r

Due to the rapid development of structural analysis techniques over the last few years there is a lack of comprehensive, up-to-date texts on the subject

This list of references covers a broad range of subjects and includes both basic and advanced methods.

ALLEMANG, R.J.; SHAPTON, W.R. BROWN, D.L.; ALLEMANG, R.J.; ZIMMERMAN, R.; Using Modal Techniques to Guide Acoustic Signa- MERGEAY, M. ture Analysis Parameter Estimation Techniques for Modal Analysis SAE Paper Number 780106, SAE Transactions, Volume SAE Paper Number 790221, SAE Transactions, Volume 87, 1978, 12 pp. 88, 1979, pp. 828-846

ALLEMANG, R.J. BROWN, D.L.; CARBON, G.; RAMSEY, K. Investigation of Some Multiple Input/Output Fre- Survey of Excitation Techniques Applicable to the quency Response Function Experimental Modal Testing of Automotive Structures Analysis Techniques SAE Paper Number 770029, 1977, 16 pp. Doctor of Philosophy Dissertation, Department of Me­chanical Engineering, University of Cincinnati, 1980, 358 CAUGHEY, T.K. pp. Classical Normal Modes in Damped Linear Dynamic

ANDERSON, D.; MILLS, B. Systems - _ , . . ' ' . ' . _ . . Journal of Applied Mechanics, Volume 27, 1960, pp. Multi-Point Excitation Techniques ^ K K

Environmental Engineering, Number 51, 1971, 6 pp.

ARCHER J S CHANG, C.S. Li i ' i w-u *• «« J i * i A Hybrid Computer Controlled Structural Dynamics Natural Vibration Modal Analysis _ J K ' NASA-SP-8012, 1968, 31 pp. , } . 0 . , , A . _ .. .n£tf%

^ Instrument Society of America. Proceedings, 1969, pp. ASHER, G.W. 114~121

A Method of Normal Mode Excitation Utilizing Admit- . u r K I , ~ r-Ar>r»A . A - - . UnbN, J.O.; UAHDA, J.A. tance Measurements ■ ■ * ■ « * L. *■ * * ■ «- ■ •• J i ~ . . , .. .. 0 ,. , ... . , Matrix Perturbation for Analytical Model Dynamics and Aeroelasticity, Proceedings, Institute of . . J

*L A *• , ~ . Af\m ™, TA Improvement the Aeronautical Sciences, 1958, pp. 69-76 AIAA 0 u u -m noo-, *n™ Ann Ann ^ AIAA Paper Number 79-0831, 1979, pp. 428-436

A S H A R M ^ ' W ' *u c « * r* 4t= ^ * COLLINS, J.D.; YOUNG, J.P.; KIEFLING, L. A Note on the Effective Degrees of Freedom of a . . . . ' ' . ' ' . 0 ' . . .... .. w u *• o* * Methods and Application of System Identification in Vibrating Structure Qh k ri V h t" AIAA Journal, Volume 5, Number 4, 1967, pp. 822-824 e ?* *!!? J , ! ' 0 " ( irh t- e + * **.«:

^ K System Identification of Vibrating Structures, ASME, BALLARD, W.C.; CASEY, S.L.; CLAUSEN, J.D. 1972' P P ' 45~71

Vibration Testing with Mechanical Impedance P D A i r , D D

Methods e* ' * i n * ~ . . ,,.. .. . ,nnri Structural Dynamics Sound and Vibration, January, 1969 , , ,.,., / „ n~-, 7 John Wiley & Sons, 527pp.

Solutions for the Multiple Input/Output Problem - ' ... . ' . '. „ _ .. , , ( 0 . , .... .. .. , ,, », . o On Multiple-Shaker Resonance Testing Journal of Sound and Vibration, Volume 44, Number 3, AIA A . ** , . .. , _ . * _ „ . _ow , n 7 , 0 _ nnc AIAA Journal, Volume 12, Number 7, 1974, pp. 924-931 1976, pp. 311-325 > > rr

BROWN D L DAT, R. r* - ' J - „ n ~- « Structural Vibration Test Methods Used by Grinding Dynamics 0 N E R A Doctor of Philosophy Dissertation, Department of Me- ,_ 0 . „ . „ oow . „__ n-. . nl r- ■ ■ i, ■ ■* t r^ ■ *• tn-rn Ann European Space Agency, ESA TT-221, 1975, 27 pp. chanical Engineering, University of Cincinnati, 1976, 400 K K v J> rr PP- DE VEUBEKE, B.F.

