

SHOCK-FRONT EMISSION MEASUREMENTS AT 10 KM/S...........................................................................................................9491R. Parker, A. Dufrene, M. Holden, T. Wakeman

TRAJECTORY, DEVELOPMENT, AND TEMPERATURE OF SPARK KERNELS EXITING INTO QUIESCENT AIR ........................................................................................................................................................................................9502

D. Blunck, B. Kiel

IMPROVEMENTS IN SCANNING INFRARED THERMOGRAPHY ...............................................................................................9511Chris Dalton, Feng Lai

EFFECT OF ACTUATOR DYNAMICS ON ACTIVE STRUCTURAL CONTROL OF OFFSHORE WIND TURBINES....................................................................................................................................................................................................9523

Gordon Stewart, Matthew Lackner

OFFSHORE FLOATING WIND TURBINES - AN AERODYNAMIC PERSPECTIVE ..................................................................9539Thomas Sebastian, Matthew Lackner

AERO-HYDRO-ELASTIC RESPONSE OF A FLOATING PLATFORM SUPPORTING SEVERAL WIND TURBINES....................................................................................................................................................................................................9566

B. Kallesoe, U. Paulson, A. Køhler, H. Hansen

EVALUATION OF VARIOUS BEAMFORMING ALGORITHMS FOR WIND TURBINE NOISE MEASUREMENT ........................................................................................................................................................................................9575

R. Ramachandran, G. Raman

A COMPREHENSIVE NUMERICAL STUDY OF AERODYNAMICS AND AEROACOUSTICS OF WIND TURBINE BLADE CONFIGURATIONS.................................................................................................................................................9586

Krishna Velliyur Ramachandran, Zachary Webster, Mei Zhuang

DNS OF UNSTEADY SHOCK BOUNDARY LAYER INTERACTION .............................................................................................9597Suman Muppidi, Krishnan Mahesh

LOW-FREQUENCY UNSTEADINESS IN DSN OF SHOCK WAVE/TURBULENT BOUNDARY LAYER INTERACTION ...........................................................................................................................................................................................9615

S. Priebe, M. Martin

SIMULATIONS OF A MACH 3 COMPRESSION-RAMP INTERACTION USING LES/RANS MODELS.................................9635Daniel Gieseking, Jack Edwards

NUMERICAL STUDY OF SHOCK-BOUNDARY LAYER INTERACTIONS FOR VARIOUS SHOCK AND FLOW CONDITIONS .................................................................................................................................................................................9662

Avinash Jammalamadaka, Zhaorui Li, Farhad Jaberi

ZONES OF INFLUENCE AND SHOCK MOTION IN A SHOCK BOUNDARY LAYER INTERACTION .................................9673Lionel Agostini, Lionel Larchevêque, Pierre Dupont, Jean-François Debiève, Jean-Paul Dussauge

DNS OF A SPATIALLY EVOLVING TRANSITIONAL/TURBULENT BOUNDARY LAYER WITH IMPINGING SHOCK WAVE ....................................................................................................................................................................9686

Yusuke Tokura, Hiroshi Maekawa

THREE-DIMENSIONAL FLOW STRUCTURES AT SUPERSONIC FLOW OVER THE COMPRESSION RAMP ............................................................................................................................................................................................................9702

I. Egorov, V. Neiland, V. Shredchenko

TWO-DIMENSIONAL INTERACTION OF THE OBLIQUE SHOCK WAVE WITH THE BOUNDARY AND HIGH-ENTROPY LAYERS OF THE BLUNT PLATE .........................................................................................................................9720

I. Egorov, I. Stuminskaya, A. Skuratov, I. Struminskaya

LOCAL HEAT TRANFSER CHARACTERISTICS OF A MULTI WALL COOLING SCHEME AT TALL IMPINGEMENT HEIGHTS USING TEMPERATURE SENSITIVE PAINT ....................................................................................9420

Roberto Claretti, Mark Ricklick, Jay Kapat

GEOMETRY EFFECTS OF DIELECTRIC BARRIER DISCHARGE ON A FLAT SURFACE ....................................................9748Chin-Cheng Wang, Subrata Roy

ACTIVE FLOW CONTROL STRATEGY OF LAMINAR SEPARATION BUBBLES DEVELOPED OVER SUBSONIC AIRFOILS AT LOW REYNOLDS NUMBERS .................................................................................................................9758

Justin Aholt, Fathi Finaish

FLOW AND THERMAL PROPERTIES INDUCED BY ELECTRIC ARC PLASMA ACTUATORS ...........................................9772Bradley Deblauw, Eli Lazar, Nachiket Kale, Nick Glumac, Craig Dutton, Greg Elliott

EFFECT OF PLASMA-BASED CONTROL FOR LOW-REYNOLDS NUMBER FLAPPING AIRFOIL PERFORMANCE.........................................................................................................................................................................................9788

Donald Rizzetta, Miguel Visbal

EFFECT OF SURFACE ROUGHNESS ON LAMINAR SEPARATION BUBBLE OVER A WING AT A LOW-REYNOLDS NUMBER ...............................................................................................................................................................................9816

Ying Zhou, Z. Wang

NUMERICAL INVESTIGATION OF SHOCK-WAVE/BOUNDARY-LAYER INTERACTION CONTROL USING PLASMA ACTUATORS ...............................................................................................................................................................9834

Michael Atkinson, Jonathan Poggie, José Camberos

EFFECTIVE THREE-DIMENSIONAL LAYOUT OF IMAGINARY BODY FORCE FOR SEPARATION CONTROL ....................................................................................................................................................................................................9848

Ittetsu Kaneda, Kengo Asada, Kozo Fujii

MOMENTUM TRANSFER IN MILLISECOND PERIODIC-PULSED DIELECTRIC-BARRIER-DISCHARGE PLASMA ACTUATOR ...............................................................................................................................................................................9863

Borui Zheng, Chao Gao, Yibin Li, Jianlei Wang, Feng Liu, Shijun Luo

LARGE EDDY SIMULATION OF TURBULENT TRANSPORT IN DISCRETE INJECTION FILM COOLING.....................9878Perry Johnson, Son Ho, Jayanta Kapat

DYNAMIC CHARACTERIZATION OF A CENTRIFUGAL COMPRESSOR WITH PORTED SHROUD ................................9906M. Gancedo, E. Guillou, R. Dimicco, E. Gutmark, A. Mohamed

SURGE INVESTIGATION IN A CENTRIFUGAL COMPRESSOR BY STEREOSCOPIC PIV ...................................................9920E. Guillou, M. Gancedo, R. Dimicco, E. Gutmark, A. Mohamed

EFFECT OF CIRCUMFERENTIAL GROOVES AND TIP RECESS ON STALL CHARACTERISTICS OF TRANSONIC AXIAL COMPRESSOR ROTOR .....................................................................................................................................9932

J. Khan, K. Parvez, S. Ahmad, A. Mushtaq

PARAMETRIC STUDY OF TIP INJECTION ON STABILITY OF TRANSONIC AXIAL FLOW COMPRESSOR ............................................................................................................................................................................................9942

Ammar Mushtaq, Khalid Parvez, Sijal Ahmad, Junaid Khan

PERFORMANCE OF THREE-DIMENSIONAL ANNULAR DIFFUSERS WITH VARYING DUMP GAP RATIOS .........................................................................................................................................................................................................9952

Bryan Bernier, Jason Dunn, Mark Ricklick, Jay Kapat

VERY-LARGE-SCALE COHERENT STRUCTURES IN THE WALL PRESSURE FIELD BENEATH A SUPERSONIC TURBULENT BOUNDARY LAYER.............................................................................................................................9964

Steven Beresh, John Henfling, Russell Spillers, Brian Pruett

WALL MODELED LARGE EDDY SIMULATION OF FLOW OVER A BACKWARD FACING STEP WITH SYNTHETIC INLET TURBULENCE ......................................................................................................................................................9979

Sunil Patil, Danesh Tafti

INFLUENCE OF FAVORABLE PRESSURE GRADIENTS ON A MACH 5.0 TURBULENT BOUNDARY LAYER ..........................................................................................................................................................................................................9994

N. Tichenor, R. Humble, R. Bowersox

STUDY OF TURBULENCE-RADIATION INTERACTION IN HYPERSONIC TURBULENT BOUNDARY LAYERS ......................................................................................................................................................................................................10010

L. Duan, A. Feldick, P. Martin, M. Modest, D. Levin

VOLUME 12

SIMULTANEOUS 3-D FLOW VISUALIZATION WITH 2-D PIV TO OBSERVE A TURBULENT BOUNDARY LAYER ........................................................................................................................................................................................................10026

Michael Melnick, Brian Thurow

TURBULENT PRESSURE SIGNATURE REDUCTION USING TURBULENT BOUNDARY LAYER SUCTION CONTROL ..................................................................................................................................................................................................10041

C. Dolder, M. Haberman, M. Villanueva, C. Tinney

SIMULATION OF TURBULENT CHANNEL FLOW USING A LINEAR AND NON LINEAR REALIZABLE UNIFIED RANS-LES MODEL ................................................................................................................................................................10060

H. Gopalan, S. Heinz, M. Stoellinger

DNS OF A LARGE-DOMAIN, MACH 3 TURBULENT BOUNDARY LAYER: TURBULENCE STRUCTURE ......................10071I. Beekman, S. Priebe, Y. Kan, M. Martin

LARGE-SCALE DISTRIBUTED COMPUTATION USING BUILDING-CUBE METHOD .........................................................10089Noriyoshi Ishikawa, Disuke Sasaki, Kazuhiro Nakahashi

A NORMAL RAY REFINEMENT TECHNIQUE FOR CARTESIAN-GRID BASED NAVIER-STOKES SOLVERS....................................................................................................................................................................................................10100

Stephen Ruffin, Mina Zaki, Vikram Kumar, Susheel Sekhar

WALL-LAYER MODELING FOR CARTESIAN GRID SOLVER USING AN OVERSET BOUNDARY LAYER ORTHOGONAL CURVILINEAR GRID ...............................................................................................................................................10137

Shanti Bhushan, Akira Hanaoka, Jianming Yang, Frederick Stern

OCTREE BASED 3-D UNSTRUCTURED GRID COARSENING AND MULTIGRID VISCOUS FLOW SOLUTIONS ...............................................................................................................................................................................................10157

Emel Mahmutyazicioglu, Ismail Hakki Tuncer, Mehmet Haluk Aksel

IMMERSED INTERFACE METHOD FOR SOLVING THE INCOMPRESSIBLE NAVIER-STOKES EQUATIONS WITH MOVING BOUNDARIES ...................................................................................................................................10167

Christoph Brehm, Hermann Fasel

THE IMMERSED BOUNDARY METHOD FOR WATER ENTRY SIMULATION ......................................................................10186S. McIntyre, M. Kinzel, S. Miller, E. Paterson, J. Lindau, R. Kunz

HEAT TRANSFER MEASUREMENTS TO EXAMINE SURFACE ROUGHNESS AND BLOWING EFFECTS IN HYPERSONIC FLOWS ......................................................................................................................................................................10200

M. Holden, E. Mundy, M. Maclean

RAREFIED COMPRESSIBLE TWO-DIMENSIONAL JET PLUME IMPINGEMENT ON A FLAT PLATE ..........................10219K. Al Khasawneh, C. Cai, H. Liu

UNCERTAINTY AND PARAMETER SENSITIVITY IN MULTIPHYSICS REENTRY FLOWS ..............................................10228R. Stogner, P. Bauman, K. Schulz, R. Upadhyay, A. Maurente

A COMPARATIVE STUDY OF NAVIER-STOKES AND DSMC SIMULATION OF HYPERSONIC FLOWFIELDS ...........................................................................................................................................................................................10237

Geng Qian, Bao-Guo Wang

VISUAL STUDY OF RESONANCE DOMINATED MICROJET FLOWS USING LASER-BASED MICRO-SCHLIEREN...............................................................................................................................................................................................10245

Chase Foster, John Solomon, Farrukh Alvi

NUMERICAL SIMULATION OF A FILM-COOLING FLOW WITH A MICRO-RAMP VORTEX GENERATOR ............................................................................................................................................................................................10259

Aaron Shinn, S. Pratap Vanka

INVESTIGATION OF VORTEX BREAKDOWN AND SCALAR MIXING IN SWIRLING TURBULENT JET FLOWS USING UNIFIED LES-RANS MODELS ................................................................................................................................10271

H. Gopalan, C. Zemtsop, S. Heinz, M. Stoellinger

HYBRID LARGE-EDDY SIMULATION / REYNOLDS-AVERAGED NAVIER-STOKES SIMULATIONS OF SONIC INJECTION INTO MACH 2 CROSSFLOW ...........................................................................................................................10284

J. Boles, R. Milligan, M. Hagenmaier, J. Edwards

ENERGY AND MASS TRANSFER DURING BINARY DROPLET COLLISION..........................................................................10303X. Chen, D. Ma, P. Khare, V. Yang

CONVERGENCE ACCELERATION TECHNIQUES FOR COUPLED ADAPTIVE CARTESIAN-STRAND GRID SOLUTIONS ...................................................................................................................................................................................10320

A. Katz, A. Wissink, V. Sankaran, J. Sitaraman, B. Roget

A PARALLEL MATRIX-FREE IMPLICIT FINITE VOLUME METHOD FOR CHEMICALLY REACTING FLOWS ON HYBRID GRIDS ..................................................................................................................................................................10338

D. Stefansk, S. Spiegel, H. Luo, J. Edwards

EFFICIENT SOLUTIONS OF THE EULER EQUATIONS IN A TIME-ADAPTIVE SPACE-TIME FRAMEWORK ..........................................................................................................................................................................................10356

Karthik Mani, Dimitri Mavriplis

AN IMPLICIT ADAPTIVE NON-LINEAR FREQUENCY DOMAIN METHOD (PNLFD) FOR VISCOUS PERIODIC STEADY STATE FLOWS ON DEFORMABLE GRIDS ................................................................................................10382

Ali Mosahebi Mohamadi, Siva Nadarajah

A TIGHTLY-COUPLED, SEMI-IMPLICIT CFD APPROACH FOR ALL-MACH NUMBER FLOWS.....................................10406Michael Kinzel, Scott Miller, Jules Lindau

AN IMPLICIT AND GLOBALLY CONSERVATIVE UNSTRUCTURED CHIMERA GRID METHOD ..................................10422X. Zhao, H. Guan, Z. Yang, S. Zhang

A STABLE UNSTRUCTURED FINITE VOLUME METHOD WITH MULTIGRID FOR PARALLEL LARGE-SCALE INCOMPRESSIBLE VISCOUS FLUID FLOW COMPUTATIONS ...................................................................................10433

Mehmet Sahin

NUMERICAL CONTINUATION FOR TURBULENT FLOWS PAST AN AEROFOIL................................................................10456Christopher Wales, Ann Gaitonde, Dorian Jones

SOME OBSERVATIONS ON FLAME PROPAGATION IN TURBULENT COMBUSTION.......................................................10468Yuval Dagan, Yoram Tambour, Eran Arad

ASSESSMENT OF PRESUMED PDF MODELS FOR LARGE EDDY SIMULATION OF TURBULENT PREMIXED FLAMES...............................................................................................................................................................................10480

Nasim Shahbazian, Clinton P. T. Groth, Ömer Gülder

ANALYSIS OF MULTIPLE SCALAR LARGE-EDDY SIMULATION/PROBABILITY DENSITY FUNCTION FORMULATION FOR TURBULENT SPRAY COMBUSTION ........................................................................................................10497

Colin Heye, Heeseok Koo, Venkat Raman

LARGE EDDY SIMULATION OF COMBUSTION DYNAMICS OF BLUFF BODY STABILIZED FLAME ..........................10512H. Li, H. Sung, V. Yang

NUMERICAL ANALYSIS OF COMBUSTION INSTABILITY MECHANISMS IN A LEAN PREMIXED CAN COMBUSTOR ............................................................................................................................................................................................10536

Francesca Rebosio, Massimiliano Di Domenico, Berthold Noll, Manfred Aigner

COMBUSTION LES OF CESAR MULTI-BURNER ANNULAR COMBUSTOR...........................................................................10548Ekaterina Fedina, Christer Fureby, Sergiy Borzov, Vladimir Gusev, Tatiana Stepanova

FLOW DYNAMICS IN COMBUSTORS WITH MULTI-ELEMENT SWIRL INJECTORS ........................................................10560Kwang-Hee Yoo, Jong-Chan Kim, Hong-Gye Sung, Liwei Zhang, Vigor Yang

EXPERIMENTAL AND NUMERICAL INVESTIGATION OF AIR-BLAST N-DODECANE INJECTION ..............................10570M. Czajkowski, O. Desjardins, B. Spatafore, J. Nabity

COMPARISON OF THREE EVAPORATION MODELS COMBINED TO THE DISTILLATION CURVE MODEL FOR MULTICOMPONENT FUEL DROPLET EVAPORATION.....................................................................................10582

P. Seers, S. Bruyère-Bergeron, X. Landry

DETERMINATION OF FUEL DROPLET EVAPORATION BASED ON MULTIPLE THERMOCOUPLE SIZES ...........................................................................................................................................................................................................10591

