4 Year B.Tech Program (Aeronautical Engineering) Structure for admission batch of 2015-16
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SCHEME OF INSTRUCTION AND EVALUATION I - VIII SEMESTER OF B.TECH. DEGREE PROGRAMME
Branch-Aeronautical Engineering
First Year Engineering
First Semester
Theory Practical Code Course Name Hours/
Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
BS Mathematics-I 3-1 4 100 50 - - - BS Chemistry/ Physics 3-0 3 100 50 2 1 50 ES Basics of Electronics /
Basic Electrical Engineering
3-0 3 100 50 2 1 50
ES Mechanics/ Thermodynamics
3-0 3 100 50
ES Programming in ‘c” 3-0 3 100 50 2 2 50 HS English Communication
Skill 3-0 2 100 50 2 1 50
ES Engineering Workshop/ Engineering Drawing
4 2 100
Total 16 18 600 300 18 7 300
Total Marks: 1200
Total Credits: 25
Second Semester
Theory Practical Code Course Name Hours/
week L/T
Credit Theory
University marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
BS Mathematics-II 3-1 4 100 50 - - - BS Chemistry/ Physics 3-0 3 100 50 2 1 50 ES Basics of Electronics /
Basic Electrical Engineering
3-0 3 100 50 2 1 50
ES Mechanics/ Thermodynamics
3-1 3 100 50
ES Data Structure Using ‘C”
3-0 3 100 50 2 2 50
HS Business communication
3-0 2 100 50 2 1 50
ES Engineering Workshop/ Engineering Drawing
4 2 100
MC NSS/NCC - - - -
Total 17 18 600 300 14 7 300
Total Marks: 1200
Total Credits: 25
4 Year B.Tech Program (Aeronautical Engineering) Structure for admission batch of 2015-16
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Second Year Engineering
Third Semester
Theory Practical Code Course Name Hours/
Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
PC Fluid Mechanics & Heat flow
3-0 3 100 50 2 1 50
PC Aero Thermodynamics 3-0 3 100 50 2 1 50 PC Strength of Materials 3-0 3 100 50 2 1 50 PC Elements of
Aeronautics 3-0 3 100 50 2 1 50
PC Avionics 3-1 4 100 50 HS Engineering Economics/
Organizational Behavior 2-1 3 100 50
Total 19 19 600 300 8 4 200
Total Marks: 1100
Total Credits: 23
For Honours and Minor Specialization
4 4 100 50
Fourth Semester
Theory Practical Code Course Name Hours/
Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
HS Purely Applied Mathematics for Specific Branch of Engineering
3-0 3 100 50
PC Aerodynamics-I 3-0 3 100 50 2 1 50 PC Aircraft Materials &
Production 3-0 3 100 50 2 1 50
PC Aircraft Structures-I 3-0 3 100 50 2 1 50 PC Propulsion-I 3-0 3 100 50 2 1 50 HS Engineering Economics/
Organizational Behavior 2-1 3 100 50
*Skill Project and Hands on
6 3 100
Total 18 18 600 300 14 7 300
Total Marks: 1200
Total Credits: 25
For Honours and Minor Specialization
4 4 100 50
*College should conduct at least one NSDC program under this category.
4 Year B.Tech Program (Aeronautical Engineering) Structure for admission batch of 2015-16
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Third Year Engineering
Fifth Semester
Theory Practical
Code Course Name Hours/Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
PC Aircraft Structures-II 3-0 3 100 50 2 1 50
PC Aerodyanmics-II 3-0 3 100 50 2 1 50
PC Aircraft Performance 3-0 3 100 50 2 1 50
PE Finite Element Method/Experimental stress Analysis/Computational fluid Dynamics
3-1 4 100 50
OE Total Quality Management/Production Management/Operational Research
3-1 4 100 50
PC Advance Lab-I 8 4 200
Total 17 17 500 250 14 7 350
Total Marks: 1100
Total Credits: 24
For Honours and Minor Specialization
4 4 100 50
4 Year B.Tech Program (Aeronautical Engineering) Structure for admission batch of 2015-16
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Sixth Semester
Theory Practical Code Course Name Hours/
Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
PC Aircraft Stability & Control
3-0 3 100 50 2 1 50
PC Propulsion-II 3-0 3 100 50 2 1 50 PE Composite Material &
Structure/Non-Destructive Testing/High Temperature Materials
3-1 4 100 50
PE Aircraft General Engineering & Maintenance/Flight Schedule & Operation/Airport Planning &Management
3-1 4 100 50
MC & GS
Environmental Science & Engineering
3-0 3 100 50
OE Industrial Lecture # 3 1 50 HS Presentation Skill & Skill
for Interview # # 2-0 1 50 4 2 100
MC Yoga 2 1 50
Total 19 18 500 300 13 7 300
Total Marks: 1100
Total Credits: 24
For Honours and Minor Specialization
4 4 100 50
# To be conducted by the Training & Placement department by inviting experts from the industry. No academician to be called.
Record may be asked by the University for verification. Evaluation to be done by the TPO.
# # To be conducted by the Training & Placement department of the College.
4 Year B.Tech Program (Aeronautical Engineering) Structure for admission batch of 2015-16
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Final Year Engineering
Seventh Semester
Theory Practical Code Course Name Hours/
Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
GS Nano Science & Bio Technology
3-1 4 100 50
PE Wind Tunnel Techniques/Experimental Fluid Dynamics/Industrial Aerodynamics
3-1 4 100 50
PE Combustion/Space Mechanics/Helicopter Engineering
3-1 4 100 50
OE Soft Computing */ Other subjects
3-1 4 100 50
PC Advance Lab-II/ Project 8 4 200 Projects on Internet of
Things 8 4 200
Total 16 16 400 200 16 8 400
Total Marks: 1000
Total Credits: 24
For Honours and Minor Specialization
4 4 100 50
*Student can choose from any department but subject must be running in that
semester.
Eighth Semester
Training cum Project Evaluation Scheme Code Course Name Hours/
Week L/T
Credit Theory
Total Marks
Marks
Industrial Training cum Project/ Entrepreneurship Training cum Project / Stratup Training cum Project
30 20 1000 Evaluation by the Industry / Training Organisation
500
Evaluation by the Institute (Report & Institute Viva)
500
Total 30 20 1000 1000 Total Marks:1000 Total Credits:20
4 Year B.Tech Program (Aeronautical Engineering) Structure for admission batch of 2015-16
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Note- Minimum Pass Mark from Industry Evaluation is 300 (i.e. 60%).