BROWN, D.L.; ALLEMANG, R.J. A Variational Approach to Pure Mode Excitation Modal Analysis Techniques Applicable to Acoustic Based on Characteristic Phase Lag Theory Problem Solution Advisory Group for Aerospace Research and Develop-Inter-Noise 78, 1978, pp. 909-914 ment, AGARD-R-39, 1956, 35 pp.

BO 0112-11

DE VEUBEKE, B.F. IBRAHIM, S.R.; GOGLIA, G.L. Comment on 'On Multiple-Shaker Resonance Model Identification of Structures from the Respons-Testing' es and Random Decrement Signatures AIAA Journal, Volume 13, Number 5, 1975, pp. 702-704 NASA-CR-155321, 1977

EWINS, D.J. IBRAHIM, S.R. Whys and Wherefores of Modal Testing. The Use of Random Decrement Technique for Identi-Journal of the Society of Environmental Engineers, Sep- fication of Structural Modes of Vibration tember 1979, 24pp. AIAA Paper Number 77-368, 1977, 10 pp.

EWINS, D.J. IMES, R.S.; JENNINGS, W.P.; OLSEN, N.L. Measurement and Application of Mechanical Imped- The Use of Transient Testing Techniques in Boeing ance Data. YC-14 Flutter Clearance Program Journal of the Society of Environmental Engineers, De- AIAA Paper Number 78-505, 1978 cember 1975 - June 1976, 32pp.

JENNINGS, W.P.; OLSEN, N.L.; WALTER, M.J. EWINS, D.J. Transient Excitation and Data Processing Tech-

Estimation of Resonant Peak Amplitudes. niques Employing the Fast Fourier Transform for Journal of Sound and Vibration, Vol. 43, No. 4, 1975. Aeroelastic Testing

Flutter Testing Techniques, NASA-SP-415, 1976, pp. EWINS, D.J.; GLEESON, P.T. 77-113

A Method for Modal Identification of Lightly Damped Structures. JOHNSTON, G.D.; COLEMAN, A.D. Journal of Sound and Vibration, Vol. 84, No. 1, 1982. Modal Test of Shuttle Engine Nozzle.

Proceedings of the Society for Experimental Stress EWINS, D.J.; SAINSBURY, M.G. Analysis, 1983.

Mobility Measurements for the Vibration Analysis of Connected Structures KENNEDY, C.C.; PANCU, CD.P. Shock and Vibration Bulletin, Volume 42, Part 1, 1972, Use of Vectors in Vibration Measurement and pp. 105-121 Analysis

Journal of Aeronautical Sciences, Volume 14, Number FAVOUR, J.D.; MITCHELL, M.L.; OLSEN, N.L. 11, 1947, pp. 603-625

Transient Test Techniques for Mechanical Imped­ance and Modal Survey Testing KLOSTERMAN, A. Shock and Vibration Bulletin, Volume 42, Part 1, 1972, On the Experimental Determination and Use of Modal pp. 71-82 Representations of Dynamic Characteristics

Doctor of Philosophy Dissertation, Department of Me-FERRANTE, M.; STAHLE, C.V.; BRESKMAN, D.G. chanical Engineering, University of Cincinnati, 1971, 184

Spacecraft Modal Testing Using Single Point Ran- pp. dom and Multi-Shaker Sine Techniques Proceedings, Institute of Environmental Sciences, 1979, KLOSTERMAN, A.; MCCLELLAND, W.A. 8 pp. Combining Experimental and Analytical Techniques

for Dynamic System Analysis FLANNELLY, W.G.; LANG, G.F. Structural Dynamics Research Corporation, 1973,20 pp.

Modal Analysis for Managers Sound and Vibration, November, 1979, pp. 18-23 KLOSTERMAN, A.

A Combined Experimental and Analytical Procedure HALVORSEN, W.G.; BROWN, D.L. for Improving Automotive System Dynamics

Impulse Technique for Structural Frequency Re- SAE Paper Number 720093, 1972 sponse Testing Sound and Vibration, November, 1977, pp. 8-21 KLOSTERMAN, A.; LEMON, J.R.

Dynamic Design Analysis via the Building Block IBANEZ, P. Approach

Force Appropriation by Extended Asher's Method Shock and Vibration Bulletin, Volume 42, Part 1, 1972, SAE Paper Number 760873, 1976, 11 pp. pp. 97-104

IBANEZ, P.; SPENCER, R.B. KLOSTERMAN, A. Experience with a Field Computerterized Vibration Modal Surveys of Weakly Coupled Systems Analysis System SAE Paper Number 760876, 1976 SAE Paper Number 791074, 1979, 12 pp.