Patrice Seers, William Thomas, Simon Bruyère-Bergeron

JET A-1 FUEL SPRAY EVAPORATION IN A TURBULENT FLOW: EXPERIMENTAL INVESTIGATIONS AND VALIDATION OF NUMERICAL MODELS ...............................................................................................................................10597

B. Rauch, P. Le Clercq, M. Aigner, M. Rachner, R. Calabria, P. Massoli

PREFERENTIAL CONCENTRATION OF WATER DROPLETS IN A VOLUME OF HOMOGENEOUS AND ISOTROPIC TURBULENCE...................................................................................................................................................................10610

G. Charalampous, Y. Hardalupas

SUB-TO-SUPERCRITICAL MIXING AND CORE LENGTH ANALYSIS OF A SINGLE ROUND JET ..................................10618Arnab Roy, Corin Segal

COMBUSTION EFFICIENCY SENSITIVITY STUDIES OF THE API INJECTOR CONCEPT ................................................10632J. Deeken, D. Suslov, O. Haidn, S. Schlechtriem

AUTOIGNITION OF LIQUID FUEL DROPLETS IN A TURBULENT CROSS-FLOW OF AIR ...............................................10640Robert Gordon, Christos Markides, Epaminondas Mastorakos

BURNING CHARACTERISTICS OF FUEL DROPLETS WITH ADDITION OF NANOPARTICLES AT DILUTE AND DENSE PARTICLE LOADING ....................................................................................................................................10651

Yanan Gan, Li Qiao

EXPERIMENTAL STUDY OF THE DIFFRACTION OF A PLANAR DETONATION WAVE INTO A CONFINED VOLUME..............................................................................................................................................................................10661

Nolan Polley, Miles Egbert, Eric Petersen

COMPARATIVE NUMERICAL AND EXPERIMENTAL STUDY OF PULSE DETONATION INITIATION THROUGH CROSSOVER SHOCK........................................................................................................................................................10676

William Stoddard, Robert Driscoll, Ephraim Gutmark

WAVE STRUCTURES AND IRREGULAR DETONATION CELLS IN METHANE-AIR MIXTURES WITH CONCENTRATION GRADIENTS .........................................................................................................................................................10695

David Kessler, Vadim Gamezo, Elaine Oran

THE DYNAMICS OF UNSTEADY DETONATION WITH DIFFUSION ........................................................................................10713Christopher Romick, Tariq Aslam, Joseph Powers

NUMERICAL STUDY AND PERFORMANCE EVALUATION FOR PULSE DETONATION ENGINE WITH AN AEROSPIKE NOZZLE ......................................................................................................................................................................10724

N. Tsuboi, Y. Kawakami, R. Ezure, A. Hayashi, E. Yamada

STUDY OF DEFLAGRATION-TO-DETONATION TRANSITION IN GAS-PARTICLE MIXTURES......................................10737Kalyana Gottiparthi, Suresh Menon

ANALYSIS AND MODELING OF EXPLOSIVE CONTAINMENT BOX FOR AIRCRAFT IN-FLIGHT PROTECTION ...........................................................................................................................................................................................10750

G. Burns, J. Bayandor

THERMODYNAMIC MODELING OF A ROTATING DETONATION ENGINE .........................................................................10760Craig Nordeen, Douglas Schwer, Fredrick Schauer, John Hoke, Baki Cetegen, Thomas Barber

MULTIPLE-STAGE PULSE TUBE CRYOCOOLERS FOR VERY LOW TEMPERATURE COOLING .................................10775Jeffrey Olson, Ted Nast

SMALL SPACE CRYOCOOLERS .........................................................................................................................................................10780J. Raab, E. Tward

CRYOGENIC PROPELLANT BOIL-OFF REDUCTION APPROACHES......................................................................................10788T. Nast, D. Frank, K. Burns

DEVELOPMENT OF A LOW-TEMPERATURE AMRR FOR SPACE APPLICATIONS............................................................10803Weibo Chen, Mark Zagarola

SIMULATION OF CRYOGENICS CAVITATION..............................................................................................................................10811Sean Kelly, Corin Segal

DEVELOPMENT OF A NUMERICAL MODEL OF A SUPERFLUID MAGNETIC PUMP FOR SPACE SCIENCE APPLICATIONS .....................................................................................................................................................................10828

Franklin Miller, Amir Jahromi

AN EXPERIMENTAL INVESTIGATION OF UNEVEN TURN WATER AND ACETONE OSCILLATING HEAT PIPES...............................................................................................................................................................................................10836

A. Hathaway, C. Wilson, H. Ma

EFFECT OF OPERATIONAL CONDITIONS ON COOLING PERFORMANCE OF PUMP-ASSISTED AND CAPILLARY-DRIVEN TWO-PHASE LOOP .......................................................................................................................................10846

M. Crepinsek, C. Park

A CAPILLARY ASSISTED THERMOSYPHON (CAT) FOR HIGH HEAT INPUT SHIPBOARD ELECTRONICS USE ................................................................................................................................................................................10855

Martin Cerza

MODEL PREDICTIVE CONTROL USING PREVIEW MEASUREMENTS FROM LIDAR ......................................................10873Jason Laks, Lucy Pao, Eric Simley, Alan Wright, Neil Kelley, Bonnie Jonkman

COMBINED LIDAR-BASED FEEDFORWARD AND FEEDBACK CONTROLLERS FOR WIND TURBINES WITH TOWER AND BLADE DAMPING .............................................................................................................................................10893

Na Wang, Kathryn Johnson

REFINEMENTS AND TESTS OF AN ADVANCED CONTROLLER TO MITIGATE FATIGUE LOADS IN THE CONTROLS ADVANCED RESEARCH TURBINE ...................................................................................................................10907

Alan Wright, Paul Fleming, Jan-Willem Van Wingerden

CONTROL OF A WIND TURBINE WITH A MAGNETIC CONTINUOUSLY VARIABLE TRANSMISSION FOR MITIGATION OF TORQUE VARIATIONS ...............................................................................................................................10920

Jacob Aho, L. Gordon Kraft

VOLUME 13

ADAPTIVE DISTURBANCE TRACKING CONTROL FOR LARGE HORIZONTAL AXIS WIND TURBINES WITH DISTURBANCE ESTIMATOR IN REGION II OPERATION ..............................................................................................10948

Mark Balas, Kaman Thapa Magar, Qian Li

ADAPTIVE DISTURBANCE TRACKING CONTROL FOR LARGE HORIZONTAL AXIS WIND TURBINES IN VARIABLE SPEED TRANSITION OPERATION .........................................................................................................................10964

M. Balas, Q. Li, K. Thapa Magar, S. Frost

ADDING FEEDFORWARD BLADE PITCH CONTROL FOR LOAD MITIGATION IN WIND TURBINES: NON-CAUSAL SERIES EXPANSION, PREVIEW CONTROL, AND OPTIMIZED FIR FILTER ME......................................10978

Fiona Dunne, Lucy Pao, Alan Wright, Bonnie Jonkman, Neil Kelley, Eric Simley

IMPROVED INDIVIDUAL PITCH CONTROL FOR WIND FARM TURBINE LOAD REDUCTION VIA WAKE MODELLING ...............................................................................................................................................................................10995

Zhongzhou Yang, Yaoyu Li, John Seem

EXPERIMENTAL OPTIMIZATION AND PERFORMANCE ANALYSIS OF A MAV SCALE CYCLOIDAL ROTOR........................................................................................................................................................................................................11007

Tejaswi Jarugumilli, Moble Benedict, Inderjit Chopra

FLOW CONTROL FOR BOUNDARY LAYER INGESTION IN AN S-DUCT DIFUSER.............................................................11018Jonathan Parham, Matthew Fitzgerald, Elena De La Rosa Blanco

OPTIMIZATION OF 2-D FLAP GEOMETRY USING MATLAB AND FUN3D ............................................................................11027Gregory Howe

A PROBABILISTIC APPROACH TO INVERSE CONVECTION-DIFFUSION ............................................................................11038Ian Tobasco, Krzysztof Fidkowski

EFFECT OF DIMPLE DEPTH ON HEAT TRANSFER ENHANCEMENT IN A RECTANGULAR CHANNEL (AR = 3:1) WITH HEMISPHERICAL DIMPLES.................................................................................................................................11049

Lance Case, C. Neil Jordan, Lesley Wright

EXPERIMENTAL AERODYNAMIC INVESTIGATION OF NASA ORION FORWARD BAY MODIFICATIONS.....................................................................................................................................................................................11060

Darren Montes, Trenton West, Thomas Yechout

DROP TOWER AND ALTERNATE IMMERSION MACHINE: DESIGN AND REVIEW ..........................................................11071Matt Bender, David Lanning

VIBRATION CONTROL OF THIN PLATES WITH PERIODICALLY DISTRIBUTER SHUNTED ARRAYS .......................11082Fillipo Casadei, Massimo Ruzzene

LARGE EDDY SIMULATIONS OF 2-D AND 3-D SPATIALLY DEVELOPING MIXING LAYERS ........................................11093C. Martha, G. Blaisdell, A. Lyrintzis

ALLOCATION OF TESTING RESOURCES IN STATISTICAL SIMULATIONS USING PARTICLE SWARM OPTIMIZATION .......................................................................................................................................................................................11104

Carolina Dubinsky, Harry Millwater

DESIGN AND VALIDATION TESTING OF THE SOLBRID ROCKET MOTOR ........................................................................11115Jacob Dennis, James Villarreal

ANALYSIS OF WEAK STABILITY BOUNDARY TRANSFERS FOR AN EARTH-MOON SYSTEM FOR THE EUROPEAN STUDENT MOON ORBITER MISSION .......................................................................................................................11125

Gianfranco Laguardia

DEVELOPMENT AND FIELD-TESTING OF A PROTOTYPE TOOLKIT FOR ASTRONAUT PLANETARY EXPLORATION ACTIVITIES ON MOON/MARS .............................................................................................................................11135

Justin Brannan, Heather Bradshaw

DYNAMICALLY VARIABLE BLADE GEOMETRY FOR WIND ENERGY.................................................................................11145Michael Ross, Greg Meess, Ephrahim Garcia

DORRA THE EUROPA EXPLORER: AN ORBITAL AND IN-SITU INVESTIGATION OF HABITABILITY .......................11155Kaitlin Gushwa, Ana Guerrero De La Pena, Jaime Cervantes, Chirag Patel, Wallace Fowler

CUBOAT: COLORADO UNDERWATER BUOYANT OCEANIC ACOUSTIC NETWORK ......................................................11166Daniel Ambrosio, Ryan Del Gizzi, Bobby Hodgkinson, Jared Kirkpatrick, Colin Miller, Julie Price, Tyler Thomas

LOX/METHANE ENGINE UTILIZING LIQUID/LIQUID CO-AXIAL SWIRL INJECTOR ......................................................11176Christopher Bostwick, Tristan Gibbs, Anusha Prabhakar

DETERMINATION OF NITRIC OXIDE CONCENTRATION IN UPPER ATMOSPHERE USING ROCKSAT.....................11187Melissa Motylinski, Sruthi Krishnan, Michelle Perez, Adam Jones, Jeff Craley

DESIGN, CONSTRUCTION, AND TESTING OF RC AIRCRAFT FOR A HYBRID PROPULSION SYSTEM.......................11197Andrew Deschenes, Kayleigh Brown, Alexandra Sobin, Gregory West

THE DESIGN AND CONSTRUCTION OF A BLENDED WING BODY UAV ...............................................................................11208Daniel Thompson, Joshuo Feys, Michael Filewich, Sharif Abdel-Magid, Dennis Dalli, Fumitaka Goto

HYBRID LINER CONCEPT WITH INTEGRATED ACTIVE DEVICES FOR ACTIVE NOISE REDUCTION IN ENGINE INTAKES AND EXHAUSTS .............................................................................................................................................11219

M. Bauer, C. Krauspe

DIRECT NUMERICAL SIMULATION OF THREE DIMENSIONAL HONEYCOMB LINER WITH CIRCULAR APERTURES .......................................................................................................................................................................11227

Qi Zhang, Daniel Bodony

IDENTIFICATION OF INDIRECT COMBUSTION NOISE AT THE EXIT OF A GAS TURBINE ...........................................11260Jeffrey Miles

STUDY OF NARROWBAND DAMPERS WITH ZERO WEIGHT PENALTY FOR AERO ENGINE COMBUSTION INSTABILITY SUPPRESSION ..................................................................................................................................11294

J. Monfort, R. Kashani, B. Kiel

MULTIDISCIPLINARY COMPUTATIONAL ROTOR NOISE PREDICTION FOR HELICOPTER ROTOR IN HIGH-SPEED FORWARD FLIGHT ......................................................................................................................................................11305

Yi Liu

UNSTEADY PSP MEASUREMENT IN LOW-SPEED FLOW - OVERVIEW OF RECENT ADVANCEMENT AT TOHOKU UNIVERSITY ...................................................................................................................................................................11316

Keisuke Asai, Daisuke Yorita

APPLICATION OF FAST PRESSURE SENSITIVE PAINT IN HYPERVELOCITY FLOW ......................................................11329William Flaherty, James Crafton, Gregory Elliott, Joanna Austin

PRESSURE-SENSITIVE PAINT APPLICATION ON TWO-DIMENSIONAL AND AXISYMMETRIC MODEL IN HYPERSONIC FLOW.........................................................................................................................................................................11337

L. Yang, E. Erdem, K. Kontis

EXPERIMENTAL STUDY OF HEAT TRANSFER MEASUREMENT USING TEMPERATURE-SENSITIVE PAINT FOR HIGH-TEMPERATURE APPLICATION IN HYPERSONIC FLOW .......................................................................11351

Hiroki Nagai, Ryosuke Swamura, Keisuke Asai

TEMPERATURE-SENSITIVE PAINT CALIBRATION METHODOLOGY DEVELOPED AT AEDC TUNNEL 9 ....................................................................................................................................................................................................................11361

Inna Kurits, Joseph Norris, Pratik Bhandari

AERODYNAMIC MEASUREMENTS IN THE MARS WIND TUNNEL AT TOHOKU UNIVERSITY .....................................11375Masayuki Anyoji, Kei Nose, Shingo Ida, Daiju Numata, Hiroki Nagai, Keisuke Asai

EFFECT OF LATERAL CONDUCTION IN A THIN FOIL HEATER ON LOCAL MEASUREMENT OF HEAT TRANSFER COEFFICIENT....................................................................................................................................................................11389

M. Miller, G. Natsui, M. Torrance, M. Ricklick, J. Kapat

AN EXPERIMENTAL STUDY INTO THE FLOW PHYSICS OF THREE-DIMENSIONAL SHOCK CONTROL BUMPS ........................................................................................................................................................................................................11401

Paul Bruce, Holger Babinsky

EXPERIMENTAL INVESTIGATION OF THE FLOW STRUCTURE FOR SHOCK WAVE/BOUNDARY LAYER INTERACTIONS AT AN INTERSECTING NORMAL AND SPANWISE PLANE.........................................................11418

D. Burton, Holger Babinsky, Paul Bruce

EXPERIMENTAL INVESTIGATION OF CORNER FLOWS IN RECTANGULAR SUPERSONIC INLETS WITH 3D SHOCK-BOUNDARY LAYER EFFECTS ..........................................................................................................................11431

Walter Eagle, James Driscoll, Jack Benek

NUMERICAL PREDICTION OF SUPERSONIC SHOCK-BOUNDARY LAYER INTERACTION ...........................................11442Vishal Bhagwandin, James Despirito

NUMERICAL ANALYSIS OF WALL PROPERTIES IN CROSSING-SHOCK-WAVE/TURBULENT-BOUNDARY-LAYER INTERACTIONS ...............................................................................................................................................11455

Yufeng Yao, Andrea Salin, Sing Lo

THE INTERACTION BETWEEN VORTEX RINGS AND OBLIQUE SHOCKS BY THE MVG CONTROLLED RAMP FLOW AT M=2.5 ..........................................................................................................................................................................11472

Q. Li, Y. Yan, X. Wang, C. Liu

OVERVIEW OF THE 1ST AIAA CFD HIGH LIFT PREDICTION WORKSHOP ........................................................................11491Jeffrey Slotnick, Judi Hannon, Mark Chaffin

NSU3D RESULTS FOR THE FIRST AIAA HIGH-LIFT PREDICTION WORKSHOP................................................................11509Mike Long, Dimitri Mavriplis

HIGH LIFT CFD SIMULATIONS WITH AN SST-BASED PREDICTIVE LAMINAR TO TURBULENT TRANSITION MODEL.............................................................................................................................................................................11530

Robin Steed

COMPUTATIONAL ASSESSMENT OF THE HILIFTPW-1 TRAP-WING MODEL USING THE ELSA CFD SOFTWARE ...............................................................................................................................................................................................11541

L. Wiart, M. Meunier

OVERFLOW ANALYSIS OF THE NASA TRAP WING MODEL FROM THE FIRST HIGH LIFT PREDICTION WORKSHOP ...................................................................................................................................................................11553

Anthony Sclafani, Jeffrey Slotnick, John Vassberg, Thomas Pulliam, Henry Lee

IMPROVING THE PREDICTION FOR THE NASA HIGH-LIFT TRAP WING MODEL...........................................................11588P. Eliasson, S. Peng, A. Hanifi

COMPUTATIONS OF HIGH-LIFT WING-BODY CONFIGURATION ON UNSTRUCTED GRIDS USING K-W MODELS ................................................................................................................................................................................................11604