Distribution of Credit Semester wise: Semester Credit
First 25
Second 25
Third 23
Fourth 25
Fifth 24
Sixth 24
Seventh 24
Eighth 20
-------------------------------------
Total 190
Internal Evaluation Scheme
Attendance & Class Interaction 05
Assignment 05
Surprise Test 05
Quiz 05
Class Test I & II 30
Total 50
Class Test Time(Hrs.): 1
Pass Mark in Internal is 50% of total marks i.e. 25
External Evaluation Scheme
University Semester Examination of 3 Hours duration.
Pass mark will be 35% which means students have to score 35 out of 100.
Practical/Sessional Evaluation Scheme
Pass mark will be 50% which means students have to score 25 out of 50.
Evaluation Scheme
Attendance & Daily Performance -10
Lab Record - 10
Lab Quiz - 05
Final Experiments & Viva – 25
-------------------------------------------------------
Total=50
All Lab examinations are to be completed one week before the end semester
examination and marks are to be displayed on the college notice board.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
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III-V SEMESTER DETAILED SYLLABUS
OF
B.TECH. DEGREE PROGRAMME
for
ADMISSION BATCH 2015-16
BRANCH-AERONAUTICAL ENGINEERING
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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Second Year Engineering
Third Semester
Theory Practical Code Course Name Hours/W
eek L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
PC Fluid Mechanics & Heat flow
3-0 3 100 50 2 1 50
PC Aero Thermodynamics 3-0 3 100 50 2 1 50 PC Strength of Materials 3-0 3 100 50 2 1 50 PC Elements of Aeronautics 3-0 3 100 50 2 1 50
PC Avionics 3-1 4 100 50 HS Engineering Economics/
Organizational Behavior 2-1 3 100 50
Total 19 19 600 300 8 4 200
Total Marks: 1100
Total Credits: 23
For Honours and Minor Specialization
4 4 100 50
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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Semester : 3rd
--------------
1. PAE3D001 Honours(O2) Aircraft Rules & Regulation- CAR I & II 4-0-0 4
2. PAE3D002 Honours(O2) Airport Planning & Management 4-0-0 4
3. PAE3D003 Honours(O2) Flight Schedule & Operation 4-0-0 4
4. PEK3E001 HS(O1) Engineering Economics 3-0-0 3
5. POB3E002 HS(O1) Organizational Behavior 3-0-0 3
6. PAE3G001 Minor(O3) Elements of Aeronautics 4-0-0 4
7. PAE3I001 PC(CP) Avionics 4-0-0 4
8. PAE3I101 PC(CP) Fluid Mechanics & Heat flow 3-0-1 4
9. PAE3I102 PC(CP) Aero Thermodynamics 3-0-1 4
10. PAE3I103 PC(CP) Strength of Material 3-0-1 4
11. PAE3I104 PC(CP) Elements of Aeronautics 3-0-1 4
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B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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PAE3I101 FLUID MECHANICS AND HEAT FLOW
UNIT I. Fluid properties And Fluid Statics:
Units & Dimensions. Properties of fluids – Specific gravity, specific weight, viscosity, compressibility, vapour pressure and gas laws – capillarity and surface tension. Pascal„s law, pressure variation with temperature, density and altitude. Hydrostatic law, piezometer, simple and differential manometers, pressure gauges, total pressure and center of pressure of plane, vertical and inclined surfaces. Buoyancy and stability of floating bodies.
UNIT II. Kinematics and Dynamics:
Stream line, path line, streak line, stream tube. Classification of flows: steady, unsteady, uniform, non-uniform, laminar, turbulent, rotational, irrotational flows. One, Two and Three dimensional flows. Continuity equation in 3D flow. Surface and Body forces. Euler„s and Bernoulli„s equations derivation, Navier–Stokes equation (explanation only). Momentum equation. Minor losses in pipes in series and parallel. Total energy line and hydraulic gradient line.
UNIT III. Flow Measurement: Flow measurement through Venturimeters and Orifice meter. Flow through notches and weirs, Viscometers, Pitot tube, U tube manometer, Muly tube manometer, Hotwire Anemometers, pressure gauge, velocity measurement in flow, flow through nozzles.
UNIT IV. Similitude and Boundary layer
Similarity laws, distorted models, Laminar flow though circular conduits and circular annuli. Boundary layer concepts. Boundary layer thickness. Hydraulic and energy gradient. Darcy – Weisbach equaition. Friction factor and Moody diagram.
UNIT V. Heat flow Basic heat transfer process, Steady state conduction through- plan walls, cylindrical wall and spherical wall. Classification of convection heat transfer, Basic Boundary layer heat taransfer aplyied to forced convection, natural convection, Basic laws of radiation heat transfer TEXT BOOKS:
1. Fluid Mechanics Hydraulics and Hydraulics Machines, Modi & Seth, Standard Publications, New Delhi. 2. Engineering Fluid Mechanics by K.L.Kumar, S.Chand &Co.. 3. Er. R. K. Rajput, Heat and Mass Transfer, S.Chand &Co..
REFERENCES:
1. Fluid Mechanics, Frank M. White, Tata Mc-Grawhill. 2. Fluid Mechanics, John F.Dauglas, Pearson Educations publishers 3. Fluid Mechanics & Hydraulic Machines, D. Ramadurgaiah, New age publishers2005.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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PAE3I102 AERO THERMODYNAMICS
.
UNIT I. BASIC THERMODYNAMICS
Systems, Zeroth Law, First Law - Heat and work transfer in flow, Second law, Clausius statement - concept of entropy entropy change in non-flow processes.
UNIT II. AIR CYCLES
Otto, Diesel, Dual combustion and Brayton combustion cycles – Air standard efficiency - Mean effective pressure – Actual and theoretical PV diagrams of two stroke and four stroke IC Engines, cycle for Jet propulsion and Rocket Propusion.
UNIT III. THERMODYNAMICS OF ONE DIMENSIONAL FLUID FLOW
Application of continuity, momentum and energy equations- Rankine cycle - Isentropic flow of ideal gases through nozzles - Simple jet propulsion system - Thrust rocket motor – Specific impulse.