KLOSTERMAN, A.; ZIMMERMAN, R. IBRAHIM, S.R. Modal Survey Activity via Frequency Response

Limitations on Random Input Forces in Randomdec Functions Computation for Modal Identification SAE Paper Number 751068, 1975 Shock and Vibration Bulletin, Volume 50, Part 3, 1980, pp. 99-112 KLOSTERMAN, A.; MCCLELLAND, W.A.; SHERLOCK, J.E.

Dynamic Simulation of Complex Systems Utilizing IBRAHIM, S.R. Experimental and Analytical Techniques

Modal Confidence Factor in Vibration Testing ASME Paper Number 75-WA/AERO-9, 1975 Shock and Vibration Bulletin, Volume 48, Part 1, 1978, pp. 183-198

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KRAMER, J.A.; BENEDICT, B.K. POTTER, D.K. Experimental-analytical Modal Analysis Interface Flight Flutter and Vibration Testing Program. Institute of Mechanical Engineers, Conference Pubiica-Proceedings of the Society for Experimental Stress tion 1976-2, 1976, pp. 9-16 Analysis, 1983.

POTTER, R.W. LEPPERT, E.L.; LEE, S.H.; DAY, F.D.; CHAPMAN, P C , Matrix Formulation of Multiple and Partial Coherence

WADA, B.K. Journal of the Acoustic Society of America, Volume 61, Comparison of Modal Test Results: Multipoint Sine Number 3, 1977, pp. 776-781 Versus Single-Point Random SAE Paper Number 760879, 1976, 15 pp. POTTER, R.W.; RICHARDSON, M.

Mass, Stiffness, and Damping Matrices from Mea-LEWIS, R.C.;WRISLEY, D.L. sured Modal Properties

A System for the Excitation of Pure Natural Modes of Instrument Society of America. ISA-74-630, 1974, 5 pp. Complex Structures Journal of Aeronautical Sciences, Volume 17, Number POTTER, R.W. 11, 1950, pp. 705-722 A General Theory of Modal Analysis for Linear

Systems LINK, M.; VOLLAN, A. Shock and Vibration Digest, Volume 7, Number 11, 1975,

Identification of Structural System Parameters from 8 pp. Dynamic Response Data Zeitschrift fur Flugwissenschaften, Volume 2, Number 3, POTTER, R.W. 1978, pp. 165-174 Compilation of Time Windows and Line Shapes for

Fourier Analysis LINSCOTT, B.S.; SHAPTON, W.R.; BROWN, D.L. Hewlett-Packard Company, 1972, 26 pp.

Tower and Rotor Blade Vibration Test Results for a 100-Kilowatt Wind Turbine RAMSEY, K. NASA-TM-X-3426, 1976, 38 pp. Effective Measurements for Structural Dynamics

Testing: Part I MARTZ, J.W.; LEIST, T. Sound and Vibration, November 1975

Application of Modal Testing Techniques to Solve Vibration Problems in Machinery Supporting RAMSEY, K. Structures Effective Measurements for Structural Dynamics ASME Paper Number 77-DET-16, 1977, 12 pp. Testing: Part II

Sound and Vibration, April 1976 MEIROVITCH, L.

Analytical Methods in Vibration RAMSEY, K.A.; RICHARDSON, M. The Macmillan Company, 555 pp. Making Effective Transfer Function Measurements

for Modal Analysis MIRIMAND, N.; BILLAUD, J.F.; LELEUX, F.; KRENEVEZ, J.P. Hewlett-Packard Company, 1975

Identification of Structural Modal Parameters by Dy­namic Tests at a Single Point RICHARDSON, M. Shock and Vibration Bulletin, Volume 46, Part 5, 1976, Modal Analysis Using Digital Test Systems pp. 197-212 Seminar on Understanding Digital Control and Analysis

I I n in Vibration Test Systems (part 2), 1975, pp. 43-64

Signal Processing with the Fast Fourier Transform RICHARDSON M • POTTER R Analyzer Identification of the Modal Properties of an Elastic Proceedings of the Society for Experimental Stress structure from Measured Transfer Function Data Analysis, 1983 Instrument Society of America, ISA ASI 74250, 1974, pp.

MITCHELL, L.D. 239-246 Improved Methods for the FFT Calculations of the Frequency Response Function RICHARDSON, M.; POTTER, R. Journal of Mechanical Design, April 1982, Vol. 104 Viscous vs. Structural Damping in Modal Analysis

46th Shock and Vibration Symposium, 1975, 8 pp. NIEDBAL, N.

State of the Art of Modal Survey Test Techniques RICHARDSON, M.; KNISKERN, J. Modal Survey, SP-121, European Space Agency 1976, Identifying Modes of Large Structures from Multiple pp 126-128 Input and Response Measurements

SAE Paper Number 760875, 1976, 12 pp. OLSEN, N.L.; WALTER, M.J.