Dasia Reyes, Sharath Girimaji, Mohagna Pandya, Khaled Abdol-Hamid

UNSTEADY FLOW SIMULATION OF A HIGH-LIFT CONFIGURATION USING A LATTICE BOLTZMANN APPROACH................................................................................................................................................................................................11622

Ehab Fares, Swen Noelting

LONGITUDINAL AERODYNAMICS OF A RAPIDLY-PITCHING FIXED-WING MICRO AIR VEHICLE..........................11640Ryan Randall, Sergey Shkarayev, Gregg Abate, Judson Babcock

EXPERIMENTAL STUDY OF AERODYNAMIC PERFORMANCE OF LOCUST AND MODEL WINGS .............................11673Rajeev Kumar, Dmytro Silin, Sergey Shkarayev

EXPERIMENTS ON PITCHING PLATES: FORCE AND FLOWFIELD MEASUREMENTS AT LOW REYNOLDS NUMBERS...........................................................................................................................................................................11687

G. Kenneth, M. Ol, L. Bernal

EXPERIMENTAL COMPLICATIONS INHERENT TO LOW REYNOLDS NUMBER WIND TUNNEL TESTING ....................................................................................................................................................................................................11705

Matthew Shields, Kamran Mohseni

EXPERIMENTAL AND COMPUTATIONAL TOOLS FOR THE DEVELOPMENT OF VALVED MICROPULSJETS FOR MAV PROPULSION APPLICATIONS .....................................................................................................11715

Joseph Scroggins, Fei Zheng, Scott Steinmetz, William Roberts

WIND TUNNEL TESTING AIRFOILS AT LOW REYNOLDS NUMBERS ...................................................................................11723M. Selig, R. Deters, G. Wiliamson

TEST, ANALYSIS AND DESIGN OF PROPELLER PROPULSION SYSTEMS FOR MAVS .....................................................11755H. Youngren, M. Chang

RECENT DEVELOPMENTS AT THE NASA LANGLEY RESEARCH CENTER NATIONAL TRANSONIC FACILITY...................................................................................................................................................................................................11775

Roman Paryz

EFFECTS OF ACTIVE STING DAMPING ON COMMON RESEARCH MODEL DATA QUALITY.......................................11788M. Acheson, S. Balakrishna

ON TRANSITION DETECTION AT HIGH SUBSONIC FREESTREAM MACH NUMBERS USING THERMORESISTIVE SURFACE SENSORS .......................................................................................................................................11811

J. Leuckert, R. Erdmann, W. Nitsche, H. Rosemann

HOT-WIRE MEASUREMENTS IN CRYOGENIC ENVIRONMENT .............................................................................................11824H. Quix, J. Quest, C. Brzek

COMPLEMENTARY NUMERICAL AND EXPERIMENTAL DATA ANALYSIS OF THE ETW TELFONA PATHFINDER WING TRANSITION TESTS .......................................................................................................................................11843

T. Streit, K. Horstmann, G. Schrauf, S. Hein, U. Fey, Y. Egami, J. Perraud, I. El Din, U. Cella, J. Quest

VOLUME 14

AERO-STRUCTURAL WIND TUNNEL EXPERIMENTS WITH ELASTIC WING MODELS AT HIGH REYNOLDS NUMBERS (HIRENASD - ASDMAD).............................................................................................................................11859

J. Ballmann, A. Boucke, B. Chen, L. Reimer, M. Behr, A. Dafnis, C. Buxel, S. Buesing, H. Reimerdes, K. Brakhage, H. Olivier, M. Kordt, J. Brink-Spelink, F. Theurich, A. Buscher

A DYNAMIC SAMPLING METHOD FOR KRIGING AND COKRIGING SURROGATE MODELS .......................................11876M. Rumpfkeil, W. Yamazaki, M. Dimitri

BALANCING HIGH FIDELITY MDAO WITH ROBUST SYSTEM DESIGN ...............................................................................11888Katherine Alston, Tyler Winter

UNCERTAINTY QUANTIFICATION IN VISCOUS HYPERSONIC FLOWS USING GRADIENT INFORMATION AND SURROGATE MODELING ............................................................................................................................11906

Brian Lockwood, Markus Rumpfkeil, Wataru Yamazaki, Dimitri Mavriplis

THE DEVELOPMENT OF HYPER-DUAL NUMBERS FOR EXACT SECOND-DERIVATIVE CALCULATIONS ......................................................................................................................................................................................11927

Jeffrey Fike, Juan Alonso

ON CONTROLLING THE EXTENT OF ROBUST SOLUTION IN UNCERTAIN ENVIRONMENT IN MULTIOBJECTIVE OPTIMIZATION .................................................................................................................................................11944

Tohid Erfani, Sergei Utyuzhnikov

INVESTIGATION OF OPTIMAL GRID DISTRIBUTIONS FOR BURGERS' EQUATION........................................................11954E. Alyanak, C. Roy., A. Choudhary

AN ADAPTIVE SPLIT-MERGE SCHEME FOR UNCERTAINTY PROPAGATION USING GAUSSIAN MIXTURE MODELS ................................................................................................................................................................................11980

Gabriel Terejanu

AN ADVANCED NURBS FITTING PROCEDURE FOR POST-PROCESSING OF GRID-BASED SHAPE OPTIMIZATIONS .....................................................................................................................................................................................11990

Gerrit Becker, Michael Schäfer, Antony Jameson

EXTENSIONS OF A SURFACE REMESHING APPROACH............................................................................................................12009Romain Aubry, Guillaume Houzeaux, Mariano Vazquez

VIRTUAL CONTROL VOLUMES FOR THREE-DIMENSIONAL UNSTRUCTURED ELLIPTIC SMOOTHING.............................................................................................................................................................................................12024

Steve Karman

BOUNDARY LAYER MESH GENERATION AND ADAPTIVITY ..................................................................................................12043Adrien Loseille, Rainald Löhner

FULLY ANISOTROPIC SPLIT-TREE ADAPTIVE REFINEMENT MESH GENERATION USING TETRAHEDRAL MESH STITCHING ..................................................................................................................................................12057

Vincent Betro, Steve Karman

EXTENSION OF METRIC-BASED ANISOTROPIC MESH ADAPTATION TO TIME-DEPENDENT PROBLEMS INVOLVING MOVING GEOMETRIES........................................................................................................................12079

F. Alauzet, G. Olivier

EXPLORATION OF MHD FLOW CONTROL FOR A HYPERSONIC BLUNT ELLIPTIC CONE WITH AN IMPREGNATED ABLATOR...................................................................................................................................................................12101

N. Bisek, J. Poggie

RADAR REMPI FOR SODIUM ION KINETICS MEASUREMENTS .............................................................................................12121Z. Zhang, Y. Wu, M. Shneider

NUMERICAL INVESTIGATION OF THE ELECTRODYNAMIC FLOW CONTROL AROUND THE DOUBLE-CONE CONFIGURATION ....................................................................................................................................................12136

Yasunori Nagata, Kazuhiko Yamada, Takashi Abe

DSMC SIMULATION OF ELECTRODYNAMIC AEROBRAKING IN A HYPERSONIC RAREFIED NITROGEN ATMOSPHERE...................................................................................................................................................................12150

Hiroshi Katsurayama, Takashi Abe

INVESTIGATION OF CN PRODUCTION FROM CARBON BASED MATERIALS IN NITROGEN PLASMAS...................12158A. Lutz, W. Owens, D. Fletcher, J. Marschall

PROGRESS IN MHD PARACHUTE CONCEPT STUDY ..................................................................................................................12174V. Bityurin, A. Bocharov, D. Baranov, N. Popov, V. Alferov, V. Tikhonov

HYPERSONIC 3D BLUNT BODY EQUILIBRIUM AIR FLOW USING HIGH ORDER WENO SCHEMES II ......................12186J. Lee, M. Huerta, G. Zha

NUMERICAL ANALYSIS OF A 150KW ENHANCED HUELS TYPE ARC HEATER ................................................................12200S. Han, J. Beyon, J. Lee, K. Kim

ON ELECTRODYNAMIC FORCE OF DIELECTRIC BARRIER DISCHARGE ..........................................................................12210F. Roveda, J. Shang, G. Huang

ELECTRICAL AND OPTICAL STUDY OF DC DRIVEN REPETITIVELY PULSEDTRANSIENT SPARK DISCHARGE IN ATMOSPHERIC AIR.................................................................................................................................................12226

M. Janda, Z. Machala, V. Martisovits

A COMPUTATIONAL DIAGNOSTIC TOOL FOR UNDERSTANDING PLASMA STERILIZATION ....................................12239Navya Mastanaiah, Chin Cheng Wang, Judith Johnson, Subrata Roy

MODELING OF STREAMER DISCHARGES IN SUPERSONIC FLOWS FOR COMBUSTION APPLICATIONS ........................................................................................................................................................................................12249

D. Breden, L. Raja

MODELING OF WEDGE-SHAPED POROUS FLAPS FOR JET NOISE REDUCTION..............................................................12273J. Xiong, A. Johnson, F. Liu, D. Papamoschou

JET NOISE CONTROL BY NOZZLE SURFACE HF DBD ACTUATORS .....................................................................................12290V. Kopiev, N. Ostrikov, M. Zaitsev, V. Kopiev, I. Belyaev, V. Bityurin, A. Klimov, I. Moralev, S. Godin

JET NOISE SHIELDING FOR ADVANCED HYBRID WING-BODY CONFIGURATION.........................................................12306Dimitri Papamoschou, Salvador Mayoral

IMPINGING JET NOISE SUPPRESSION USING WATER MICROJETS .....................................................................................12322P. Ragaller, A. Annaswamy, J. Gustavsson, F. Alvi

A FLOW SIMULATION OF AN AXISYMMETRIC SUPERSONIC INLET WITH SUPPORT STRUTS AND ANNULAR BYPASS DUCT .....................................................................................................................................................................12337

Matthew Conway, Adam Lavely, Greg Blaisdell

ANALYSIS OF EXHAUST PLUME EFFECTS ON SONIC BOOM FOR A 59-DEGREE WING BODY MODEL ...................12357Raymond Castner

PRELIMINARY DESIGN AND COMPUTATIONAL ANALYSIS OF AN EJECTOR NOZZLE WITH CHEVRONS................................................................................................................................................................................................12376

Deepak Thirumurthy, Gregory Blaisdell, Anastasios Lyrintzis, John Sullivan

COMPARATIVE RESEARCH OF 2-D AND 3-D INTAKES FOR CRUISE M=1.6 CIVIL AIRCRAFT .....................................12393V. Vinogradov, V. Stepanov, Y. Melnikov

EFFECT OF PASSIVE BLEED SYSTEM ON AN INTEGRATED DIVERTERLESS SUPERSONIC INLET...........................12412Jehanzeb Masud, Farooq Akram

A FLIGHT CENTERED APPROACH TO ASSESS DYNAMIC FLIGHT SIMULATOR FORCE CUEING FIDELITY ...................................................................................................................................................................................................12424

David Klyde, J. Gavin Howe, R. Wade Allen, Michael McCauley, Peter Crane

THE PATH PILOTING TASKS: PROBLEMS AND SOLUTIONS ...................................................................................................12440Alexander Efremov, Mihail Tijaglik

UAV PERFORMANCE RATING SCALE BASED ON THE COOPER-HARPER PILOTED RATING SCALE ......................12451M Christopher Cotting

AIRCRAFT MANEUVER DESIGN USING BIFURCATION ANALYSIS AND NONLINEAR CONTROL TECHNIQUES ...........................................................................................................................................................................................12459

Amit Khatri, Nandan Sinha

A FRAMEWORK FOR CONSTRAINED CONTROL ALLOCATION USING CFD-BASED TABULAR DATA .....................12471A. Da Ronch, M. Ghoreyshi, D. Vallespin, K. Badcock, Z. Mengmeng, J. Opplestrup, A. Rizzi

WIND SHEAR EFFECT ON FINAL GLIDE ........................................................................................................................................12489U. Solies, A. Bogershausen

PIV IN NASA AMES UNITARY WIND TUNNELS .............................................................................................................................12498James Heineck, Edward Schairer, Stephen Walker

NO PLIF IMAGING IN THE CUBRC 48” SHOCK TUNNEL ...........................................................................................................12509N. Jiang, J. Bruzzese, R. Patton, J. Sutton, W. Lempert, J. Miller, T. Meyer, R. Parker, T. Wadham, M. Holden, P. Danehy

APPLYING CLEAN SEEDING FOR VELOCIMETRY IN THE AFRL TRISONIC GASDYNAMICS FACILITY .................12523Brian Love, Mark Reeder, Ryan Schmit, Tom Presdorf

PLANNING IMAGE-BASED MEASUREMENTS IN WIND TUNNELS BY VIRTUAL IMAGING ...........................................12534Laura Kushner, Edward Schairer

DEVELOPMENT OF COHERENT RAMAN MEASUREMENTS OF TEMPERATURE IN CONDENSED PHASES.......................................................................................................................................................................................................12548

S. McGrane, N. Dang, C. Bolme, D. Moore

FEMTOSECOND PURE-ROTATIONAL COHERENT ANTI-STOKES RAMAN SCATTERING GAS-PHASE DIAGNOSTICS ..........................................................................................................................................................................................12553

Sean Kearney, Justin Serrano

CONCENTRATION MEASUREMENTS IN CO/N2 AND AR/N2 GAS MIXTURES USING FEMTOSECOND COHERENT ANTI-STOKES RAMAN SCATTERING ......................................................................................................................12562

R. Lucht, D. Richardson, W. Kulatilaka, S. Roy, J. Gord

HYBRID FS/PS CARS SPECTROSCOPY FOR SINGLE-SHOT KHZ-RATE THERMOMETRY IN HIGH-TEMPERATURE FLAMES .....................................................................................................................................................................12574

J. Miller, C. Dedic, M. Slipchenko, T. Meyer, H. Stauffer, J. Gord

COMBUSTION MEASUREMENTS IN A COUNTER-FLOW BURNER AND PROGRESS TOWARDS VIBRATIONAL ERE-CARS MEASUREMENTS IN HIGH-PRESSURE FLAMES ......................................................................12583

Aman Satija, Devashish Bangar, Sameer Naik, Normand Laurendeau, Robert Lucht, Sukesh Roy, James Gord

FUN3D AND CFL3D COMPUTATIONS FOR THE FIRST HIGH LIFT PREDICTION WORKSHOP ....................................12595Mike Park, Elizabeth Lee-Rausch, Christopher Rumsey

CFD COMPARISON STUDY FOR TRAPEZOIDAL HIGH-LIFT WING CONFIGURATIONS BY STRUCTURED AND UNSTRUCTURED MESH METHOD ..............................................................................................................12619

Mitsuhiro Murayama, Kazuomi Yamamoto, Kentaro Tanaka

DLR CONTRIBUTION TO THE FIRST HIGH LIFT PREDICTION WORKSHOP .....................................................................12651S. Crippa, S. Milber-Wilkending, R. Rudnik

SUMMARY OF THE FIRST AIAA CFD HIGH LIFT PREDICTION WORKSHOP.....................................................................12673C. Rumsey, M. Long, R. Stuever, T. Wayman

EXPERIMENTAL STUDY OF CO-FLOW JET AIRFOIL PERFORMANCE ENHANCEMENT USING DISCREET JETS .......................................................................................................................................................................................12705

B. Dano, G. Zha, M. Castillo

THREE DIMENSIONAL RANS COMPUTATION USING DEFORMING MESH FOR SYNTHETIC JET SIMULATION ............................................................................................................................................................................................12728

Ilyong Yoo, Seungsoo Lee

STUDY OF STALL DELAY OVER A GENERIC AIRFOIL USING SYNTHETIC JET ACTUATOR .......................................12744N. Durrani, B. Haider

ACCELERATION OF AN UNSTRUCTURED HYBRID MESH RANS SOLVER BY PORTING TO GPU ARCHITECTURES ...................................................................................................................................................................................12752

W. Dawes, Caleb Dhanasekaran, William Kellar

PERFORMANCE OF UNSTRUCTURED FINITE VOLUME CODE ON A CLUSTER WITH MULTIPLE GPUS PER NODE ......................................................................................................................................................................................12762

Keith Obenschain, Andrew Corrigan, Gopal Patnaik

VOLUME 15

A FULL-DEPTH AMALGAMATED PARALLEL 3D GEOMETRIC MULTIGRID SOLVER FOR GPU CLUSTERS .................................................................................................................................................................................................12772

Dana Jacobsen, Inanc Senocak

SCALABILITY OF INCOMPRESSIBLE FLOW COMPUTATIONS ON MULTI-GPU CLUSTERS USING DUAL-LEVEL AND TRI-LEVEL PARALLELISM ............................................................................................................................12789

Dana Jacobsen, Inanc Senocak

PORTING OF FEFLO TO MULTI-GPU CLUSTERS.........................................................................................................................12800A. Corrigan, R. Löhner

ITERATIVE STRAIN-GAGE BALANCE CALIBRATION DATA ANALYSIS FOR EXTENDED INDEPENDENT VARIABLE SETS........................................................................................................................................................12811

Norbert Ulbrich

THERMAL AND PRESSURE CHARACTERIZATION OF A WIND TUNNEL FORCE BALANCE USING THE SINGLE VECTOR SYSTEM ...................................................................................................................................................................12827