UNIT IV. REFRIGERATION AND AIR COMPRESSORS
Principles of refrigeration, Air conditioning - Heat pumps - Vapour compression - Vapour absorption types - Coefficient of performance,. Classification and working principle of compressors
UNIT V. STOICHIOMETRY, FUELS AND COMBUSTION
Basic of Stoichiometry in chemical reaction, Limiting reactant, exess rectatnt, , Clasification of fuels, Combustion reaction, fuel-air ratio, Aplication of Stoichiometry in combustion calculation
TEXT BOOKS
1. Rathakrishnan, E, “Fundamentals of Engineering Thermodynamics”, Prentice – Hall, India, 2000
2. Nag. P.K., “Engineering Thermodynamics”, Tata McGraw-Hills Co., Ltd., Seventh Edn., 1993
3. Yunus A.Cengal. “Thermodynamics an Engineering Approach”, Tata McGraw-Hill Co. Ltd., 3rd Edition, 2002.
4 D. P. Mishra, Fundamentals of Combustion, Prentice Hall of India, New Delhi, revised edition, 2010.
5 v. Ganesan, Internal Combustion Engines, Tata McGraw-Hills Co
REFERENCES
1. Mayhew, A. and Rogers, B., “Engineering Thermodynamics”, Longman Green & Co. Ltd., London, E.L.B.S. Edition, 1990.
2. Van Wylen, G.J. and Sonntag, R.E., “Fundamentals of Classical Thermodynamics (S.I.Version)”, Second Edition, 1986.
3. Bacon, D.H., “Engineering Thermodynamics”, Butterworth & Co., London, 1989. 5. D. P. Mishra, Engineering Thermodynamics, Cengage Learning India Pvt. Ltd, 2011.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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PAE3I103 STRENGTH OF MATERIALS
UNIT I. BASICS AND AXIAL LOADING
Stress and Strain – Hooke‟s Law – Elastic constants and their relationship– Statically determinate cases - statically indeterminate cases –composite bar. Thermal Stresses – stresses due to freely falling weight.
UNIT II. STRESSES IN BEAMS
Shear force and bending moment diagrams for simply supported and cantilever beams- Bending stresses in straight beams-Shear stresses in bending of beams with rectangular, I & T etc cross sections-beams of uniform strength UNIT III. DEFLECTION OF BEAMS
Double integration method – McCauley‟s method - Area moment method – Conjugate beam method-Principle of super position-Castigliano‟s theorem and its apllication UNIT IV. TORSION
Torsion of circular shafts - shear stresses and twist in solid and hollow circular shafts – closely coiled helical springs.
UNIT V. BI AXIAL STRESSES
Stresses in thin circular cylinder and spherical shell under internal pressure – volumetric Strain. Combined loading – Principal Stresses and maximum Shear Stresses - Analytical and Graphical methods.
TEXT BOOKS
1. Nash William – “Strength of Materials”, TMH, 1998 2. Timoshenko.S. and Young D.H. – “Elements of strength materials Vol. I and Vol.
II”., T. Van Nostrand Co-Inc Princeton-N.J. 1990.
REFERENCES
1. Dym C.L. and Shames I.H. – “Solid Mechanics”, 1990.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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PAE3I104 ELEMENTS OF AERONAUTICS
UNIT I HISTORY OF FLIGHT Balloon flight – ornithopters - early airplanes by wright brothers, biplanes and monoplanes, developments in aerodynamics, materials, structures and propulsion over the years.
UNIT II BASICS OF FLIGHT MECHANICS Physical properties and structure of the atmosphere, temperature, pressure and altitude relationships, newton‟s law of motions applied to aeronautics - evolution of lift, drag and moment. aerofoils, mach number, maneuvers.
UNIT III AIRCRAFT CONFIGURATIONS Different types of flight vehicles, classifications. components of an airplane and their functions. conventional control, powered control, basic instruments for flying - typical systems for control actuation.
UNIT IV AIRPLANE STRUCTURES AND MATERIALS General types of construction, monocoque, semi-monocoque and geodesic constructions, typical wing and fuselage structure. metallic and non-metallic materials, use of aluminium alloy, titanium, stainless steel and composite materials. stresses and strains – hooke‟s law – stress - strain diagrams - elastic constants.
UNIT V POWER PLANTS Basic ideas about piston, turboprop and jet engines - use of propeller and jets for thrust production - comparative merits, principles of operation of rocket, types of rockets and typical applications, exploration into space.
TEXT BOOKS: 1. Anderson, J.D., “Introduction to Flight”, McGraw-Hill, 1995. 2. Stephen. A. Brandt, "Introduction to Aeronautics: A design perspective" American Institute of
Aeronautics & Astronautics,1997
REFERENCES: 1. Kermode, A.C., “Mechanics of Flight”, Himalayan Book, 1997
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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PAE3I001 AVIONICS
OBJECTIVE
To introduce the basic concepts of navigation & communication systems of aircraft.
UNIT I INTRODUCTION TO AVIONICS
Need for Avionics in civil and military aircraft and space systems – Integrated Avionics system –
Typical avionics sub systems – Design approaches and recent advances - Application
Technologies.
UNIT –II FLIGHT DECK AND COMMUNICATION SYSTEMS
Flight deck display technologies – CRT, LED, LCD, Touch screen – Head up display – Electronic
instrumentation systems. Aircraft audio systems basic – audio transmitter and receiver principles – VHF
communication system – UHF communication systems.
UNIT III DIGITAL AVIONICS ARCHITECTURE
Avionics system architecture– salient features and applications of Data buses MIL–STD 1553 B–
ARINC 429–ARINC 629
UNIT-IV RANGING AND POSITIONG SYSTEMS
VHF Omni range – VOR receiver principles – distance maturity equipment – principles of operation
– Instrument landing system – localizer and glide slope. Global positioning system principles –
triangulation – position accuracy – applications in aviation.
UNIT V AUTO FLIGHT SYSTEM
Automatic flight control systems – fly by wire and fly by light technologies – flight director systems – flight
management systems- Utility systems Reliability and maintainability - Certification
TEXT BOOKS
1. Elements of electronic navigation, N.S.Nagaraja, Tata Mc Graw Hill, 1995.
2. Avionic systems Operation and maintenance, Janes W.Wasson,
Jeppesen Sandersen Training products (Sterling Book House, Mumbai),1994.
REFERENCES
1. Introduction to Avionics, Dala R. Cundy, Rich S. Brown, Parson
2. Principle of Avionics, Albert Hel frick, Avionics Communications Inc., 2000.
3. Aircraft Instrumentation and Integrated systems EHJ Pallet, Longman Scientific Technical (Sterling Book House, Mumbai) 1996.