747 Shuttle Carrier Aircraft/Space Shuttle Orbiter RUSSELL, R.H.; DEEL, J.C. Mated Ground Vibration Test: Data via Transient Ex- Modal Analysis: Trouble-Shooting to Product Design citation and Fast Fourier Transform Analysis Sound and Vibration, November 1977, pp. 22-28 SAE Paper Number 770970, 1977, 12 pp.

SMITH, S.; STROUD, R.C.; HAMMA, G.A.; HALLAUER, W.L.; PETERSON, E.L.; KLOSTERMAN, A.L. YEE, R.C.

Obtaining Good Results from an Experimental Modal MODALAB - A Computerized Data Acquisition and Survey Analysis System for Structural Dynamic Testing Society of Environmental Engineers, Symposium, Lon- Instrument Society of America Proceedings, Volume 12, don, England, 1977, 22 pp. 1975, pp. 183-189

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SNOEYS, R.; ROESEMS, D.; VANDEURZEN, U.; TAYLOR, G.A.; GAUKROGER, D.R.; SKINGLE, C.W. VANHONACKER, P. MAMA - A Semi-Automatic Technique for Exciting Surveys of Modal Analysis Applications the Principal Modes of Vibration of Complex Annals of the CIRP, Volume 28, Number 2, 1979, 14 pp. Structures

Aeronautical Research Council, ARC-R/M-3590, 1967, SNYDER, V.W. 20 pp.

Structural Modification and Modal Analyses. Proceedings of the Society for Experimental Stress VAN BRUSSEL H. Analysis, 1983. Comparative Assessment of Harmonic, Random,

Swept Sine, and Shock Excitation Methods for the SPRINGER, W.T.; LAWRENCE, K.L. Identification of Machine Tool Structures with Rotat-

Fracture Healing Estimates Based on the Structural ing Spindles Frequency Response Function. Catholic University of Leuven, Leuven, Belgium, 1975, 6 Proceedings of the Society for Experimental Stress pp. Analysis, 1983.

VAN KARSEN, C.; ALLEMANG, R. J. STAHLE, C.V.; FORLIFER, W.R. Single and Multiple Input Modal Analysis for Auto-

Ground Vibration Testing of Complex Structures motive Structures. Flight Flutter Testing Symposium, NASA-SP-385, 1958, Proceedings of the Society for Experimental Stress pp. 83-90 Analysis, 1983.

STAHLE, C.V., JR. VARIOUS AUTHORS. Phase Separation Technique for Ground Vibration Proceedings of the 1st International Modal Analysis Testing Conference. Union College, New York, 1982. Aerospace Engineering, July 1962, 8 pp.

VARIOUS AUTHORS. STAHLE, C.V. Proceedings of the 2nd International Modal Analysis

Modal Test Methods and Applications Conference Vols I & II. Union College, New York, 1984. Journal of Environmental Sciences, Jan/Feb 1978, 4 pp.

WALGRAVE, S.C.; EHLBECK, J.M. STRESAU, S.S. Understanding Modal Analysis.

Mode Test of a Wing Pair of the HARM Missile. SAE Paper No. 780695, 1978. Proceedings of the Society for Experimental Stress Analysis, 1983. YOUNG, J.P.; ON, F.J.

Mathmafical Modeling via Direct Use of Vibration STROUD, R.C.; BONNER, C.J.; CHAMBERS, G.J. Data

Modal Testing Options for Spacecraft Developments SAE Paper Number 690615, 1969 SAE Paper Number 781043, 1978, pp. 3922-3936

ZAVERI, K. STROUD, R.C.; SMITH, S.; HAMMA, G.A. Modal Analysis of Large Structures - Multiple Exciter

MODALAB - A New System for Structural Dynamic Systems Testing Bruel & Kjaer, 1984, 124 pp. Shock and Vibration Bulletin. Volume 46, 1976, pp. 153-175 ZIMMERMAN, H.; COLLMANN, D.; NATKE, H.G.

Experience Gained in Adjusting the Mathmatical STRUCTURAL MEASUREMENT SYSTEMS Model of the VFW 614 Short Haul Aircraft by Use of

An Introduction to Structural Dynamics Modification Measured Eigenfrequencies Structural Measurement Systems, November 1979, 56 Zeitschrift fur Flugwissenschaften, Volume 25, Number pp. 5, 1977, pp. 278-285

SU, Y.W.T.; CRAIG, R.R. A Simulation Study of Multiple-Shaker Resonance Testing University of Texas at Austin, Engineering Mechanics Research Laboratory, EMRL Report Number 1094, 1972, 77 pp. Compiled September 1984