K. Lynn, S. Commo, T. Johnson, P. Parker

FORCE MEASUREMENTS IN HYPERVELOCITY FLOWS WITH AN ACCELERATION COMPENSATED STRAIN GAGE BALANCE .....................................................................................................................................................................12847

Eric Marineau, Matthew Maclean, Erik Mundy, Michael Holden

FORCE MEASUREMENTS IN HYPERVELOCITY FLOWS WITH AN ACCELERATION COMPENSATED PIEZOELECTRIC BALANCE ................................................................................................................................................................12862

Eric Marineau

DESIGN AND PERFORMANCE OF AN ACTIVE STING DAMPER FOR THE NASA COMMON RESEARCH MODEL .......................................................................................................................................................................................................12874

S. Balakrishna, David Butler, Michael Acheson, Eugene White

EXPERIMENTAL STUDY OF A DBD-PLASMA DRIVEN CHANNEL FLOW.............................................................................12883Marco Debiasi, Jiun-Ming Li

THE INFLUENCE OF ELECTRODE CONFIGURATION AND DIELECTRIC TEMPERATURE ON PLASMA ACTUATOR PERFORMANCE ..............................................................................................................................................................12896

R. Erfani, C. Hale, K. Kontis

INDUCED FLOW FROM SERPENTINE PLASMA ACTUATORS ACTING IN QUIESCENT AIR..........................................12908Ryan Durscher, Subrata Roy

ON MULTI-BARRIER PLASMA ACTUATORS .................................................................................................................................12919Ryan Durscher, Subrata Roy

NUCLEAR PROPULSION BASED ON INDUCTIVELY DRIVEN LINER COMPRESSION OF FUSION PLASMOIDS ..............................................................................................................................................................................................12930

John Slough

DESIGN OF Z-PINCH AND DENSE PLASMA FOCUS POWERED VEHICLES .........................................................................12938T. Polsgrove, S. Fincher, R. Adams, J. Cassibry, R. Cortex, M. Turner, C. Maples, J. Miernik, G. Statham, L. Fahisinski, J. Santarius, T. Percy

SCALING LAWS FOR MERGING AND IMPLOSION OF DISCRETE PLASMA JETS .............................................................12948J. Cassibry, M. Stanic, S. Hsu, D. Witherspoon, M. Gilmore

ENVIRONMENTALLY RESPONSIBLE AIR AND GROUND TRANSPORTATION ..................................................................12963Ramesh Agarwal

AN ETHNOGRAPHIC APPROACH TO HUMAN-MACHINE RELATIONSHIPS IN COMMERCIAL AVIATION: HEADS-UP GUIDANCE AND ENHANCED VISION ..................................................................................................13001

David Mindell, Zara Mirmalek

HYDROXYL RADICAL KINETICS IN REPETITIVELY PULSED HYDROGEN-AIR NANOSECOND PLASMAS ...................................................................................................................................................................................................13008

I. Choi, Z. Yin, I. Adamovich, W. Lempert

EFFECT OF SINGLET DELTA OXYGEN PRODUCTION ON THE KINETICS OF LOW TEMPERATURE REPETITIVELY PULSED NONEQUILIBRIUM PLASMAS ............................................................................................................13028

S. Bowman, I. Adamovich, W. Lempert

FLAME SPEED ENHANCEMENT BY O2(A1ΔG) .................................................................................................................................13047

Timothy Ombrello, Viswanath Katta, Campbell Carter

STUDIES OF C2H6/ AIR AND C3H8/ AIR PLASMA ASSISTED COMBUSTION KINETICS IN A NANOSECOND DISCHARGE ................................................................................................................................................................13057

M. Uddi, H. Guo, W. Sun, Y. Ju

KINETIC EFFECTS OF NON-EQUILIBRIUM PLASMA ON PARTIALLY PREMIXED FLAME EXTINCTION ............................................................................................................................................................................................13071

W. Sun, M. Uddi, S. Won, Y. Ju, T. Ombrello, C. Carter

DYNAMICS OF H2O TEMPERATURE AND CONCENTRATION IN ZONE OF PLASMA-ASSISTED HIGH-SPEED COMBUSTION ............................................................................................................................................................................13087

S. Leonov, A. Firsov, D. Yarantsev, M. Bolshov, Y. Kuritsin, V. Liger, V. Mironenko

INSTABILITY WAVE CONTROL BY PLASMA ACTUATORS: PROBLEMS AND PROSPECTS ..........................................13096V. Kopiev, N. Ostrikov, V. Kopiev, I. Belyaev, G. Faranosov

USE OF A MICROPHONE PHASED ARRAY TO DETERMINE NOISE SOURCES IN ROCKET PLUMES .........................13117Jayanta Panda, Robert Mosher

EXTENSIBLE RECTANGULAR NOZZLE MODEL SYSTEM ........................................................................................................13129Franco Frate, James Bridges

AN AERODYNAMIC AND ACOUSTIC ASSESSMENT OF CONVERGENT-DIVERGENT NOZZLES WITH CHEVRONS................................................................................................................................................................................................13162

Franco Frate, Abbas Khavaran

EFFECTS OF RING GROOVE AND DUTY CYCLE ON PLASMA ACTUATOR PERFORMANCE IN HIGH SPEED JETS...............................................................................................................................................................................................13179

Casey Hahn, Martin Kearney-Fischer, Mo Samimy

UNSTEADY THREE-DIMENSIONAL SIMULATION RESEARCH OF FAN-OGV-STRUT-PYLON INTERACTION IN JAPANESE ECO ENGINE PROJECT ...............................................................................................................13197

Yoshinori Ooba, Takeshi Murooka, Takashi Yamane, Osamu Nozaki, Takeshi Ishiyama

AN EXTENSIVE CRASHWORTHINESS METHODOLOGY FOR ADVANCED PROPULSION SYSTEMS, PART I: SOFT IMPACT DAMAGE ASSESSMENT OF COMPOSITE FAN STAGE ASSEMBLIES ........................................13210

M. Kim, A. Zammit, A. Siddens, J. Bayandor

AN EXTENSIVE CRASHWORTHINESS METHODOLOGY FOR ADVANCED PROPULSION SYSTEMS, PART II: DAMAGE AND VIBRATION INSTABILITY ANALYSIS OF JET ENGINE FORWARD SEC ................................13226

A. Siddens, J. Bayandor

PRELIMINARY STUDY FOR QUANTITATIVE MEASUREMENT OF FLOW FIELDS BY FOCUSING SCHLIEREN METHOD ...........................................................................................................................................................................13237

Masashi Kashitani, Yutaka Yamaguchi, Hideki Kitano

MEASUREMENTS IN OVEREXPANDED SUPERSONIC JETS BY RAINBOW SCHLIEREN DEFLECTOMETRY .................................................................................................................................................................................13248

Y. Miyazato, Y. Ishida, H. Yamamoto, K. Matsuo

STEREOSCOPIC PLANAR LASER-INDUCED FLUORESCENCE IMAGING AT 500 KHZ ....................................................13255Taylor Medford, Paul Danehy, Stephen Jones, Naibo Jiang, Matthew Webster, Walter Lempert, Joseph Miller, Terry Meyer, B. Bathel, J. Inman

HIGH-SPEED IMAGING OF FUEL/OH DISTRIBUTIONS IN A GAS TURBINE PILOT BURNER AT ELEVATED PRESSURE ..........................................................................................................................................................................13268

Andreas Lantz, Robert Collin, Johan Sjöholm, Zhongshan Li, Per Petersson, Marcus Aldén

DENSITY MEASUREMENTS OF A HIGH-SPEED, COMPRESSIBLEFLOW FIELD USING ACETONE PLANAR LASER INDUCEDFLUORESCENCE (PLIF) .....................................................................................................................13276

John Reid, Kyle Lynch, Brian Thurow

AN EXPERIMENTAL STUDY OF THE FORMATION AND UNSTEADY CHARACTERISTICS OF INLET VORTICES .................................................................................................................................................................................................13290

Zhijin Wang, Ismet Gursul

COMPRESSIBLE VORTEX LOOPS IN A SHOCK TUBE WITH HELIUM DRIVER .................................................................13317Raffaello Mariani, Konstantinos Kontis

ANALYTICAL/EXPERIMENTAL COMPARISON OF THE AXIAL VELOCITY IN TRAILING VORTICES ......................13324M. Giuni, E. Benard

FLOW OVER 50° DELTA WINGS WITH DIFFERENT LEADING-EDGE RADII ......................................................................13335Nick Verhaagen

INVESTIGATION OF A TRAILING VORTEX NEAR FIELD BY STEREOSCOPIC PARTICLE IMAGE VELOCIMETRY .......................................................................................................................................................................................13349

M. Giuni, R. Green, E. Benard

LARGE EDDY SIMULATIONS OF PERSISTENT AIRCRAFT CONTRAILS..............................................................................13359Alexander Naiman, Sanjiva Lele, Mark Jacobson

INVESTIGATION OF VISCOUS EFFECTS ON THE AEROELASTIC STABILITY OF TRANSONIC AIRFOILS ...................................................................................................................................................................................................13371

Hugo Almeida, Joao Luiz Azevedo

THE ROLE OF STRUCTURAL NONLINEARITIES IN WIND TURBINE BLADE AEROELASTIC ANALYSIS .................13401Brian Freno, Robert Brown, Paul Cizmas

LIFTOFF AND TRANSITION AERODYNAMICS OF THE ARES I (A106) LAUNCH VEHICLE ............................................13439Francis Capone, John Paulson, Gary Erickson

ARES I AERODYNAMIC TESTING AT THE BOEING POLYSONIC WIND TUNNEL.............................................................13470Jeremy Pinier, Charles Niskey, Jeremy Hanke, William Tomek

ARES I AERODYNAMIC TESTING AT THE NASA LANGLEY UNITARY PLAN WIND TUNNEL ......................................13487Gary Erickson, Floyd Wilcox

ARES I-X UPPER STAGE SIMULATOR COMPARTMENT PRESSURE COMPARISONS DURING ASCENT ...................13555W. Downs, R. Kirchner, L. Hand, B. McLachlan, S. Nelson

COMPARISONS OF CROSSWIND VELOCITY PROFILE ESTIMATES USED IN FAST-TIME WAKE VORTEX PREDICTION MODELS........................................................................................................................................................13566

M. Pruis, D. Delisi, N. Ahmad

LARGE-EDDY SIMULATION OF WAKE VORTEX EVOLUTION FROM ROLL-UP TO VORTEX DECAY ......................13575T. Misaka, F. Holzäpfel, T. Gerz, M. Manhart, F. Schwertfirm

ADVECTION OF MICROPHYSICAL SCALARS IN TERMINAL AREA SIMULATION SYSTEM (TASS) ...........................13586Nashat Ahmad, Fred Proctor

SIMULATION OF BENCHMARK CASES WITH THE TERMINAL AREA SIMULATION SYSTEM (TASS) ......................13618Nashat Ahmad, Fred Proctor

HURRICANE AND OCEANIC PROPERTIES RELATIVE TO AEROSPACE VEHICLE R&D AND FACILITIES ...............................................................................................................................................................................................13632

D. Johnson, W. Vaughan

DESIGN UNDER THE STEP_SATDB AND QUICKSAT: A WEB-BASED AND OPEN SOURCE SATELLITE DESIGN AUTOMATION ENVIRONMENT .........................................................................................................................................13667

Andrew Santangelo

IMPROVED TECHNOLOGY IMPACT MODELING THROUGH TECHNOLOGY SYNERGY MATRICES ........................13678Farooq Akram, Matthew Prior, Dimitri Mavris

VOLUME 16

A MODELING METHODOLOGY AND ENVIRONMENT FOR INTEGRATED TRIM ANALYSIS FOR A REUSABLE BOOSTER SYSTEM ..........................................................................................................................................................13690

Bradford Robertson, Daniel Crowley, Daniel Garmendia, Rebecca Douglas, Dimitri Mavris, Barry Hellman

DESIGN STANDARD FOR AN AIRBORNE RESCUE VALISE FOR INFANTS AND SMALL CHILDREN...........................13699A. Nguyen, C. Bil, G. Hanlon, J. Berman

HYBRID ELECTRIC INTEGRATED OPTIMIZED SYSTEM (HELIOS) - DESIGN OF A HYBRID PROPULSION SYSTEM FOR AIRCRAFT ..........................................................................................................................................13706

J. Koster, C. Humbargar, E. Serani, A. Velazco, D. Hillery, D. Larrabee, T. Wormer, J. Marshman, E. Petersen, D. Gaide, L. Makepeace

STRUCTURES EDUCATION WITHIN THE PENN STATE FLIGHT VEHICLE DESIGN AND FABRICATION COURSE ........................................................................................................................................................................13716

J. Cole, M. Maughmer, K. Jackson

COMPARATIVE MEASUREMENTS OF EARTH AND MARTIAN ENTRY ENVIRONMENTS IN THE NASA LANGLEY HYMETS FACILITY ...........................................................................................................................................................13725

S. Splinter, K. Bey, J. Gragg, A. Brewer

TWO-AXIS LASER-INDUCED FLUORESCENCE OF SINGLY-CHARGED XENON INSIDE A 6-KW HALL THRUSTER ................................................................................................................................................................................................13747

Wensheng Huang, Alec Gallimore, Timothy Smith

FAR-FIELD PLUME MEASUREMENTS OF A NESTED-CHANNEL HALL-EFFECT THRUSTER .......................................13764Raymond Liang, Alec Gallimore

NANO-SATELLITE GATLING-GUN PULSED PLASMA THRUSTER..........................................................................................13786L. Watson, R. Branam, R. Huffman, J. Zwahlen, N. Rosenblad

RELATION BETWEEN THRUST AND THE NUMBER OF CHARGES IN A DUSTY PLASMA SPACE THRUSTER ................................................................................................................................................................................................13808

T. Matsushita, K. Ishii, M. Matsui, Y. Yamagiwa

LASER DIAGNOSTICS OF PLASMA ENHANCED FLAMES IN A WAVEGUIDE MICROWAVE DISCHARGE SYSTEM ............................................................................................................................................................................13813

S. Hammack, X. Rao, Z. Williamson, T. Lee, C. Carter

TIME-RESOLVED TEMPERATURE MEASUREMENTS OF LASER-DESIGNATED, MICROWAVE DRIVEN IGNITION ...................................................................................................................................................................................................13821

J. Michael, M. Edwards, R. Miles

SIMULTANEOUS PARTICLE-IMAGE VELOCIMETRY AND CHEMILUMINESCENCE VISUALIZATION OF MILLISECOND PULSED CURRENT-VOLTAGE INDUCED PERTURBATIONS OF A PREMIXED PROPANE/AIR FLAME...........................................................................................................................................................................13828

J. Schmidt, A. Lynch, S. Kostka, B. Ganguly

POINT-TO-PLANE PULSED DISCHARGE INITIATED FLAME STRUCTURE MODIFICATION IN PROPANE-AIR FLAME...........................................................................................................................................................................13842

Jacob Schmidt, Biswa Ganguly

ENHANCEMENT OF BURNING VELOCITY IN PREMIXED BURNER FLAME DUE TO ELECTRON HEATING BY MICROWAVE IRRADIATION....................................................................................................................................13852

Koichi Sasaki, Koji Shinohara, Noriharu Takada

THERMAL AND AERODYNAMIC EFFECT OF ENERGY DEPOSITION ON BLUNT BODY IN SUPERSONIC FLOW ...............................................................................................................................................................................13857

Kellie Anderson, Doyle Knight

AIR SUPERSONIC FLOW CONTROL BY ENERGY DEPOSITION AND MHD ACTION NEAR BODY’S FRONT PART ............................................................................................................................................................................................13869

Tatiana Lapushkina, Alexander Erofeev, Sergey Ponyaev, Sergey Bobashev

CHARACTERIZATION OF FLOWFIELD TYPES INITIATED BY INTERACTION OF MICROWAVE FILAMENT WITH SUPERSONIC BODY ............................................................................................................................................13881

Olga Azarova, Doyle Knight, Yuri Kolesnichenko

DRAG REDUCTION STUDIES BY STEADY ENERGY DEPOSITION AT MACH 5 ..................................................................13895Erinc Erdem, Leichao Yang, Konstantinos Kontis

MODELING OF ELECTRON TEMPERATURE IN HYPERSONIC FLOWS................................................................................13915M. Kim, A. Gulhan, I. Boyd

THE EFFECT OF HEAT ON TURBULENT MIXING NOISE IN SUPERSONIC JETS ...............................................................13937Woutijn Baars, Charles Tinney, Nathan Murray, Bernard Jansen, Praveen Panickar

TOWARDS PREDICTION OF DUAL-STREAM JET NOISE: DATABASE GENERATION ......................................................13951Krishna Viswanathan, Michael Caech, In-Cheol Lee

SHOCK-INDUCED BOUNDARY LAYER SEPARATION IN C-D NOZZLES AND ITS IMPACT ON JET NOISE ..........................................................................................................................................................................................................13978

K. Zaman, T. Bencic, M. Clem, A. Fagan

EFFECTS OF SUPERSONIC JET CONDITIONS ON BROADBAND SHOCK-ASSOCIATED NOISE ....................................13992C. Kuo, D. McLaughlin, P. Morris