4. Aircraft Radio Systems, J.Powell, Pitman publishers, 1998.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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Strength of Materials LABORATORY
LIST OF EXPERIMENTS
1. Brinell Hardness test
2. Rockwell Hardness test
3. Tension test
4. Torsion test
5. Izod Impact test
6. Charpy Impact test
7. Reverse plate bending Fatigue test
8. Rotating Beam Fatigue test
9. Testing of springs
10. Block Compression Test
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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Fluid Mechanics and Heat Flow LABORATORY
(Common to Aeronautical, Automobile, Mech & Prod)
OBJECTIVE
To study the flow measurement and the performance of fluid machinery
LIST OF EXPERIMENTS
1. Calibration of venturimeter
2. Pressure measurement with pitot static tube
3. Determination of pipe flow losses.
4. Verification of Bernoulli‟s theorem
5. Flow visualization by Heleshaw apparatus
6. Performance test on centrifugal pumps
7. Performance test on reciprocating pumps
8. Determination of Viscosity of a Fluid
9. Conduction through multy layer wall
10. Natural convection
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 3rd Semester
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Aero Engineering LABORATORY
OBJECTIVE
To enhance the basic knowledge in applied thermodynamics
LIST OF EXPERIMENTS
1. Performance test on a 4-stroke engine
2. Valve timing of a 4 – stroke engine and port timing of a 2 stroke engine
3. Determination of effectiveness of a parallel flow heat exchanger
4. Determination of effectiveness of a counter flow heat exchanger
5. Determination of heating value of a fuel
6. COP test on a vapour compression refrigeration test rig
7. COP test on a vapour compression air-conditioning test rig
8. Determination of specific heat of solid
9. Determination of Thermal Conductivity of solid.
10. Determination of Thermal Resistance of a Composite wall.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
4 Year B.Tech(Aeronautical Engineering )Program Structure for admission batch of 2015-16
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Fourth Semester
Theory Practical
Code Course Name Hours/Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
HS Applied Mathematics III 3-0 3 100 50
PC Aerodynamics-I 3-0 3 100 50 2 1 50
PC Aircraft Materials & Production
3-0 3 100 50 2 1 50
PC Aircraft Structures-I 3-0 3 100 50 2 1 50
PC Propulsion-I 3-0 3 100 50 2 1 50
HS Engineering Economics/ Organizational Behavior
2-1 3 100 50
*Skill Project and Hands on
6 3 100
Total 18 18 600 300 14 7 300
Total Marks: 1200
Total Credits: 25
For Honours and Minor Specialization
4 4 100 50
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
4 Year B.Tech(Aeronautical Engineering )Program Structure for admission batch of 2015-16
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Semester : 4th
--------------
1. PAE4D001 Honours(O2) Airframe Repair & Maintenance 4-0-0 4
2. PAE4D002 Honours(O2) Boundary Layer Theory 4-0-0 4
3. PAE4D003 Honours(O2) Theory of Plates & Shells 4-0-0 4
4. PAE4E001 HS(CP) Applied Mathematics III 3-0-0 3
5. PEK4E002 HS(O1) Engineering Economics 3-0-0 3
6. POB4E003 HS(O1) Organizational Behavior 3-0-0 3
7. PAE4G001 Minor(CP) Aerodynamics-I 4-0-0 4
8. PAE4I101 PC(CP) Aerodynamics-I 3-0-1 4
9. PAE4I102 PC(CP) Aircraft Materials & Production 3-0-1 4
10. PAE4I103 PC(CP) Aircraft Structures-I 3-0-1 4
11. PAE4I104 PC(CP) Propulsion - I 3-0-1 4
12. PAE4I201 PC(CP) Skill Project and Hands on 0-0-3 3
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B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
4 Year B.Tech(Aeronautical Engineering )Program Structure for admission batch of 2015-16
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PAE4E001 Applied Mathematics - III
Module-I
Complex Analysis:
Analytic function, Cauchy-Riemann equations, Complex integration: Line integral in the complex plane,
Cauchy’s integral theorem, Cauchy’s integral formula, Derivatives of analytic functions, Taylor’s series,
Maclaurin’s series, Laurent’s series, Singularities and zeros.
Module-II
Complex Analysis:
Residue integration method, evaluation of real integrals
Numerical Methods: Errors of numerical results, error propagation,., Lagrange Interpolation, Newton divided difference
interpolation, Newton’s forward and backward interpolation, Spline interpolation.
Module-III
Numerical Methods:
Numerical integration: The trapezoidal rule, The Simpson’s rules, Gauss Integration formulas.
Solution of ordinary differential equation: Euler’s method, Improvement of Euler’s method, Runge-Kutta
methods, multi step methods, Methods for system and higher order ordinary differential equations.
Module-IV
Probability Theory and Its Applications: Probability, Random variables, Probability distributions, Mean
and variance; Features of Probability Distribution: Binomial, Poisson, Uniform and Normal distribution,
Distribution of several random variables.
Statistical Techniques and Its Applications: Scope of Statistics, Random sampling, Sampling Distribution,
Correlation analysis, Regression Analysis, Fitting Straight Lines, Estimation of Parameters, Statistical
Hypothesis.
Text books: 1. E. Kreyszig,” Advanced Engineering Mathematics:,Tenth Edition, Wiley India
2. S.Pal and S.C. Bhunia, “Engineering Mathematics” Oxford University Press
3. Jay L. Devore, “Probability and Statistics for Engineering and Sciences”, Seventh Edition,
Thomson/CENGAGE Learning India Pvt. Ltd
Reference books:
1. E.B. Saff, A.D.Snider, “Fundamental of Complex Analysis”, Third Edition, Pearson Education, New
Delhi
2. P. V. O’Neil, “Advanced Engineering Mathematics”, CENGAGE Learning, New Delhi
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
4 Year B.Tech(Aeronautical Engineering )Program Structure for admission batch of 2015-16
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PAE4I101 AERODYNAMICS – I
UNIT 1. REVIEW OF BASIC FLUID MECHANICS
Continuity, momentum and energy equations.
UNIT 2. TWO DIMENSIONAL FLOWS
Basic flows – Source, Sink, Free and Forced vortex, uniform parallel flow. Their combinations, Ideal Flow over
a circular cylinder, D’Alembert’s Paradox, Magnus effect, KuttaJonkowski’s Theorem, Starting Vortex, Kutta
condition, Pressure and velocity distributions on bodies with and without circulation in ideal and real fluid
flows.
.UNIT 3. AIRFOIL THEORY
Cauchy-Riemann relations, Complex Potential, Methodology of Conformal Transformation, Kutta-Joukowski
transformation and its applications, Karman Trefftz Profiles, Thin Airfoil theory and its applications.
