scheme of instruction and evaluation i - viii semester …

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


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


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Second Year Engineering

Third Semester


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


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/


*Skill Project and Hands on

6 3 100

Total 18 18 600 300 14 7 300

Total Marks: 1200

Total Credits: 25


4 4 100 50

*College should conduct at least one NSDC program under this category.


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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


4 4 100 50


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Sixth Semester


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


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.


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Final Year Engineering

Seventh Semester


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


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


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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/


Total 19 19 600 300 8 4 200

Total Marks: 1100

Total Credits: 23


4 4 100 50


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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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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.


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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.


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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.


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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


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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.


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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


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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


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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


4 4 100 50



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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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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



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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



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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)



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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.



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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



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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


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


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.


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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


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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

scheme of instruction and evaluation i - viii semester …

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