THE INFLUENCE OF “ENTHALPY FLUX-MOMENTUM FLUX” COUPLING ON THE ACOUSTIC SPECTRUM OF HEATED JETS ............................................................................................................................................................14017

Mohammed Afsar, Marvin Goldstein, Amy Fagan

ENTRY, DESCENT, AND LANDING WITH PROPULSIVE DECELERATION: SUERSONIC SPHERE-CONE MODEL TESTING ISSUES .....................................................................................................................................................................14042

Bryan Palaszewski, Tim Bencic

INVESTIGATIONS OF PERIPHERAL 4-JET SONIC AND SUPERSONIC PROPULSIVE DECELERATION JETS ON A MARS SCIENCE LABORATORY AEROSHELL ..........................................................................................................14067

Josh Codoni, Erin Reed, James McDaniel, Hicham Alkandry, Iain Boyd

AEROTHERMODYNAMICAL STUDY FOR THE ENTRY OF AN APOPHIS-LIKE ASTEROID ............................................14081L. Ferrier, J. Vérant, J. Moschetta

PARAMETRIC MASS MODELING FOR MARS ENTRY, DESCENT AND LANDING SYSTEM ANALYSIS STUDY.........................................................................................................................................................................................................14102

Jamshid Samareh, D. Komar

STUDY OF CAPSULE GEOMETRY FOR DUST SAMPLE ACQUISITION DURING MARS ATMOSPHERIC ENTRY FLIGHT........................................................................................................................................................................................14118

Ippei Terata, Keisuke Nakajima, Yousuke Ogino, Keisuke Sawada

EXPERIMENTAL INVESTIGATION OF LONGITUDINAL STABILITY OF THE REENTRY VEHICLE WITH TOROIDAL BALLUTE................................................................................................................................................................14129

Hirotaka Otsu

INVESTIGATION OF THE UNSTEADY BEHAVIOR OF A CIRCULATION CONTROL WING USING COMPUTATIONAL FLUID DYNAMICS .............................................................................................................................................14137

Jonathan Lichtwardt, David Marshall

IMPROVED MESHING TECHNIQUE FOR THE ENGINE EXHAUST OF AN OVER-THE-WING ENGINE AND CIRCULATION CONTROL WING CONFIGURATION .........................................................................................................14150

J. Pham, D. Marshall

NUMERICAL SIMULATIONS OF TURBULENT FLOWS AROUND A HIGH LIFT WING-BODY CONFIGURATION ...................................................................................................................................................................................14172

Bowen Zhong, Kebing Tang, Dimitris Drikakis, Shijun Guo

NUMERICAL STUDY OF FLOW SEPARATION CONTROL OVER A OA209 AIRFOIL USING DEPLOYABLE VORTEX GENERATOR .............................................................................................................................................14191

Gilles Joubert, Arnaud Le Pape, Serge Huberson

COMPUTATIONAL STUDIES OF AIRCRAFT LIFE-SUPPORT SYSTEMS ................................................................................14211Y. Zhu, X. Zhao, S. Zhang

NUMERICAL SIMULATIONS OF SUPERSONIC JET IMPINGING ON A FLAT PLATE ........................................................14227Patrick Hu, Nagendra Dittakavi

NUMERICAL COMPUTATION OF WALL PRESSURE FLUCTUATIONS DUE TO A TURBULENT BOUNDARY LAYER ................................................................................................................................................................................14234

Niloufar Mahmoudnejad, Klaus Hoffmann

CALCULATION OF UNSTEADY CONTROL SURFACE AERODYNAMICS USING REDUCED-ORDER MODELS .....................................................................................................................................................................................................14254

Kentaro Nakai, Koji Shimoyama, Shigeru Obayashi, Hiroyuki Morino, Hitoshi Yamaguchi

UNSTEADY AERODYNAMICS OF MINIATURE TRAILING-EDGE EFFECTORS BASED ON INDICIAL METHODS..................................................................................................................................................................................................14263

Bernardo Oliveira Vieira, Michael Kinzel, Mark Maughmer

EXPERIMENTAL INVESTIGATIONS INTO TRANSONIC SHOCK WAVE UNSTEADINESS ...............................................14287Paul Bruce, Ioana Coman, Geoff Holt, John Harvey

POD-GALERKIN PROJECTION OF FLAPPING WINGS ................................................................................................................14299Z. Liang, H. Dong, P. Beran

EXPERIMENTAL STUDY OF A GROUND VORTEX: THE EFFECT OF THE CROSSFLOW VELOCITY..........................14309Jorge Barata, Nuno Bernardo, Pedro Santos, André Silva

MULTI-SPECIES EFFECTS FOR PLUME MODELING ON LAUNCH VEHICLE SYSTEMS .................................................14317L. Hall, M. Applebaum, W. Eppard

BEST PRACTICES FOR CFD SIMULATIONS OF LAUNCH VEHICLE ASCENT WITH PLUMES - OVERFLOW PERSPECTIVE .................................................................................................................................................................14342

M. Gusman, J. Housman, C. Kiris

USM3D SIMULATIONS OF SATURN V PLUME INDUCED FLOW SEPARATION ..................................................................14357Karen Deere, Alaa Elmiligui, Khaled Abdol-Hamid

ESTABLISHING APPROACHES TO MODELING THE ARES I-X AND ARES I ROLL CONTROL SYSTEM WITH FREE-STREAM INTERACTION...............................................................................................................................................14375

S Paul Pao, Karen Deere, Khaled Abdol-Hamid

PLUME-INDUCED FLOW SEPARATION OVER A CONE-CYLINDER FLARE BODY ...........................................................14398J. Kless, G. Klopfer

OVERFLOW VALIDATION FOR PREDICTING PLUME IMPINGEMENT OF UNDEREXPANDED AXISYMMETRIC JETS ONTO ANGLED FLAT PLATES ...............................................................................................................14420

Henry Lee, Goetz Klopfer

DEMONSTRATION OF OPERATIONAL REAL-TIME SPACE WEATHER PROTOTYPES FOR AVIATION RADIATION AND MAGNETOSPHERIC SUB-STORMS..................................................................................................................14434

W. Tobiska, D. Bouwer, R. Shelley, C. Mertens, B. Gersey, W. Atwell, J. Love, J. Gannon, P. Friberg, V. Eccles, R. Schunk, D. Intriligator, W. Burke, P. Hagan, Michael Hesse, M. Kuznetsova

MODELING SECONDARY ELECTRON EMISSION EXPERIMENT............................................................................................14441J. Wang, P. Wang, M. Belhai, J. Mateo-Velez

PLASMA CONDITIONS DURING THE GALAXY 15 ANOMALY AND THE POSSIBILITY OF ESD FROM SUBSURFACE CHARGING....................................................................................................................................................................14448

D. Ferguson, W. Denig, J. Rodriguez

INVESTIGATION OF BUBBLE TOPOLOGY IN TUBES WITH CONSTANT BEND RADII IN A MICROGRAVITY ENVIRONMENT.....................................................................................................................................................14462

J. Bernardo, A. Wick, J. Bennewitz, M. Chrin, J. Braun

TIMINGS OF FEFLO ON THE SGI-ICE MACHINES .......................................................................................................................14473Rainald Lohner, Fernando Mut, Fernando Camelli

SOLVCON: A PYTHON-BASED CFD SOFTWARE FRAMEWORK FOR HYBRID PARALLELIZATION ..........................14483Yung-Yu Chen, David Bilyeu, Lixiang Yang, Sheng-Tao John Yu

AERODYNAMIC TESTING CAPABILITIES OF THE NASA GLENN 10- BY 10-FOOT SUPERSONIC WIND TUNNEL......................................................................................................................................................................................................14493

A. Arrington, C. Pastor, S. Simerly

REFURBISHMENT AND TESTING TECHNIQUES IN A TRANSONIC LUDWIEG TUNNEL.................................................14509T. Balcazar, E. Braun, F. Lu, D. Tran, D. Wilson

FUTURE TEST NEEDS OF U.S. NATIONAL WIND TUNNELS FOR NASA’S AERONAUTICS TEST PROGRAM: AN APPROACH FOR MAPPING GROUND TEST FACILITY USAGE PROJECTIONS INTO CAPABILITY PROJECTIONS ...............................................................................................................................................................14518

J. Kallimani, C. Ohlandt, P. Anton, J. Osburg

MONTE CARLO MODEL OF NATIONAL WIND TUNNEL DEMAND ........................................................................................14530C. Ohlandt, P. Anton, J. Kallimani, J. Osburg

PERFORMANCE STUDIES OF THE VASIMR® VX-200 .................................................................................................................14540Edgar Bering, Benjamin Longmier, Maxwell Ballenger, Chris Olsen, Jared Squire, Franklin Chang Diaz

NOVEL CONTROL OF MAGNETOPLASMA THRUSTER BY USING A ROTATING RF SYSTEM ......................................14566Y. Yasaka, S. Nishino, M. Yamamoto, S. Nakamoto, H. Takeno, H. Yonemori

MAGNETOHYDRODYNAMIC NUMERICAL ANALYSIS OF MAGNETIC PLASMA SAIL INCLUDING THE EFFECT OF INTERPLANETARY MAGNETIC FIELD ....................................................................................................................14573

N. Yamamoto, M. Matsumoto, I. Funaki, Y. Yamagiwa

ASSESSMENT OF CHARACTERISTICS OF MHD GENERATORS ON ALUMINUM OXIDATION PRODUCTS ................................................................................................................................................................................................14584

A. Sheindlin, V. Bityurin, P. Ivanov, V. Miroshnichenko

STUDY OF TRANSIENT AND UNSTEADY EFFECTS OF PLASMA ACTUATION IN TRANSITIONAL FLOW OVER AN SD7003 AIRFOIL ......................................................................................................................................................14592

P. Riherd, S. Roy, D. Rizzetta, M. Visbal

VOLUME 17

ACTIVE FLOW CONTROL BASED ON DISTRIBUTED THERMAL FIELDS: PRINCIPLES AND THEIR REALIZATION..........................................................................................................................................................................................14606

Nina Yurchenko, Igor Yurchenko

ACTIVE FLOW CONTROL WITH MW-GENERATED THERMAL FIELDS: ELECTRODYNAMIC MODELLING .............................................................................................................................................................................................14616

I. Esakov, P. Lavrov, A. Ravaev, K. Khodataev, N. Yurchenko, P. Vinogradsky, A. Zhdanov

MAIN FEATURES AND APPLICATION OF ELECTROMAGNETIC VIBRATORS LOCATED NEAR TO A METAL WALL ..........................................................................................................................................................................................14626

Alexander Ravaev, Lev Grachev, Igor Esakov, Pavel Lavrov

FLOW SEPARATION CONTROL ON AIRFOIL WITH PULSED NANOSECOND DISCHARGE ACTUATOR ...................14635Giuseppe Correale, Ilia Popov, Aleksandr Rakitin, Andrei Starikovskii, Steven Hulshoff, Leo Veldhuis

UNSTEADY FLOW AND AERODYNAMIC NOISE ANALYSIS AROUND JAXA LANDING GEAR MODEL BY BUILDING-CUBE METHOD ...........................................................................................................................................................14642

Hiroshi Onda, Ryotaro Sakai, Daisuke Sasaki, Kazuhiro Nakahashi

REVIEW OF TURBULENT BOUNDARY LAYER MODELS FOR ACOUSTIC ANALYSIS .....................................................14652Terri Miller, Judith Gallman, Mark Moeller

AERO-ACOUSTIC PERFORMANCE OF FRACTAL SPOILERS ...................................................................................................14672Jovan Nedic, Bharathram Ganapathisubramani, John Christos Vassilicos, Jacques Boree, Laurent-Emmanuel Brizzi, Andreas Spohn

NUMERICAL SIMULATION OF THREE-DIMENSIONAL JET SCREECH TONES USING A GENERAL PURPOSE FINITE-VOLUME CFD CODE ...........................................................................................................................................14692

Konstantin Kurbatskii

COMPUTATIONAL AEROACOUSTICS OF TURBULENT JETS USING LARGE EDDY SIMULATION AND ACOUSTIC INTENSITY BASED METHOD OF THE ASTE-P TOOLSET ....................................................................................14701

Patrick Hu, Nagendra Dittakavi, Mei Zhuang

COMPUTATION OF AERODYNAMIC SOUND AROUND COMPLEX STATIONARY AND MOVING BODIES .......................................................................................................................................................................................................14708

Jung-Hee Seo, Rajat Mittal

VERIFICATION OF A MULTI-TIME-STEP ADAMS-BASHFORTH (MTSAB) TIME-MARCHING SCHEME USING EXTERNAL VERIFICATION ANALYSIS (EVA) .................................................................................................................14720

Daniel Ingraham, Vasanth Allampalli, Ray Hixon

AN OPTIMIZED SPECTRAL DIFFERENCE SCHEME FOR CAA PROBLEMS.........................................................................14738J. H. Gao, Z. G. Yang, X. D. Li

NITRIC OXIDE PLIF MEASUREMENTS IN THE HYPERSONIC MATERIALS ENVIRONMENTAL TEST SYSTEM (HYMETS).................................................................................................................................................................................14750

J. Inman, B. Bathel, C. Johansen, P. Danehy, S. Jones, J. Gragg, S. Splinter

FLOW PROPERTY MEASUREMENT USING LASER-INDUCED FLUORESCENCE IN THE NASA AMES INTERACTION HEATING FACILITY.................................................................................................................................................14776

Jay Grinstead, Barry Porter, Enrique Carballo

INVESTIGATION OF A BOW SHOCK IN A SHOCK TUBE FLOW FACILITY USING HYDROXYL TAGGING VELOCIMETRY (HTV) ......................................................................................................................................................14786

Amber Perkins, Marc Ramsey, Robert Pitz, Joseph Wehrmeyer, Andrew Nelius

SUPERSONIC MASS FLUX MEASUREMENTS VIA TUNABLE DIODE LASER ABSORPTION AND NON-UNIFORM FLOW MODELING .............................................................................................................................................................14795

Leyen Chang, Christopher Strand, Jay Jeffries, Ronald Hanson, Glenn Diskin, Richard Gaffney, Diego Capriotti

TUNABLE DIODE LASER ABSORPTION SENSOR FOR MEASUREMENTS OF TEMPERATURE AND WATER CONCENTRATION IN SUPERSONIC FLOWS..................................................................................................................14814

Christopher Goldenstein, Ian Schultz, Jay Jeffries, Ronald Hanson

CAVITY ENHANCED ABSORPTION SPECTROSCOPY OF HIGH ENTHALPY PLASMA FLOW UNDER MECHANICAL VIBRATION..................................................................................................................................................................14822

Satoshi Nomura, Tsuyoshi Kaneko, Kimiya Komurasaki, Hiroki Takayanagi, Kazuhisa Fujita

IMPROVED WALL SHEAR STRESS MEASUREMENTS ON A SUPERSONIC MICROJET IMPINGEMENT SURFACE ...................................................................................................................................................................................................14829

Jonathan Naughton, Bridget Schabron, Michael Hind, Farrukh Alvi

UNSTEADY DISTRIBUTED WALL SHEAR STRESS MEASUREMENTS IN FLUID FLOWS .................................................14839Ebenezer Gnanamanickam, John Sullivan

A SAPPHIRE BASED FIBER OPTIC DYNAMIC PRESSURE SENSOR FOR HARSH ENVIRONMENTS: FABRICATION AND CHARACTERIZATION ...................................................................................................................................14852

B. Griffin, D. Mills, T. Schmitz, M. Sheplak

EFFECTS OF ICING ON ROTARY WING LOADS AND SURFACE HEAT TRANSFER ..........................................................14863J. Bain, R. Deresz, L. Sankar, T. Egolf, R. Flemming, E. Kreeger

ICING WIND TUNNEL TESTS OF A CONTAMINATED SUPERCRITICAL ANTI-ICED WING SECTION DURING SIMULATED TAKE-OFF.......................................................................................................................................................14876

C. Clark, M. Macmaster

EXPERIMENTAL INVESTIGATIONS ON THE PERFORMANCE DEGRADATION OF A LOW-REYNOLDS-NUMBER AIRFOIL WITH DISTRIBUTED LEADING EDGE ROUGHNESS ..............................................................................14890

Yan Zhang, Takafumi Igarashi, Hui Hu

DES/DDES POST-STALL STUDY WITH ICED AIRFOIL ................................................................................................................14908Alejandro Lorenzo, Eusebio Valero, Valentín De-Pablo

DEVELOPMENT, DEPLOYMENT, AND SUPPORT OF A SET OF MULTI-DISCIPLINARY, PHYSICS-BASED SIMULATIONSOFTWARE PRODUCTS ...............................................................................................................................14918

Robert Meakin, Christopher Atwood, Nathan Hariharan

OVERVIEW OF THE HELIOS VERSION 2.0 COMPUTATIONAL PLATFORM FOR ROTORCRAFT SIMULATIONS..........................................................................................................................................................................................14933

V. Sankaran, A. Wissink, A. Datta, J. Sitaraman, M. Potsdam, B. Jayaraman, A. Katz, S. Kamkar, B. Roget, D. Mavriplis, H. Saberi, W. Chen, W. Johnson, R. Strawn