UNIT 4. AIRFOIL AND WING THEORY
Vortex Filament, Biot and Savart Law, Bound Vortex and trailing Vortex, Horse Shoe Vortex, Lifting Line Theory
and its limitations.
UNIT 5. VISCOUS FLOW
Boundary layer and boundary layer thickness, displacement thickness, momentum thickness, Energy thickness,
Shape parameter, Boundary layer equations for a steady, two dimensional incompressible flow, Boundary Layer
growth over a Flat plate, Critical Reynolds Number, Blasius solution, Basics of Turbulent flow, Prandtl’s mixing
length hypothesis, Free shear layers.
TEXT BOOKS
1. Anderson, J.D., “Fundamentals of Aerodynamics”, McGraw-Hill Book Co., New York, 1998.
REFERENCES
1. Houghton, E.L., and Carruthers, N.B., “Aerodynamics for Engineering students”, Edward Arnold Publishers Ltd., London, 1989.
2. Milne Thomson, L.H., “Theoretical aerodynamics”, Macmillan, 1985. 3. Clancey, L.J., “Aerodynamics”, Pitman, 1986
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
4 Year B.Tech(Aeronautical Engineering )Program Structure for admission batch of 2015-16
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PAE4I102 Aircraft Material & Production
UNIT I. AIRCRAFT MATERIALS-FERROUS- NON -FERROUS
Characteristics,properties and identification of common alloy steels used in aircraft, Heat treatment and application
of alloy steels, Characteristics,properties and identification of common non-ferrous materials used in aircraft , Heat
treatment and application of non-ferrous materials
UNIT II. COMPOSITE AND NON -METALLIC Characteristics,properties and identification of common composite and non-metallic materials,other than wood
used in aircraft., Sealent and bonding agent, Construction methods of wooden airframe structures,
Characteristics,properties and types of wood and glue used inaeroplanes , Characteristics,properties and types
offabricusedinaeroplanes
UNIT III MACHIINING
General principles (with schematic diagrams only) of working and commonly performed operations in the following
machines: Lathe, Shaper, Planer, Horizontal milling machine, Universal drilling machine, Cylindrical grinding
machine, Capstan and Turret lathe. Basics of CNC machines. General principles and applications of the following
processes: Abrasive jet machining, Ultrasonic machining, Electric discharge machining, Electro chemical
machining, Plasma are machining, Electron beam machining and Laser beam machining.
UNIT IV FORMING AND SHAPING OF PLASTICS Types of plastics-characteristics of the forming and shaping processes-Moulding of Thermoplastics-working
principles and typical applications of Injection moulding- Thermoforming-processing of thermosets-working
principles and typical applications-
UNIT V METAL FORMING AND POWDER METALLURGY Principles and applications of the following processes: Forging, Rolling, Extrusion, Wire
drawing and Spinning, Powder metallurgy-Principal steps involved advantages. Disadvantages and limitations of
powder metallurgy
TEXT BOOK:
1. Tittertion , Aircraft Materials And Processes 2. Harija choudry, Elements of workshop Technology, vol. I and II Media
promoters and publishers pvt., Ltd., Mumbai, 2001.
REFERENCES:
1. R. K. Jain and S. C. Gupta, production Technology, Khanna Publishers. 16th
Edition, 2001. 2. H. M. T. production technology-Hand book, Tata Mc Graw-Hill, 2000. 3. Roy. A. Linberg, process and materials of manufacturing technology, PHI,
2000. 4. M. Adithan and A. B. Cupta, manufacturing technology, New Age, 1996. 5. Serope Kalpajian, Steven R. Schimid, Manuyfacturing Engineering and
Technology, Pearson Education, Inc.2002 (second Indian Reprint)
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
4 Year B.Tech(Aeronautical Engineering )Program Structure for admission batch of 2015-16
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PAE4I103 AIRCRAFT STRUCTURES – I
.
UNIT 1. STATICALLY DETERMINATE STRUCTURES
Analysis of plane Truss-Method of joints-3 D Truss-Plane frames-Composite beam.
UNIT 2. STATICALLY INDETERMINATE STRUCTURES
Propped Cantilever- Fixed-Fixed beams-Clapeyron's Three Moment Equation - Moment Distribution Method.
UNIT 3. ENERGY METHODS
Strain Energy due to axial, bending and Torsional loads – Castigliano’s theorems- Maxwell's Reciprocal theorem, Unit load method - application to beams, trusses, frames, rings, etc.
UNIT 4. COLUMNS
Columns with various end conditions – Euler’s Column curve – Rankine’s formula - Column with initial curvature - Eccentric loading – South well plot – Beam column.
UNIT 5. FAILURE THEORY
Maximum Stress theory – Maximum Strain Theory – Maximum Shear Stress Theory – Distortion Theory – Maximum Strain energy theory – Application to aircraft Structural problems.
TEXT BOOK
1. Donaldson, B.K., “Analysis of Aircraft Structures – An Introduction”, McGraw-Hill, 1993.
2. Bruhn.E.F.”Analysis and design of flight vehicle structures” Tri set of offset company, USA,1973.
REFERENCE
1. Timoshenko, S., “Strength of Materials”, Vol. I and II, Princeton D. Von Nostrand Co, 1990.
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PAE4I104 PROPULSION – I
UNIT I FUNDAMENTALS OF AIR BREATHING ENGINES
Operating principles of piston engines – thermal efficiency calculations – classification of piston engines - illustration of working of gas turbine engine – the thrust equation – factors affecting thrust – effect of pressure, velocity and temperature changes of air entering compressor – methods of thrust augmentation – characteristics of turboprop, turbofan and turbojet – performance characteristics. UNIT II SUBSONIC AND SUPERSONIC INLETS FOR JET ENGINES
Internal flow and Stall in subsonic inlets – Boundary layer separation – Major features of external flow near a
subsonic inlet – Relation between minimum area ratio and eternal deceleration ratio – Diffuser performance –
Supersonic inlets – Starting problem on supersonic inlets – Shock swallowing by area variation – External
declaration – Models of inlet operation.