RIGID AND MANEUVERING RESULTS WITH CONTROL SURFACE AND 6DOF MOTION FOR KESTREL V2 .................................................................................................................................................................................................................14955

Scott Morton, Timothy Eymann, David McDaniel, David Sears, Brett Tillman, Todd Tuckey

ADDRESSING GEOMETRY NEEDS OF SYSTEMS ENGINEERING WITH DAVINCI SOFTWARE ....................................14975Gregory Roth, John Livingston, Christopher Dailey, Alan Cline

TIP VORTEX FIELD RESOLUTION USING AN ADAPTIVE DUAL-MESH COMPUTATIONAL PARADIGM ..................14988N. Hariharan, A. Wissink, M. Steffen, M. Potsdam

HIGH RESOLUTION CFD SIMULATIONS OF MANEUVERING AIRCRAFT USING THE CREATE-AV/KESTREL SOLVER...........................................................................................................................................................................15015

John Dean, James Clifton, David Bodkin, Justin Ratcliff

NUMERICAL INVESTIGATION OF THE FLOW ANGULARITY EFFECTS OF THE NASA LANGLEY UPWT ON THE ARES I DAC1 0.01-SCALE MODEL .......................................................................................................................15037

H. Lee, G. Klopfer, J. Onufer

ENHANCEMENTS TO TETRUSS FOR NASA CONSTELLATION PROGRAM .........................................................................15067M. Pandya, Hampton; N. Frink, K. Abdol-Hamid, J. Samareh, E. Parlette, J. Taft

DEBRIS TRANSPORT MODELING TECHNIQUES ON LAUNCH VEHICLE SYSTEMS ........................................................15094L. Hall, M. Applebaum, W. Eppard

CARTESIAN EULER CODE APPLICATION FOR LAUNCH VEHICLE SYSTEMS ..................................................................15112Les Hall, William Eppard, Michael Applebaum, John Blevins

A QUASI-STEADY FLEXIBLE LAUNCH VEHICLE STABILITY ANALYSIS USING STEADY CFD WITH UNSTEADY AERODYNAMIC ENHANCEMENT ..............................................................................................................................15145

R. Bartels

A COMPARISON OF COMPUTATIONAL MODELS FOR FLUID-STRUCTURE INTERATION STUDIES OF FLEXIBLE FLAPPING WING SYSTEMS............................................................................................................................................15158

Timothy Fitzgerald, Marcelo Valdez, B. Balachandran

HIGH-ORDER SIMULATIONS OF LOW REYNOLDS NUMBER MEMBRANE AIRFOILS UNDER PRESCRIBED MOTION ..........................................................................................................................................................................15173

J. Jaworski, R. Gordnier

LEADING AND TRAILING EDGE EFFECTS ON THE AERODYNAMIC PERFORMANCE OF COMPLIANT AEROFOILS...............................................................................................................................................................................................15199

Sara Arbos-Torrent, Zi Yang Pang, Bharathram Ganapathisubramani, Rafael Palacios Nieto

THRUST AND EFFICIENCY OPTIMIZATION OF A HARMONICALLY DEFORMING THIN AIRFOIL FOR MAV DESIGN ............................................................................................................................................................................................15215

W. Walker, M. Patil, R. Canfield

EFFECTS OF MEMBRANE VIBRATION ON THE FLOW FIELD SURROUNDING FLAT-PLATE MEMBRANE AIRFOILS .........................................................................................................................................................................15234

Kyle Scott, James Hubner, Lawrence Ukeiley, Peter Ifju

COUPLED VISCOUS VORTEX PARTICLE METHOD AND UNSTRUCTURED COMPUTATIONAL FLUID DYNAMICS SOLVER FOR ROTORCRAFT AERODYNAMIC INTERACTION ANALYSIS ...................................................15251

J. Zhao, C. He, L. Zhang, H. Zhao, P. Hu

PREDICTION OF HELICOPTER MANEUVER LOADS USING BDF/TIME SPECTRAL METHOD ON UNSTRUCTURED MESHES ...................................................................................................................................................................15264

Z. Yang, D. Mavriplis, J. Sitaraman

ROTOR LOADS PREDICTION USING HELIOS: A MULTI-SOLVER FRAMEWORK FOR ROTORCRAFT CFD/CSD ANALYSIS ...............................................................................................................................................................................15285

J. Sitaraman, M. Potsdam, B. Jayaraman, A. Datta, A. Wissink, D. Mavriplis, H. Saberi

AN UNSTRUCTURED HYBRID CFD APPROACH FOR COMPUTING ROTOR WAKE FLOWS ..........................................15320Chunhua Sheng, Qiuying Zhao, Nischint Rajmohan, Lakshmi Sankar, John Bridgeman, Jim Narramore

CFD INVESTIGATION OF UNSTEADY ROTORCRAFT AIRFOIL AERODYNAMICS: MITES AND DYNAMIC STALL ....................................................................................................................................................................................15337

James Coder, Mark Maughmer, Preston Martin

EXPERIMENTAL INVESTIGATIONS OF THE NASA COMMON RESEARCH MODEL IN THE NASA LANGLEY NATIONAL TRANSONIC FACILITY AND NASA AMES 11-FT TRANSONIC WIND TUNNE ...........................15356

Melissa Rivers, Ashley Dittberner

ANALYSIS OF NASA COMMON RESEARCH MODEL DYNAMIC DATA .................................................................................15384S. Balakrishna, M. Acheson

PRESSURE-SENSITIVE PAINT MEASUREMENTS ON THE NASA COMMON RESEARCH MODEL IN THE NASA 11-FT TRANSONIC WIND TUNNEL ........................................................................................................................................15397

James Bell

A COMPARISON OF THE MEASURED AND COMPUTED SKIN FRICTION DISTRIBUTION ON THE COMMON RESEARCH MODEL ...........................................................................................................................................................15412

G. Zilliac, T. Pulliam, M. Rivers, J. Zerr, M. Delgado, N. Halcomb, H. Lee

INTAKE LIP DESIGN SYSTEM FOR GAS TURBINE ENGINES FOR SUBSONIC APPLICATIONS ....................................15429A. Pierluissi, C. Smith, D. Bevis

ADJOINT-BASED MULTIDISCIPLINARY DESIGN OPTIMIZATION OF COOLED GAS TURBINE BLADES .................15436Arash Mousavi, Siva Nadarajah

ADAPTIVE WING/AEROFOIL DESIGN OPTIMISATION USING MOEA COUPLED TO UNCERTAINTY DESIGN METHOD....................................................................................................................................................................................15454

D. Lee, J. Periaux, L. Gonzalez, E. Onate, N. Qin

MULTIDISCIPLINARY OPTIMIZATION OF A HOVERING WING WITH A SERVICE-ORIENTED FRAMEWORK AND EXPERIMENTAL MODEL VALIDATION ...................................................................................................15472

D. Bryson, B. Stanford, A. McClung, T. Sims, J. Miranda, P. Beran, G. Parker

OPTIMUM TRANSVERSE SPAN LOADS FOR TRANSPORT CATEGORY AIRCRAFT .........................................................15495Shane Donovan, Timothy Takahashi, Matt Stohr, Jason Petermeier

VOLUME 18

DATA COMPRESSION OF LARGE-SCALE FLOW COMPUTATION FOR AERODYNAMIC/AEROACOUSTIC ANALYSIS ...............................................................................................................................15509

Ryotaro Sakai, Hiroshi Onda, Daisuke Sasaki, Kazuhiro Nakahashi

DETECTING PATTERNS IN VECTOR FIELDS ................................................................................................................................15521L. Xu, H. Dinh, P. Mordohai, T. Ramsay

SCIENTIFIC CONTRIBUTIONS OF LEE H. SENTMAN III............................................................................................................15536D. Carroll, W. Solomon

TWO-DIMENSIONAL SIMULATIONS OF MICRO CAVITY DISCHARGES FOR MICRO-PROPULSION APPLICATIONS ........................................................................................................................................................................................15548

Hariswaran Sitaraman, Laxminarayan Raja

LASER SUPPORTED DETONATION IN ARGON ATMOSPHERE................................................................................................15558K. Shimamura, K. Michigami, B. Wang, K. Komurasaki, Y. Arakawa

MODELING OF THERMAL PENETRATION OF 1.07 µM CONTINUOUS WAVE BEAM WITH TARGET ABSORPTIVITY CORRECTIONS.........................................................................................................................................................15566

K. Lee, W. Baek, H. Kwon, A. Gojani, J. Yoh, W. Sin

TIME-RESOLVED MEASUREMENTS OF PLASMA-INDUCED MOMENTUM OF AIR AND N2 UNDER DBD ACTUATION..............................................................................................................................................................................................15576

Sergey Leonov, Dmitry Opaits, Richard Miles, Victor Soloviev

COMPUTATIONAL STUDY OF FLOW GENERATION BY CHARGED PARTICLES IN DBD PLASMA ACTUATORS .............................................................................................................................................................................................15587

Shoichi Ebato, Yousuke Ogino, Naofumi Ohnishi

PLASMA CONTROL OF A TURBULENT BOUNDARY LAYER IN AN UNSTARTING SUPERSONIC FLOW ...................15597Seong-Kyun Im, Hyungrok Do, Mark Cappelli

MACH 5 BOW SHOCK CONTROL BY A NANOSECOND PULSE SURFACE DBD...................................................................15606Munetake Nishihara, Keisuke Takashima, Joseph Rich, Igor Adamovich

FLOW AROUND WING MODEL WITH A SURFACE HF DISCHARGE ......................................................................................15623A. Klimov, I. Moralev, V. Bityurin, P. Kazansky, D. Chertov, I. Borisov

ROLE OF IONIZATION-OVERHEATING INSTABILITY IN FORMATION OF VOLUMETRIC STRUCTURE OF MICROWAVE STREAMER DISCHARGE ...................................................................................................................................15631

Dmitry Bychkov, Lev Grachev, Igor Esakov

EXPERIMENTAL STUDY OF ABILITY OF A SURFACE SUBCRITICAL STREAMER DISCHARGE TO ABSORB THE ENERGY OF MICROWAVE RADIATION IN DEPENDENCE ON ANGLE OF ITS FALLING ....................15637

K. Alexandrov, E. Alfeev, L. Grachev, I. Esakov, A. Khomenko, K. Khodataev

NOVEL METHODS OF GENERATION OF ATMOSPHERIC PRESSURE PLASMAS FOR THE AEROSPACE AND OTHER APPLICATIONS...............................................................................................................................................................15644

S. Kolosenok, V. Sukhomlinov, Y. Vei, A. Kuranov, A. Savarovsky

QUENCHING OF EXCITED ELECTRONIC STATES OF MOLECULAR NITROGEN IN NANOSECOND PULSED DISCHARGES IN ATMOSPHERIC PRESSURE AIR .......................................................................................................15653

M. Bak, W. Kim, M. Cappelli

THE LINEAR ELECTROMAGNETIC VIBRATOR AS THE INITIATOR OF ELECTRIC BREAKDOWN OF AIR IN DEEPLY SUBCRITICAL FIELD OF QUASIOPTICAL MICROWAVE BEAM..............................................................15660

I. Esakov, L. Grachev, K. Khodotaev

PHYSICS-BASED SYSTEMS LEVEL JET NOISE MODELING......................................................................................................15670Eric Gamble, Jonathan Bachmann, Chris Magdziasz

ADJOINT-BASED OPTIMAL CONTROL OF A MACH 1.3 TURBULENT JET FOR NOISE REDUCTION ..........................15689Jeonglae Kim, Daniel Bodony, Jonathan Freund

EFFECT OF CHEVRONS ON DOUBLE STREAM JET NOISE FROM HYBRID CAA COMPUTATIONS............................15700Francois Vuillot, Nicolas Lupoglazoff, Maxime Huet

NUMERICAL INVESTIGATION OF 3-D SUPERSONIC JET FLOWS USING LARGE EDDY SIMULATION .....................15723Shih-Chieh Lo, Gregory Blaisdell, Anastasios Lyrintzis

AERODYNAMIC AND ACOUSTIC OPTIMIZATION FOR FAN FLOW DEFLECTION...........................................................15744Andrew Johnson, Juntao Xiong, Sara Rostamimonjezi, Liu Feng, Dimitri Papamoschou

PIV MEASUREMENTS OF CHEVRONS ON F400-SERIES TACTICAL AIRCRAFT NOZZLE MODEL ..............................15766James Bridges, Mark Wernet, Franco Frate

WATER TUNNEL EXPERIMENTAL STUDIES OF LEADING EDGE VORTEX CONTROL ON DELTA WING MAV ................................................................................................................................................................................................15781

A. Jaroszewicz, J. Stachow, K. Sibilski, A. Zyluk

WIND TUNNEL GENERATED TURBULENCE .................................................................................................................................15792Michael Sytsma, Lawrence Ukeiley

DEVELOPMENT AND FLIGHT TESTING OF A WINGED UAS WITH VERTICAL TAKE-OFF AND LANDING CAPABILITIES .....................................................................................................................................................................15811

Charles Hall

EVALUATION OF BI-HARMONIC AMPLITUDE AND BIAS MODULATION FOR FLAPPING WING MAV CONTROL ..................................................................................................................................................................................................15818

M. Anderson, N. Sladek, R. Cobb

ESTIMATION OF MAV UNSTEADY AERODYNAMIC PARAMETERS FROM DYNAMIC WATER TUNNEL TESTING ....................................................................................................................................................................................................15832

A. Jaroszewicz, M. Garbowski, K. Sibilski, A. Zyluk

VALIDATING PIV MEASUREMENTS IN SUPERSONIC JETS USING SHADOWGRAPH OPTICAL IMAGING ...................................................................................................................................................................................................15843

A. Wroblewski, R. Locke, M. Wernet, J. Bridges

NEW SEEDING AND SURFACE TREATMENT METHODS FOR PARTICLE IMAGE VELOCIMETRY ............................15854Adam Perce, Frank Lu

THE EFFECTS OF WIND TUNNEL WALLS ON THE NEAR-FIELD BEHAVIOR OF A WINGTIP VORTEX ....................15864Hirofumi Igarashi, Paul Durbin, Hui Hu, Scott Waltermire, Joe Wehrmeyer

CHARACTERISTICS OF THERMAL ANEMOMETERS AT LOW-PRESSURE CONDITION IN A MARS WIND TUNNEL .........................................................................................................................................................................................15882

Daiju Numata, Masayuki Anyoji, Yasuhiro Sugino, Hiroki Nagai, Keisuke Asai

EXPERIMENTAL VELOCITY PROFILES IN THE CAP SHOCK PATTERN OF A THRUST OPTIMIZED ROCKET NOZZLE ...................................................................................................................................................................................15893

M. Ramsey, R. Pitz, T. Jenkins, Y. Matsutomi, C. Yoon, W. Anderson

TOWARDS DESIGNING WITH 3-D BUMPS FOR WING DRAG REDUCTION..........................................................................15905Jeremy Eastwood, Jerome Jarrett

ASTE-P: SOFTWARE PACKAGE FOR MULTIDISCIPLINARY, MULTIPHYSICS, MULTISCALE AND MULTIFIDELITY ANALYSIS AND DESIGN (4MAO) OF AEROSPACE VEHICLES ...............................................................15923

P. Hu, L. Xue, K. Ni, N. Dittakavi, H. Zhao, R. Kamakoti

COMPARISON OF ADAPTIVE SAMPLING METHODS FOR GENERATION OF SURROGATE AERODYNAMIC MODELS ....................................................................................................................................................................15940

Thomas Mackman, Christian Allen, Mehdi Ghoreyshi, Kenneth Badcock

DERIVATIVE-ENHANCED VARIABLE FIDELITY SURROGATE MODELING FOR AERODYNAMIC FUNCTIONS...............................................................................................................................................................................................15953

W. Yamazaki, D. Mavriplis

AERODYNAMIC OPTIMIZATION OF THE FLAT PLATE LEADING EDGE FOR EXPERIMENTAL STUDIES OF LAMINAR AND TRANSITIONAL BOUNDARY LAYERS ......................................................................................15974

Ronald Hanson, Howard Buckley, Philippe Lavoie

A CREATE SHADOW-OPS PERSPECTIVE OF TURBO AND OVERFLOW 2 APPLICATION TO TWO AXIAL FLOW COMPRESSORS ............................................................................................................................................................15985

J. Sirbaugh, A. Watts

AERODYNAMIC CONTROL SURFACE IMPLEMENTATION IN KESTREL V2.0 ...................................................................15996D. McDaniel, D. Sears, T. Tuckey, B. Tillman, S. Morton

AN EFFICIENT METHOD OF COMPUTING MANEUVERING AIRCRAFT SURFACE LOADS USING CFD, PROPER ORTHOGONAL DECOMPOSITION, AND SYSTEM IDENTIFICATION...................................................................16020

C. Lillian, D. McDaniel, S. Morton

EXTENSIBLE SOFTWARE ENGINEERING PRACTICES FOR THE HELIOS HIGH-FIDELITY ROTARY-WING SIMULATION CODE...................................................................................................................................................................16029

Buvaneswari Jayaraman, Andrew Wissink, Sameer Shende, Stephen Adamec, Venkateswaran

NUMERICAL STUDY COMPARING RANS AND LES APPROACHES ON A CIRCULATION CONTROL AIRFOIL .....................................................................................................................................................................................................16043

Christopher Rumsey, Takafumi Nishino

STALL SUPPRESSION OF A LOW-REYNOLDS-NUMBER AIRFOIL WITH A DYNAMIC BURST CONTROL PLATE....................................................................................................................................................................................16072

Travis Grager, Alric Rothmayer, Hui Hu

REYNOLDS NUMBER SCALABILITY FOR SEPARATION CONTROL ON A LAMINAR AIRFOIL....................................16082M. Thake, N. Packard, C. Bonilla, K. Gompertz, J. Bons

EXPERIMENTAL AND NUMERICAL STUDIES OF ACTIVE FLOW CONTROL TECHNIQUE FOR THE REDUCTION OF HELICOPTER BVI NOISE .....................................................................................................................................16093

C. Velez, P. Coronado, H. Al-Kuran, A. Deperta, M. Ilie

FURTHER INVESTIGATION INTO THE ORIGIN OF THE CARBUNCLE PHENOMENON IN AERODYNAMIC SIMULATIONS .........................................................................................................................................................16107

M. Ramalho, J. Azevedo

APPROXIMATE ENTROPY LAYER SWALLOWING MODEL FOR THE ENGINEERING LEVEL AEROTHERMODYNAMICS CODE CBAERO ...................................................................................................................................16140

David Kinney

PREDICTION OF FLUID – SURFACE INTERACTIONS AND AEROTHERMAL ENVIRONMENTS USING CBAERO .....................................................................................................................................................................................................16154

David Kinney

MODEL UNCERTAINTIES IN A SHARP LEADING-EDGE HYPERSONIC BOUNDARY LAYER ........................................16168Marat Kulakhmetov, Alina Alexeenko

GEOMETRICAL RELATIONSHIPS FOR OSCULATING CONES AND OSCULATING FLOWFIELD WAVERIDERS...........................................................................................................................................................................................16180

Patrick Rodi

AERODYNAMIC AND AEROTHERMAL ENVIRONMENT MODELS FOR A MARS ENTRY, DESCENT, AND LANDING SYSTEMS ANALYSIS STUDY..................................................................................................................................16187

David Kinney

DESIGN AND EVALUATION OF A STRUCTURALLY INTEGRATED VERTICAL AXIS WIND TURBINE.......................16198J. Stockton, J. Hill, A. Larson, J. Jacob

GYROPLANE ROTOR AERODYNAMICS REVISITED - BLADE FLAPPING AND RPM VARIATION IN ZERO-G FLIGHT......................................................................................................................................................................................16221

E. Niemi, B. Gowda

EFFECT OF INFLOW MODELING ON COUPLING BETWEEN ROTOR FLIGHT MECHANICS AND AEROMECHANICS..................................................................................................................................................................................16238

Nischint Rajmohan, Lakshmi Sankar, Mark Costello

OPTIMISING ASPECTS OF ROTOR BLADES IN FORWARD FLIGHT ......................................................................................16256Catherine Johnson, George Barakos

ANALYSIS OF LIQUID DRAINAGE FROM A CONCENTRIC CYLINDER CAPACITANCE PROBE IN RESPONSE TO A SETTLING THRUST ...............................................................................................................................................16284

E. Rame, G. Zimmerli

THE CAPILLARY FLOW EXPERIMENTS (CFE-2) ON ISS: STATUS..........................................................................................16293W. Blackmore, M. Weislogel, Y. Chen, L. Kiewidt, J. Klatte, C. Bunnell

THE CONSTRAINED VAPOR BUBBLE (CVB) EXPERIMENT IN THE MICROGRAVITY ENVIRONMENT OF THE INTERNATIONAL SPACE STATION ..................................................................................................................................16303

Arya Chatterjee, Joel Plawsky, Peter Wayner, David Chao, Ronald Sicker, Tibor Lorik, Louis Chestney, John Eustace, John Zoldak

OBSERVATION AND ANALYSIS OF SMECTIC ISLANDS IN SPACE (OASIS) .........................................................................16322N. Clark, J. Maclennan, M. Glaser, C. Park, R. Stannarius, P. Tin, N. Hall

IMPROVED MEASUREMENTS OF “TUNNEL NOISE” PRESSURE FLUCTUATIONS IN THE AEDC HYPERVELOCITY WIND TUNNEL NO. 9 .........................................................................................................................................16344

A. Bounitch, D. Lewis, J. Lafferty

HIGH ACCURACY, HIGH TEMPERATURE PRESSURE PROBES FOR AERODYNAMIC TESTING .................................16356A. Ned, S. Goodman, J. Vandeweert, S. Carter

NUMERICAL MODEL OF AN ASPIRATED TEMPERATURE PROBE........................................................................................16362Robert Rhodes, Trevor Moeller

SHAPE OPTIMIZATION OF A DUCTED ROTOR SYSTEM FOR AERODYNAMIC PERFORMANCE................................16373R. Singh, S. Dinavahi

DESIGN OF A HYBRID WING-BODY AIRCRAFT TO MAXIMIZE MARKET DISRUPTION ................................................16381A. Donaldson, J. Gibbs, P. Mody

COMPARISON OF SAMPLING METHODS FOR A DYNAMIC PRESSURE REGULATOR....................................................16392Johan Persson, Johan Ölvander

OPTIMIZATION OF INDUCED VELOCITY FOR PLASMA ACTUATOR WITH MULTIPLE ENCAPSULATED ELECTRODES USING RESPONSE SURFACE METHODOLOGY ..............................................................16403

Rasool Erfani, Tohid Erfani, Craig Hale, Konstantinos Kontis, Sergei Utyuzhnikov

TAILORING THE AIR PLASMA WITH DOUBLE LASER PULSES..............................................................................................16412Mikhail Shneider, Aleksei Zheltikov, Richard Miles

VOLUME 19

A DISCONTINUOUS GALERKIN METHOD FOR THE MAGNETOHYDRODYNAMICS ON ARBITRARY GRIDS..........................................................................................................................................................................................................16425

Behrouz Halashi, Hong Luo, Daniel Spicer, Peter Macniece

EULER EQUATIONS FLOW FIELD DEPENDENT FINITE ELEMENT METHOD ...................................................................16442Seth Thompson, Jason Cassibry

METHANE-AIR MIXTURE IGNITION BY COMBINED LASER AND MICROWAVE DISCHARGES .................................16451A. Tropina, J. Michael, M. Shneider, R. Miles

IGNITION DELAY AND TIME-RESOLVED TEMPERATURE MEASUREMENTS IN NANOSECOND PULSE HYDROGEN-AIR AND ETHYLENE-AIR PLASMAS AT ELEVATED INITIAL TEMPERATURES ......................................16458

Zhiyao Yin, Igor Adamovich

NONEQUILIBRIUM PLASMA RELAXATION AND THERMALIZATION IN HYDROCARBON-AIR MIXTURES.................................................................................................................................................................................................16482

A. Starikovskiy, N. Aleksahdrov

PLASMATRONS POWERED BY PULSED HIGH–VOLTAGE NANOSECOND DISCHARGE FOR ULTRA–LEAN FLAMES STABILIZATION ........................................................................................................................................................16488

A. Nikipelov, A. Rakitin, I. Popov, G. Correale, A. Starikovskii

NON-SELFMAINTAINED GAS DISCHARGE FOR IMPACT ON FLAMMABLE GAS MIXTURES (THEORY) .................16495Vladimir Bychkov, Nikolai Ardelyan, Konstantin Kosmachevskii, Igor Kochetov

NON-SELFMAINTAINED GAS DISCHARGE FOR IMPACT ON FLAMMABLE GAS MIXTURES (EXPERIMENT) ........................................................................................................................................................................................16508

V. Bychkov, D. Bychkov, S. Denisjuk, V. Gudovich

PULSED SHOCK TUBE ACTUATORS FOR NOISE REDUCTION IN HIGH SPEED APPLICATIONS.................................16522R. Ramachandran, G. Raman

EFFECTS OF SHEAR-LAYER CHARACTERISTIC ON THE FEEDBACK-LOOP MECHANISM IN SUPERSONIC OPEN CAVITY FLOWS................................................................................................................................................16535

Weipeng Li, Taku Nonomura, Kozo Fujii

FLOW DRIVEN OSCILLATING VORTEX GENERATORS FOR CONTROL OF CAVITY RESONANCE ..........................16547Pavel Danilov, Todd Quackenbush

COMPUTATIONAL MODELING OF A MODIFIED ROD IN CROSS-FLOW DEVICE ON A REALISTIC FIGHTER AIRCRAFT CONFIGURATION .........................................................................................................................................16555

William Coirier, Shawn Westmoreland, Keith Jordan, Jennie Barber, Robert Tramel, Shane Lackey

PROGRESS ON ACTIVE CONTROL OF OPEN CAVITIES ............................................................................................................16575H. Takahashi, F. Liu, M. Palaviccini, M. Oyarzun, J. Griffin, L. Ukeiley, L. Cattafesta

COST-EFFICIENT STATE ESTIMATION FOR PRECISION PROJECTILES ............................................................................16591L. Fairfax, F. Fresconi, M. Costello

AN INTEGRATED SIX DEGREE-OF-FREEDOM TRAJECTORY SIMULATOR FOR HYBRID SOUNDING ROCKETS...................................................................................................................................................................................................16602

Seffat Chowdhury, Jean Pitot De La Beaujardiere, Michael Brooks, Lance Roberts

LINEAR TIME INVARIANT FORMULATION OF THE GYROSCOPIC PROBLEM USING QUATERNION MATHEMATICS .......................................................................................................................................................................................16615

George Davailus

REVERSE LAUNCH ABORT SYSTEM PARACHUTE ARCHITECTURE TRADE STUDY .....................................................16635D. Litton, S. O'Keefe, R. Winski

NONLINEAR AEROELASTIC SIMULATION OF X-HALE: A VERY FLEXIBLE UAV............................................................16654Carlos Cesnik, Weihua Su

REDUCED ORDER MODEL BASED SIMULATION OF AEROELASTIC(AE) AEROSERVOELASTIC (ASE) DYNAMICS USING ASTE-P TOOLSET...............................................................................................................................................16667

P. Hu, K. Ni, L. Xue, H. Zhao, M. Brenner

AVERAGING OF THE NONLINEAR DYNAMICS OF FLAPPING WING MICRO AIR VEHICLES FOR SYMMETRICAL FLAPPING..................................................................................................................................................................16680

Christopher Orlowski, Anouck Girard

DIFFERENTIAL LASER IONIZATION TAGGED RADAR ANEMOMETRY (LITRA) .............................................................16695A. Dogariu, S. McGuire, S. Zaidi, R. Miles

CHARACTERIZATION OF THERMOPHOSPHOR PARTICLES FOR SIMULTANEOUS IMAGING OF VELOCITY AND TEMPERATURE.......................................................................................................................................................16702

N. Jain, J. Seitzman, T. Jenkins, B. Heeg

TOWARDS SIMULTANEOUS HIGH-SPEED MIXTURE FRACTION AND VELOCITY IMAGING IN TURBULENT JETS...................................................................................................................................................................................16716

Randy Patton, Naibo Jiang, Walter Lempert, Jeffrey Sutton

PROGRESS TOWARDS THE DEVELOPMENT OF A 3D PIV FLOW MEASUREMENT SYSTEM FOR WIND TUNNEL APPLICATIONS ......................................................................................................................................................................16730

Morteza Gharib, Daegyoum Kim, Abdollah Khodadoust

AN UNSTRUCTURED COMPUTATIONAL FLUID DYNAMICS METHOD FOR ROTORCRAFT AERODYNAMIC INTERACTION .........................................................................................................................................................16740

Hongwu Zhao, Patrick Hu, Chengjian He, Jinggen Zhao

COMPUTATION OF AERODYNAMIC FLOWS OVER BLUFF BODIES USING AN OVERSET-GRID APPROACH................................................................................................................................................................................................16751

R. Jelic, S. Sherer, R. Greendyke

CFD VALIDATION USING DATA FROM A CLASSIC EXPERIMENTAL TEST PROGRAM FOR A HIGHLY CONTOURED BODY OF REVOLUTION HAVING REGIONS OF CONVERGENT/DIVERGENT FLOWS WITH ADVERSE/FAVORABLE PRESSURE GRADIENTS .............................................................................................................16770

B. Kulfan

CFD SIMULATIONS OF LAUNCH ENVIRONMENTS FOR DELTA IV VEHICLES AT THE SLC-6 LAUNCH PAD ..............................................................................................................................................................................................................16801

Ari Majamaki, Jinwook Lee

A PRACTICAL ANALYSIS OF UNSTEADY FLOW AROUND A BICYCLE WHEEL, FORK AND PARTIAL FRAME USING CFD ................................................................................................................................................................................16829

Matthew Godo, David Corson, Steve Legensky

NON-REPEATABILITY OF STORE SEPARATION TRAJECTORIES FROM INTERNAL WEAPON BAYS DUE TO UNSTEADY CAVITY FLOW EFFECTS - LESSONS LEARNED FROM A 2D INVESTIGATION...........................16854

Neal Kraft, Andrew Lofthouse

WEAPONS BAY ACOUSTIC SUPPRESSION USING A NOVEL ROD IN CROSSFLOW CONFIGURATION......................16863Shane Lackey, Robert Tramel, D. Brian Landrum

FIN-SHED VORTEX MODELING WITHIN MISSILE DATCOM...................................................................................................16884Christopher Rosema, Joshua Doyle

IMPROVED VALIDATION METHODOLOGY FOR MISSILE DATCOM DEVELOPMENT...................................................16899Joshua Doyle, Christopher Rosema

A TIME-DOMAIN HARMONIC BALANCE METHOD FOR DYNAMIC DERIVATIVES PREDICTIONS ............................16922David Hassan, Frederic Sicot

SHAPE OPTIMIZATION OF AN AXISYMMETRIC DIFFUSER AND A 3D HYDRO-TURBINE DRAFT TUBE USING A GENETIC ALGORITHM .......................................................................................................................................................16937

Robert Fares, Xiaomin Chen, Ramesh Agarwal

ON AERODYNAMIC DESIGN THROUGH MULTIPOINT NUMERICAL OPTIMIZATION ...................................................16946Howard Buckley, David Zingg

VARIABLE-FIDELITY KINEMATIC OPTIMIZATION OF A TWO-DIMENSIONAL HOVERING WING ..........................16961J. Moore, B. Stanford, A. McClung, P. Beran

INTEGRATING USER-PREFERENCE SWARM ALGORITHM AND SURROGATE MODELING FOR AIRFOIL DESIGN.....................................................................................................................................................................................16978

R. Carrese, H. Winarto, X. Li

AERODYNAMIC SHAPE OPTIMIZATION VIA DISCRETE VISCOUS ADJOINT EQUATIONS FOR THE K-ωSST TURBULENCE AND γ-REө TRANSITION MODELS ............................................................................................................16994

Peyman Khayatzadeh, Siva Nadarajah

ADJOINT BASED AERODYNAMIC OPTIMIZATION OF SUPERSONIC BIPLANE AIRFOILS............................................17004R. Hu, A. Jameson, Q. Wang

PARALLEL ADJOINT FRAMEWORK FOR AERODYNAMIC SHAPE OPTIMIZATION OF COMPONENT-BASED GEOMETRY ................................................................................................................................................................................17028

M. Nemec, M. Aftosmis

AN EXPERIMENTAL INVESTIGATION INTO THE EFFECT OF GURNEY FLAPS ON VARIOUS AIRFOILS ...................................................................................................................................................................................................17054

Julia Cole, Bernardo Vieira, James Coder, Amandeep Premi, Mark Maughmer

WING TWIST DESIGN CONSIDERATIONS FOR TRANSPORT CATEGORY AIRCRAFT ....................................................17063S. Donovan, T. Takahashi

EXPERIMENTAL STUDIES OF TIP-VORTEX FORMATION; INFLUENCE OF BLADE-TIP GEOMETRY ON THE VORTEX CHARACTERISTICS ............................................................................................................................................17071

D. Cousin, M. Morikone, S. Hirst, J. Elder, M. Ilie

SMALL-SCALE PROPELLERS OPERATING IN THE VORTEX RING STATE.........................................................................17082Omkar Shetty, Michael Selig

PROPELLER PERFORMANCE DATA AT LOW REYNOLDS NUMBERS ..................................................................................17098John Brandt, Michael Selig

AERODYNAMIC ANALYSIS OF OPEN TRAILING EDGE AIRFOILS AT LOW REYNOLDS NUMBER ............................17116Rodolfo Sant, Luis Ayuso, Jose Meseguer

COMPARISON OF RESOURCE REQUIREMENTS FOR A WIND TUNNEL TEST DESIGNED WITH CONVENTIONAL VS. MODERN DESIGN OF EXPERIMENTS METHODS ...............................................................................17129

Richard Deloach, John Micol

UNIQUE ASPECTS OF ACCOMMODATING TWO RECENT PARACHUTE TESTS AT THE NATIONAL FULL-SCALE AERODYNAMICS COMPLEX ....................................................................................................................................17161

P. Goulding, C. Rogers, D. Adams, A. Witkowski, K. Desabrais, T. Jenkins

STUDY ON FLOW FIELD OF STAGE SEPARATION WITH TWO REVERSAL ASYMMETRIC JETS................................17179X. Zhao, Q. Haijian, Y. Baoqin, Z. Weimin