UNIT III NOZZLES
Theory of flow in isentropic nozzles – nozzles and choking – Nozzle throat conditions – Nozzle efficiency –
Losses in nozzles – Over expanded and under – expanded nozzles – Ejector and variable area nozzles –
Interaction of nozzle flow with adjacent surfaces – Thrust reversal
UNIT IV COMPRESSORS
Principle of operation of centrifugal compressor – Work done and pressure rise – Velocity diagrams –
Diffuser vane design considerations – Concept of prewhirl, rotation stall and surge – Elementary theory of
axial flow compressor – Velocity triangles – degree of reaction – Three dimensional –Compressor blade
design – Centrifugal and Axial compressor performance characteristics
UNIT V COMBUSTION CHAMBERS
Classification of combustion chambers – Important factors affecting combustion chamber design –
Combustion process – Combustion chamber performance – Effect of operating variables on performance –
Flame tube cooling – Flame stabilization – Use of flame holders – Numerical problems.
TEXT BOOKS: 1. Hill, P.G. & Peterson, C.R. “Mechanics & Thermodynamics of Propulsion” Addison – Wesley
Longman INC, 1999. 2. James Award, "Aerospace Propulsion System"
REFERENCES: 1. Cohen, H. Rogers, G.F.C. and Saravana muttoo, H.I.H. “Gas Turbine Theory”, Longman, 1989. 2. Oates, G.C., “Aero thermodynamics of Aircraft Engine Components”, AIAA Education Series, New
York, 1985. 3. Rolls Royce, "Jet Engine”, 5th Edition, Rolls Royce Technical Publications, 2005. 4. Mathur, M.L. and Sharma, R.P., “Gas Turbine, Jet and Rocket Propulsion”, Standard Publishers &
Distributors, Delhi, 1999.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
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AIRCRAFT STRUCTURES LAB –I
LIST OF EXPERIMENTS
1. Determination of Young’s modulus of steel using mechanical extensometers.
2. Determination of Young’s modulus of aluminum using electrical extensometers
3. Determination of fracture strength and fracture pattern of ductile and brittle
materials
4. Determination of forces in statically indeterminate force system.
5. Deflection of beams with various end conditions.
6. Verification of Maxwell’s Reciprocal theorem & principle of superposition
7. Column – Testing
8. South – well’s plot.
9. Testing of Riveted Joints.
10. Determination of membrane stresses in a thin cylinder under internal pressure.
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AERODYNAMICS – 1 LABORATORY
LIST OF EXPERIMENTS
1. Study of wind tunnel
2. Calibration of subsonic wind tunnel
2. Flow visualization in water flow channel
3. Flow visualization of smooth and rough circular cylinder.
4. Pressure distribution over smooth and rough circular cylinder.
6. Pressure distribution over a rough circular cylinder.
7. Pressure distribution over a symmetric aerofoil.
8. Pressure distribution over a cambered aerofoil.
9. Flow visualization of airfoil with different angle of attack..
10. Force measurement using wind tunnel balance of airfoil
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 4th Semester
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PROPULSION LAB- 1 LABORATORY
LIST OF EXPERIMENTS
1. Study of an aircraft piston engine. (Includes study of assembly of sub systems,
various components, their functions and operating principles)
2. Study of camshaft operation, firing order and magneto, valve timing
3. Study of auxiliary system. Pump and carburetor
4. Study of an aircraft jet engine and assemble process
5. Velocity profiles of free jets.
6. Velocity profiles of wall jets.
7. Study of forced convective heat transfer over a flat plate.
8. Pressure measurement of a subsonic ramjet duct
9. Wall pressure distribution in subsonic diffuser
10. Wall pressure distribution in subsonic Nozzle
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PRODUCTION TECHNOLOGY LABORATORY
LIST OF EXPERIMENTS
1. LATHE
1.1. Facing, plain turning and step turning 1.2. Taper turning using compound rest. 1.3. Taper turning using taper turning attachment 1.4. Single start V thread, cutting and knurling 1.5. Boring and internal thread cutting.
2. SHAPER AND SLOTTER
2.1. Machining a V- block (in a Shaper) 2.2. Machining hexagonal shape (in a Shaper) 2.3. Machining internal key-way (in a slotter)
3. DRILLING
3.1 Drilling 4 or 6 holes at a given pitch circle on a plate 3.2. Drilling, reaming and tapping
4. MILLING
4.1. Plain Milling Exercise 4.2. Gear Milling Exercise
5. GRINDING
Cylindrical Grinding Exercise
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 5th Semester
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Fifth Semester
Theory Practical Code Course Name Hours/
Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/Week L/T
Credit Practical
Marks
PC Aircraft Structures-II 3-0 3 100 50 2 1 50 PC Aerodyanmics-II 3-0 3 100 50 2 1 50 PC Aircraft Performance 3-0 3 100 50 2 1 50 PE Finite Element
Method/Experimental stress Analysis/Computational fluid Dynamics
3-1 4 100 50
OE Total Quality Management/Production Management/Operational Research
3-1 4 100 50
PC Advance Lab-I 8 4 200
Total 17 17 500 250 14 7 350
Total Marks: 1100
Total Credits: 24
For Honours and Minor Specialization
4 4 100 50
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Semester : 5th
--------------
1. PAE5D001 Honours(O4) Fatique & Fracture Mechanics 4-0-0 4
2. PAE5D002 Honours(O4) Finite Element Method 4-0-0 4
3. PAE5D003 Honours(O4) Computational Fluid Dynamics 4-0-0 4
4. PAE5G001 Minor(CP) Propulsion - I 4-0-0 4
5. PAE5H001 OE(O2) Total Quality Management 4-0-0 4
6. PAE5H002 OE(O2) Production Management 4-0-0 4
7. PAE5H003 OE(O2) Operational Research 4-0-0 4
8. PAE5I101 PC(CP) Aircraft Structures-II 3-0-1 4
9. PAE5I102 PC(CP) Aerodynamics-II 3-0-1 4
10. PAE5I103 PC(CP) Aircraft Performance 3-0-1 4
11. PAE5I201 PC(CP) Advance Lab - I 0-0-4 4
12. PAE5J001 PE(O3) Finite Element Method 4-0-0 4
13. PAE5J002 PE(O3) Experimental Stress Analysis 4-0-0 4
14. PAE5J003 PE(O3) Computational fluid Dynamics 4-0-0 4
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28
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PAE5I101 Aircraft Structures – II
Module – I UNSYMMETRICAL BENDING
Principal axis and neutral axis methods- bending stresses in beams of symmetric sections with skew loads-
bending stresses in beams of unsymmetrical sections.
Module – 2. SHEAR FLOW IN OPEN SECTIONS
Thin walled beams, Concept of shear flow, shear centre, Elastic axis. With one axis of
symmetry, with wall effective and ineffective in bending, unsymmetrical beam sections.