UAV POWER PLANT PERFORMANCE EVALUATION .................................................................................................................17187Ashwin Ravi, Andrew Arena

OPTICAL HEATING, THERMOGRAPHY AND DEFORMATION MEASUREMENT OF NOZZLE WALL STRUCTURES ...........................................................................................................................................................................................17194

Andreas Gernoth, Joerg Riccius, Stefan Schlechtriem

AN EQUATION SET FOR ASME NOZZLE DISCHARGE AND THRUST COEFFICIENTS.....................................................17207Kevin Mikkelsen, Richard Brasket

DELAUNAY GRAPH MAPPING-BASED MESH DEFORMATION FOR SIMULATION OF A SPANWISE RIGID AND FLEXIBLE FLAPPING NACA0012 WING USING DES WITH PARALLEL IMPLEMENT ...............................17245

Naveed Durrani, Salimuddin Zaheer, Ning Qin

SMOOTH MIXED MESHES FOR ACCELERATION OF RANS CFD IN AIRCRAFT ANALYSIS AND DESIGN .......................................................................................................................................................................................................17259

Jochen Wild

DEVELOPMENT OF AN OVERSET GRID COMPUTATIONAL FLUID DYNAMICS SOLVER ON GRAPHICAL PROCESSING UNITS .....................................................................................................................................................17274

K. Soni, D. Chandar, J. Sitaraman

AUTOMATED OFF-BODY CARTESIAN MESH ADAPTION FOR ROTORCRAFT SIMULATIONS ....................................17298Sean Kamkar, Antony Jameson, Andrew Wissink, Venkateswaran Sankaran

PERIODIC PULSE DISCHARGE SELF-FOCUSING AND STREAMER-TO-SPARK TRANSITION IN UNDER-CRITICAL ELECTRIC FIELD ...............................................................................................................................................17323

A. Starikovskiy, S. Pancheshnyi, A. Rakitin

VOLUME 20

STUDY OF A LONGITUDINAL PLASMOID CREATED BY CAPACITY HF DISCHARGE IN SWIRL AIRFLOW...................................................................................................................................................................................................17332

A. Klimov, V. Bityurin, B. Tolkunov, I. Moralev, A. Boytsov

VALUES OF AIR BREAKDOWN FIELDS WITH RESPECT TO HEIGHT OVER EARTH.......................................................17350V. Bychkov, S. Volkov, I. Kochetov

INVESTIGATION OF MINIATURE MAGNETO-PLASMA COMPRESSORS AS A BASIC PART FOR PERSPECTIVE PLASMA ACTUATORS FOR SUPERSONIC FLOWS..........................................................................................17357

Igor Mashek, Valery Lashkov, Yury Kolesnichenko, Vadim Brovkin

FAST NONEQUILIBRIUM PLASMA THERMALIZATION IN N2-O2 MIXTURES FOR DIFFERENT PULSE POLARITIES AND ITS APPLICATION TO PREVENT ICE FORMATION .................................................................................17363

M. Rios, M. Nudnova, S. Kindusheva, N. Aleksahdrov, A. Starikovskiy

NONEQUILIBRIUM PLAMSA LIQUID WATER - DYNAMICS OF GENERATION AND QUENCHING ..............................17370A. Starikovskiy, Y. Yang, Y. Cho, A. Fridman

PCBOOM MODEL PREDICTION COMPARISONS WITH FLIGHT TEST MEASUREMENT DATA....................................17377Christopher Hobbs, Juliet Page

ADVANCED SONIC BOOM PREDICTION USING AUGMENTED BURGER'S EQUATION...................................................17388Sriram Rallabhandi

ASSESSMENT OF COMMON PRACTICE FOR SONIC BOOM CALCULATION......................................................................17405Angelo Scandaliato, Meng-Sing Liou

FEASIBILITY STUDY OF USING A SMALL-SCALE UAS FOR SONIC BOOM MINIMIZATION RESEARCH .................17426T. Jung, R. Starkey, B. Argrow

BODY TORQUE GENERATION FOR A FLAPPING WING MICRO AIR VEHICLE BY ANGLE OF ATTACK CHANGE.....................................................................................................................................................................................................17438

Michael Oppenheimer, David Sigthorsson, David Doman

MICRO AIR VEHICLE PERFORMANCE ENHANCEMENT USING EXCITED FLEXIBLE LIFTING SURFACE ...................................................................................................................................................................................................17472

Hong Yang

DEVELOPMENT AND INTEGRATION OF ADAPTIVE ROBOTIC MULTI-MODAL SYSTEM (ARM2S) ............................17495J. Dickson, C. Kulinka, M. Martin, J. Yeol, J. Clark

SLIDING MODE HEADING CONTROL FOR AUTONOMOUS SMALL UAV WITHOUT GYRO INFORMATION ........................................................................................................................................................................................17506

Ryota Kojima, Kakuji Ogawara, Hidenori Shingin

3-DIMENSIONAL TREE-BASED TRAJECTORY PLANNING WITH HIGHLY MANEUVERABLE VEHICLES..................................................................................................................................................................................................17524

Baron Johnson, Rick Lind

MULTI-STAGE FUSION ALGORITHM FOR ESTIMATION OF AERODYNAMIC ANGLES IN MINI AERIAL VEHICLE ...................................................................................................................................................................................17539

C. Ramprasadh, Hemendra Arya

TOWARDS THE DEVELOPMENT OF HIGH-SPEED 1-D RAMAN SCATTERING IN TURBULENT NON-PREMIXED FLAMES...............................................................................................................................................................................17552

Kathryn Gabet, Naibo Jiang, Walter Lempert, Jeffrey Sutton

PRESSURE AND THERMOCHEMISTRY MEASUREMENTS IN HIGH SPEED FLOWS USING ROTATIONAL AND VIBRATIONAL RAMAN SPECTROSCOPY .................................................................................................17562

Alex Bayeh, Adonios Karpetis

SPATIALLY RESOLVED TEMPERATURE AND WATER VAPOR CONCENTRATION DISTRIBUTIONS IN A FLAT FLAME BURNER BY TUNABLE DIODE LASER ABSORPTION TOMOGRAPHY ...................................................17570

Elliott Bryner, Kristin Busa, James McDaniel, Christopher Goyne, Glenn Diskin

TIME RESOLVED FILTERED RAYLEIGH SCATTERING MEASUREMENT OF A BUOYANT JET IN A CO-FLOW ..........................................................................................................................................................................................................17591

F. Benhassen, M. Polanka, M. Reeder

SPATIALLY- AND TEMPORALLY-RESOLVED MULTI-PARAMETER INTERFEROMETRIC RAYLEIGH SCATTERING............................................................................................................................................................................................17609

Daniel Bivolaru, Andrew Cutler, Paul Danehy

DEMONSTRATION OF CAPABILITY OF WATER FLUX MEASUREMENT IN A SCRAMJET COMBUSTOR USING TUNABLE DIODE LASER ABSORPTION TOMOGRAPHY AND STEREOSCOPIC PIV ...............................................................................................................................................................................................................17619

K. Busa, E. Bryner, J. McDaniel, C. Goyne, C. Smith, G. Diskin

AN ERROR TRANSPORT EQUATION IN PRIMITIVE VARIABLE FORMULATION .............................................................17633X. Tong, E. Luke

A HIGH-RESOLUTION METHOD FOR FLOW SIMULATIONS WITH CARTESIAN MESH METHOD..............................17645Takashi Ishida, Soshi Kawai, Kazuhiro Nakahashi

DELAYED DETACHED EDDY SIMULATION OF A STALL FLOW OVER NACA0012 AIRFOIL USING HIGH ORDER SCHEMES .......................................................................................................................................................................17665

Hongsik Im, Gecheng Zha

WHEN THE EXACT DISCRETE GRADIENT IS NOT THE BEST CHOICE IN OPTIMAL SHAPE DESIGN? .....................17681Alfonso Bueno-Orovio, Carlos Castro, Karthikeyan Duraisamy, Francisco Palacios, Enrique Zuazua

CONTINUOUS ADJOINT APPROACH FOR THE SPALART-ALLMARAS MODEL IN AERODYNAMIC OPTIMIZATION .......................................................................................................................................................................................17695

Alfonso Bueno-Orovio, Carlos Castro, Francisco Palacios, Enrique Zuazua

VALIDATION AND VERIFICATION OF THE NAVIER-STOKES SOLUTIONS OBTAINED FROM THE APPLICATIONS OF THE INTEGRO-DIFFERENTIAL SCHEME .................................................................................................17718

F. Ferguson, M. Dhanasar, N. Dasque

FURTHER ASSESSMENT OF PLASMA ACTUATOR ENHANCEMENT THROUGH ELECTRODE MODIFICATIONS.....................................................................................................................................................................................17733

Eric Stephen, Thomas McLaughlin

RETROSPECTIVE COST ADAPTIVE FLOW CONTROL USING A DIELECTRIC BARRIER DISCHARGE ACTUATOR WITH PARAMETER-DEPENDENT MODELING......................................................................................................17754

Y. Cho, J. Hoagg, D. Bernstein, W. Shyy

PIV STUDY ON STEADY AND PERIODIC-PULSED DIELECTRIC-BARRIER-DISCHARGES .............................................17769Chong Ma, Huaxing Li, Feng Liu, Shijun Luo

EXPERIMENTAL INVESTIGATION OF A SUBORBITAL REUSABLE BOOSTER CONCEPT WITH CANARDS...................................................................................................................................................................................................17785

M. Post, M. Dobransky, W. Shackelford, B. Hellman

EXPERIMENTAL INVESTIGATION OF A SUBORBITAL REUSABLE BOOSTER CONCEPT WITH A BODY FLAP ...............................................................................................................................................................................................17810

Andrew Miller, Roderick Mills, Martiqua Post, Barry Hellman

PART 1: THE WIND TUNNEL MODEL DESIGN AND FABRICATION OF CAL POLY’S AMELIA 10 FOOT SPAN HYBRID WING-BODY LOW NOISE CESTOL AIRCRAFT .................................................................................................17821

K. Jameson, D. Marshall, R. Golden, E. Paciano, R. Englar, R. Gaeta, J. Paterson, D. Mason

PART 2: PREPARATION FOR WIND TUNNEL MODEL TESTING AND VERIFICATION OF CAL POLY’S AMELIA 10 FOOT SPAN HYBRID WING-BODY LOW NOISE CESTOL AIRCRAFT..............................................................17832

K. Jameson, D. Marshall, R. Ehmann, E. Paciano, R. Englar, W. Horne

INVESTIGATION OF ORION CREW EXPLORATION VEHICLE FORWARD BAY COVER SEPARATION CHARACTERISTICS ...............................................................................................................................................................................17844

D. Montes, T. West, T. Yechout

EXPERIMENTAL STUDY OF A NACA 4412 AIRFOIL WITH MOVABLE GURNEY FLAP....................................................17856Mauricio Camocardi, Julio Di Leo, Juan Delnero, Jorge Lerner

TRAILING EDGE FLEXION INFLUENCES LEADING EDGE VORTICES AND AERODYNAMIC FORCES IN FLAPPING WINGS .............................................................................................................................................................................17871

L. Zhao, X. Deng, S. Sane

LIFT GENERATION AND FLOW MEASUREMENTS OF A ROBOTIC INSECT .......................................................................17879Zheng Hu, Bo Cheng, Xinyan Deng

NON-SINUSOIDAL TRAJECTORY OPTIMIZATION OF FLAPPING AIRFOIL USING UNSTEADY ADJOINT APPROACH ............................................................................................................................................................................17887

B. Lee, M. Padulo, M. Liou

A SCALING PARAMETER FOR THE THRUST GENERATION OF FLAPPING FLEXIBLE WINGS. ..................................17902Chang-Kwon Kang, Hikaru Aono, Carlos Cesnik, Wei Shyy

LIFT, DRAG AND FLOW-FIELD MEASUREMENTS AROUND A SMALL ORNITHOPTER .................................................17929R. Alarcon, F. Shu, B. Balasubramaniam

3D FLAPPING WING SIMULATION WITH HIGH ORDER SPECTRAL DIFFERENCE METHOD ON DEFORMABLE MESH.............................................................................................................................................................................17949

Kui Ou, Patrice Castonguay, Antony Jameson

PIV ON SIMPLE MECHANICAL FLAPPING WINGS FOR HOVER-LIKE KINEMATICS......................................................17966Benjamin Hagen, Aaron Altman

SIMULATION OF SPACECRAFT FUEL TANK SELF-PRESSURIZATION USING EULERIAN-LAGRANGIAN METHOD .......................................................................................................................................................................17977

Jaeheon Sim, Chih-Kuang Kuan, Wei Shyy

INTRODUCING SE-FIT: SURFACE EVOLVER - FLUID INTERFACE TOOL FOR STUDYING CAPILLARY SURFACES .................................................................................................................................................................................................17997

Y. Chen, B. Schaffer, M. Weislogel, G. Zimmerli

PROPELLANT QUANTITY GAUGING USING THE RADIO FREQUENCY MASS GAUGE ...................................................18008G. Zimmerli, M. Asipauskas, J. Wagner, J. Follo

TRANSIENT CONVECTION DUE TO IMPOSED HEAT FLUX: APPLICATION TO LIQUID ACQUISITION DEVICES ....................................................................................................................................................................................................18019

W. Duval, D. Chato, M. Doherty

PICOSECOND CARS MEASUREMENTS OF VIBRATIONAL DISTRIBUTION FUNCTIONS IN A NONEQUILIBRIUM MACH 5 FLOW...................................................................................................................................................18041

A. Montello, M. Nishihara, J. Rich, I. Adamovich, W. Lempert

MEASUREMENT OF ELECTRON LOSS RATES IN ATMOSPHERIC PRESSURE AIR BY RADAR REMPI......................18062Arthur Dogariu, Mikhail Shneider, Richard Miles

AERO-OPTICS OF SUPERSONIC BOUNDARY LAYERS ...............................................................................................................18066Stanislav Gordeyev, Eric Jumper, Tim Hayden

INVESTIGATIONS OF SURFACE-CATALYZED RECOMBINATION REACTIONS IN THE MARS ATMOSPHERE..........................................................................................................................................................................................18079

Max Dougherty, Walt Owens, Jason Meyers, Douglas Fletcher

CONFINED AND UNCONFINED LASER-INDUCED SPARKS IN HYDROGEN AT ELEVATED PRESSURES...................18090Stefan Brieschenk, Sean O'Byrne, Harald Kleine

THE AERO-OPTICAL ENVIRONMENT OF A HELICOPTER IN HOVER .................................................................................18102C. Porter, R. Rennie, E. Jumper

EXPERIMENTAL MEASUREMENTS OF AN AIRCRAFT-MOUNTED POD CONCEPT FOR IMPROVED AERO-OPTIC PERFORMANCE............................................................................................................................................................18113

G. Crahan, R. Rennie, E. Jumper

PLASMA ASSISTED IGNITION BELOW SELF-IGNITION THRESHOLD IN METHANE, ETHANE, PROPANE AND BUTANE-AIR MIXTURES........................................................................................................................................18121

L. Wu, J. Lane, N. Cemansky, D. Miller, A. Fridman, A. Starikovskiy

DISCHARGES OVER FLAMMABLE AND DIELECTRIC LIQUIDS .............................................................................................18129A. Alexandrov, V. Chernikov, D. Vaulin, S. Volkov, A. Kostyuk, V. Bychkov, D. Bychkov

COMPACT AND POWER–INTENSIVE CATALYST–FREE PARTIAL OXIDATION REFORMER OF LIQUID FUELS TO SYNGAS .................................................................................................................................................................18140

A. Rakitin, I. Popov, G. Correale, A. Nikipelov, A. Starikovskii

PLASMA-ASSISTED REACTION OF HETEROGENEOUS AL-H2O MIXTURE IN HIGH-SPEED SWIRL FLOW ..........................................................................................................................................................................................................18146

A. Klimov, V. Bityurin, A. Grigorenko, A. Efimov, D. Kutuzov, B. Tolkunov, A. Tsymbal, L. Polyakov

POSITIONING THE INTERNATIONAL SPACE STATION FOR THE UTILIZATION ERA ...................................................18154M. Uhran

FROM MARINE ANIMALS TO PLASMA AERODYNAMICS ........................................................................................................18164N. Yurchenko

A NOVEL INTEGRATOR-LESS ROBUST ADAPTIVE CONTROL SCHEME FOR AEROSPACE TRACKING APPLICATIONS ........................................................................................................................................................................................18178

A. Mannava, S. Balakrishnan

ORION PA-1 THERMAL FLIGHT OPERATIONS AND LESSONS-LEARNED...........................................................................18189J. Gasbarre, D. Buffington, D. Lamb

GRAVITY AND RELATIVISTIC PHENOMENA ...............................................................................................................................18208J. Nissen, Q. Bailey, J. Lipa, H. Paik

TRANSFORMING RESPONSIVE SPACE SENSOR TASKING .......................................................................................................18216E. Miller, J. Hicks, J. Barlow, P. Paulsen

COARSENING IN SOLID-LIQUID MIXTURES: EFFECT OF MICROGRAVITY ACCELERATIONS ON PARTICLE SEDIMENTATION..............................................................................................................................................................18221

E. Gulsoy, K. Wittman, J. Thompson, P. Voorhees

Author Index