.
Module – 3. SHEAR FLOW IN CLOSED SECTIONS
Bredt – Batho formula, Single and multi – cell structures.- Shear flow in single & multicell
structures under torsion. Shear flow in single and multicell under bending with walls
effective and ineffective.
.
Module – 4. BUCKLING OF PLATES
Vortex Filament, Biot and Savart Law, Bound Vortex and trailing Vortex, Horse Shoe Vortex, Lifting Line Theory
and its limitations.
Module –5. STRESS ANALYSIS IN WING AND FUSELAGE
Shear resistant web beams-Tension field web beams(Wagner’s) – Shear and bending
moment distribution for cantilever and semi-cantilever types of beams
TEXT BOOKS
1. Peery, D.J., and Azar, J.J., “Aircraft Structures”, 2nd edition, McGraw–Hill, N.Y., 2007.
2. Megson, T.M.G., “Aircraft Structures for Engineering Students”, Edward Arnold, 2007.
REFERENCES
1. Bruhn. E.H. “Analysis and Design of Flight vehicles Structures”, Tri – state off set
company, USA, 1985.
2. Rivello, R.M., “Theory and Analysis of Flight Structures”, McGraw-Hill, 1993.
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PAE5I102 Aerodynamics – II
Module – I ONE DIMENSIONAL COMPRESSIBLE FLOW
Energy, Momentum, continuity and state equations, velocity of sound, adiabatic steady
state flow equations, Flow through convergent- divergent passage, Performance under
various back pressures.
Module – II NORMAL, OBLIQUE SHOCKS
Prandtl equation and Rankine – Hugonoit relation, Normal shock equations, Pitot static
tube, corrections for subsonic and supersonic flows, Oblique shocks and corresponding
equations, θ- β- M relation, Hodograph and pressure turning angle, shock polar, flow past wedges and
concave corners, strong, weak and detached shocks,
Module – III EXPANSION WAVES, RAYLEIGH AND FANNO FLOW
Flow past convex corners, Expansion hodograph, Reflection and interaction of shocks and expansion,
waves. Method of Characteristics Two dimensional supersonic nozzle contours. Rayleigh and Fanno Flow,
Module – IV SUPERSONIC AND TRANSONIC FLOW
Lift, drag pitching moment and center of pressure of supersonic profiles. Lower and upper critical Mach
numbers, Lift and drag divergence, shock induced separation, Characteristics of swept wings, Effects of
thickness, camber and aspect ratio of wings, Transonic area rule.
TEXT BOOK
1. Rathakrishnan, E., “Gas Dynamics”, Prentice Hall of India, 2003.
REFERENCES
1. Shapiro, A.H., “Dynamics and Thermodynamics of Compressible Fluid Flow”, Ronald
Press, 1982.
2. Zucrow, M.J. and Anderson, J.D., “Elements of gas dynamics”, McGraw-Hill Book Co.,
New York, 1989.
3. Anderson Jr., D., – “Modern compressible flows”, McGraw-Hill Book Co., New York
1999.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 5th Semester
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PAE5I103 AIRCRAFT PERFORMANCE
OBJECTIVE:
To make the student understand the performance of airplanes under various flight conditions like take off, cruise,
landing, climbing, gliding, turning etc.
Module – I GENERAL CONCEPTS:
International Standard atmosphere, IAS, EAS, TAS, Propeller theory- Froude momentum and blade element
theories, Propeller co-efficients, Use of propeller charts, Performance of fixed and variable pitch propellers, High
lift devices, Thrust augmentation
Module – II DRAG OF BODIES
Streamlined and bluff body, Types of drag, Effect of Reynold’s number on skin friction and pressure drag, Drag
reduction of airplanes, Dragpolar, Effect of Mach number on drag polar
Module – III STEADY LEVEL FLIGHT
Steady level flight, Thrust required and Power required, Thrust available and Power available for propeller driven
and jet powered aircraft, Effect of altitude, maximum level flight speed, conditions for minimum drag and
minimum power required, Effect of drag divergence on maximum velocity, Range and Endurance of Propeller
and Jet airplanes.
Module – IV GLIDING AND CLIMBING FLIGHT
Shallow and steep angles of climb, Rate of climb, Climb hodograph, Maximum Climb angle and Maximum Rate
of climb- Effect of design parameters for propeller , Absolute and service ceiling, Gliding flight, Glide hodograph
Module – V ACCELERATD FLIGHT
Estimation of take-off and landing distances, Methods of reducing landing distance, level turn, minimum turn
radius, bank angle and load factor, Constraints on load factor, Pull up and pull down maneuvers, maximum turn
rate, V-n diagram.
TEXT BOOKS:
1. Houghton,E.L. and Carruthers, N.B. Aerodynamics for engineering students,
Edward Amold Publishers, 1988.
2. Anderson, Jr., J.D. Aircraft Performance and Design, McGraw-Hill International
Edition, 1999
REFERENCES:
1. Kuethe, A.M. and Chow, C.Y., Foundations of Aerodynamics, John Wiley & Sons,
1982.
2. J.J.Bertin, Aerodynamics for Engineers, Prentice-Hall, 1988.
3. L.J. Clancey, Aerodynamics, Pitman, 1986
4. Anderson, Jr., J.D. Introduction to Flight, McGraw-Hill International Edition, 1999
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16 5th Semester
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PAE5D002 FINITE ELEMENT METHOD
OBJECTIVE
To introduce the concept of numerical analysis of structural components
Module – I
INTRODUCTION
Review of basic approximate methods of analyses – Stiffness and Flexibility matrix for simple cases –
Governing equation and convergence criteria of finite element method.
Module – II
DISCRETE ELEMENTS
Bar, Frame, beam elements – Application to static, dynamic analysis.
Module – III
CONTINUUM ELEMENTS
Various types of 2-D-elements Application to plane stress, plane strain and axisymmetric problems.
Module – IV
ISOPARAMETRIC ELEMENTS
Applications to two and three-dimensional problems(four, eight and nine nodded element), Numerical
Integration
Module – V
FIELD PROBLEM
Applications to other field problems like heat transfer and fluid flow.
TEXT BOOK
1. Tirupathi.R.C and Ashok D.B, “Introduction to Finite Elements in Engineering”,
Prentice Hall India, Third Edition, 2003.
REFERENCES
1. Reddy J.N. “An Introduction to Finite Element Method”, McGraw-Hill, 2000.
2. Krishnamurthy, C.S., “Finite Element Analysis”, Tata McGraw-Hill, 2000.
3. Bathe, K.J. and Wilson, E.L., “Numerical Methods in Finite Elements Analysis”,
Prentice Hall of India, 1985.
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PAE5J002 EXPERIMENTAL STRESS ANALYSIS
OBJECTIVE
To bring awareness on experimental method of finding the response of the structure to
different types of load.
Module – I MEASUREMENTS & EXTENSOMETER
Principles of measurements, Accuracy, Sensitivity and range of measurements. Mechanical, Optical
Acoustical and Electrical extensometers and their uses, Advantages
and disadvantages.
Module – II ELECTRICAL RESISTANCE STRAIN GAUGES
Principle of operation and requirements, Types and their uses, Materials for strain gauge. Calibration and
temperature compensation, cross sensitivity, Rosette analysis, Wheastone bridge for static and dynamic
strain measurements, strain indicators.
Module – III PHOTOELASTICITY
Two dimensional photo elasticity, Concept of light – photoelastic effects, stress optic law, Interpretation of
fringe pattern, Compensation and separation techniques, Photo elastic materials. Introduction to three
dimensional photo elasticity.
Module – IV BRITTLE COATING AND MOIRE METHODS
Introduction to Moire techniques, brittle coating methods and holography.
Module – V NON – DESTRUCTIVE TESTING
Fundamentals of NDT, Radiography, ultrasonic, magnetic particle inspection, Fluorescent penetrant
technique, Eddy current testing, Acoustic Emission Technique.
TEXT BOOKS
1. Srinath, L.S., Raghava, M.R., Lingaiah, K., Garagesha, G., Pant B., and
Ramachandra, K., “Experimental Stress Analysis”, Tata McGraw-Hill, New Delhi, 1984.
REFERENCES
1. Dally, J.W., and Riley, W.F., “Experimental Stress Analysis”, McGraw-Hill Inc., New
York, 2005, IV edition.
2. Hetyenyi, M., “Hand book of Experimental Stress Analysis”, John Wiley and Sons Inc.,
New York, 1972.
3. Pollock A.A., “Acoustic Emission in Acoustics and Vibration Progress”, Ed. Stephens
R.W.B., Chapman and Hall, 1993
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PAE5J003 COMPUTATIONAL FLUID DYNAMICS
OBJECTIVE
To study the flow of dynamic fluids by computational methods
Module-I
FUNDAMENTAL CONCEPTS
Introduction - Basic Equations of Fluid Dynamics - Incompressible In viscid Flows: Mathematical properties
of Fluid Dynamics Equations -_ Elliptic, Parabolic and Hyperbolic equations - Well posed problems -
discretization of partial Differential Equations. Explicit finite difference methods of subsonic, supersonic and
viscous flows.
Module-II
DISCRETIZATION
Boundary layer Equations and methods of solution -Implicit time dependent methods for inviscid and
viscous compressible flows - Concept of numerical dissipation –Stability properties of explicit and implicit
methods - Conservative upwind discretization for Hyperbolic systems - Further advantages of upwind
differencing.
Module-III
GRID GENERATION
Structured grids. Types and transformations. Generation of structured grids. Unstructured grids. Delany
triangulation.
Module-IV
FINITE VOLUME TECHNIQUES
Finite Volume Techniques - Cell Centered Formulation - Lax - Vendoroff Time Stepping - Runge - Kutta
Time Stepping - Multi - stage Time Stepping - Accuracy -. Cell Vertex Formulation - Multistage Time
Stepping - FDM -like Finite Volume Techniques – Central and Up-wind Type Discretizations - Treatment of
Derivatives. Flux – splitting schemes. Pressure correction solvers – SIMPLE, PESO. Vorticity transport
formulation. Implicit/semi-implicit schemes.
TEXT BOOK
1. Fletcher, C.A.J., “Computational Techniques for Fluid Dynamics”, Vols. I and II,
Springer - Verlag, Berlin, 1988.
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REFERENCES
1. John F. Wendt (Editor), “Computational Fluid Dynamics - An Introduction”, Springer –
Verlag, Berlin, 1992
2. Charles Hirsch, “Numerical Computation of Internal and External Flows”, Vols. I and II.
John Wiley & Sons, New York, 1988.
3. Klaus A Hoffmann and Steve T. Chiang. “Computational Fluid Dynamics for
Engineers”, Vols. I & II Engineering Education System, P.O. Box 20078, W. Wichita,
K.S., 67208 - 1078 USA, 1993.
4. Anderson, Jr.D., “Fundamentals of Aerodynamics”, McGraw-Hill, 2000.
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Total Quality Management/Production Management/Operational Research common to other branch
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AIRCRAFT STRUCTURES LAB – II LABORATORY
LIST OF EXPERIMENTS
1. Unsymmetrical bending of beams
2. Shear centre location for open sections
3. Shear centre location for closed sections
4. Constant strength beam
5. Flexibility matrix for cantilever beam
6. Beam with combined loading
7. Calibration of Photo- elastic materials
8. Stresses in circular discs and beams using photoelastic techniques
9. Vibrations of beams
10. Wagner beam – Tension field beam
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AERODYNAMICS – II LABORATORY
LIST OF EXPERIMENTS
1.Determin the CL calculation from pressure destitution
2.Determination of profile drag of bodies by wake survey method.
3. Pressure distribution over a finite wing.
4. Pressure distribution over a Nose cone model.
5. Determination of Base drag of a missile model.
6. Pressure distribution over a water tank model for various wind speeds.
7. B/L hight using hotware anemometer
8. Calibration of Supersonic Wind Tunnel.
9. Flow visualization studies in supersonic flows.
10. Flow visualization over missile
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AIRCRAFT PERFORMANCE LABORATORY
OBJECTIVE
To introduce and develop the basic concept of aircraft design.
Each student is assigned the design of an Airplane (or Helicopter or any other flight
vehicle), for given preliminary specifications. The following are the assignments to be
carried out:
EXPERIMENTS
1. Comparative configuration study of different types of airplanes
2. Comparative study on specification and performance details of aircraft
3. Preparation of comparative data sheets
4. Work sheet layout procedures
5. Comparative graphs preparation and selection of main parameters for the design
6. Preliminary weight estimations, selection of main parameters,
7. Power plant selection, Aerofoil selection, Wing tail and control surfaces
8. Preparation of layouts of balance diagram and three view drawings
9. Drag estimation
10. Detailed performance calculations