B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
Second Year Engineering Third Semester Code
Course Name
Hours/ Week L/T
Credit Theory
University Marks
Internal Evaluation
Hours/ Week L/T
Credit Practical
Marks
PC
3-0
3
100
50
2
1
50
PC
Fluid Mechanics & Heat flow Aero Thermodynamics
PC
Strength of Materials
PC
Elements of Aeronautics
3-0 3-0 3-0
3 3 3
100 100 100
50 50 50
2 2 2
1 1 1
50 50 50
PC
Avionics
HS
Engineering Economics/ Organizational Behavior
3-1 2-1
4 3
100 100
50 50
19
19
600
300
8
4
200
4
4
100
50
Total Total Marks: 1100 Total Credits: 23 Honours Aircraft Rules & RegulationCAR I & II/ Airport Planning & Management / Flight Schedule & Operation Minor Elements of Aeronautics
1
Practical
Page
Theory
Aircraft Rules & Regulation- CAR I & II Airport Planning & Management Flight Schedule & Operation Engineering Economics Organizational Behavior Elements of Aeronautics Avionics Fluid Mechanics & Heat flow Aero Thermodynamics Strength of Material Elements of Aeronautics
4-0-0 4-0-0 4-0-0 3-0-0 3-0-0 4-0-0 4-0-0 3-0-1 3-0-1 3-0-1 3-0-1
4 4 4 3 3 4 4 4 4 4 4 --27 ---
2
Semester : 3rd -------------1. PAE3D001 Honours(O2) 2. PAE3D002 Honours(O2) 3. PAE3D003 Honours(O2) 4. PEK3E001 HS(O1) 5. POB3E002 HS(O1) 6. PAE3G001 Minor(O3) 7. PAE3I001 PC(CP) 8. PAE3I101 PC(CP) 9. PAE3I102 PC(CP) 10. PAE3I103 PC(CP) 11. PAE3I104 PC(CP)
3rd Semester
Page
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
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:
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3
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
FLUID MECHANICS AND HEAT FLOW LABORATORY (Common to Aeronautical, Automobile, Mech & Prod) OBJECTIVE To study the flow measurement and the performance of fluid machinery
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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1.
4
LIST OF EXPERIMENTS
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
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. 2. 3. 4 5
Rathakrishnan, E, “Fundamentals of Engineering Thermodynamics”, Prentice – Hall, India, 2000 Nag. P.K., “Engineering Thermodynamics”, Tata McGraw-Hills Co., Ltd., Seventh Edn., 1993 Yunus A.Cengal. “Thermodynamics an Engineering Approach”, Tata McGraw-Hill Co. Ltd., 3rd Edition, 2002. D. P. Mishra, Fundamentals of Combustion, Prentice Hall of India, New Delhi, revised edition, 2010. v. Ganesan, Internal Combustion Engines, Tata McGraw-Hills Co
REFERENCES
3. 5.
5
2.
Mayhew, A. and Rogers, B., “Engineering Thermodynamics”, Longman Green & Co. Ltd., London, E.L.B.S. Edition, 1990. Van Wylen, G.J. and Sonntag, R.E., “Fundamentals of Classical Thermodynamics (S.I.Version)”, Second Edition, 1986. Bacon, D.H., “Engineering Thermodynamics”, Butterworth & Co., London, 1989. D. P. Mishra, Engineering Thermodynamics, Cengage Learning India Pvt. Ltd, 2011.
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1.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
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.
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6
10. Determination of Thermal Resistance of a Composite wall.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
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 beamsBending 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.
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
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10. Block Compression Test
7
9. Testing of springs
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
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
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8
REFERENCES: 1. Kermode, A.C., “Mechanics of Flight”, Himalayan Book, 1997
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
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.
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4. Aircraft Radio Systems, J.Powell, Pitman publishers, 1998.
9
3. Aircraft Instrumentation and Integrated systems EHJ Pallet, Longman Scientific Technical (Sterling Book House, Mumbai) 1996.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
PEK3E001
3rd Semester
ENGINEERING ECONOMICS
Theory L/T (Hours per week):2/1, Credit: 3
Module I (12 hours) Engineering Economics- Nature, Scope, Basic problems of an economy, Micro Economics and Macro Economics. Demand- Meaning of demand, Demand function, Law of Demand and its exceptions, Determinants of demand, Elasticity of demand & its measurement (Simple numerical problems to be solved ), SupplyMeaning of supply, Law of supply and its exception, Determinants of supply, Elasticity of supply, Determination of market equilibrium (Simple numerical problems to be solved). Production-Production function, Laws of returns: Law of variable proportion, Law of returns to scale
Module II (12 hours)
Cost and revenue concepts, Basic understanding of different market structures, Determination of equilibrium price under perfect competition (Simple numerical problems to be solved), Break Even Analysis-linear approach (Simple numerical problems to be solved). Banking -Commercial bank, Functions of commercial bank, Central bank, Functions of Central Bank. Inflation-Meaning of inflation, types, causes, measures to control inflation. National Income-Definition, Concepts of national income, Method of measuring national income.
Module III (12 hours)
Time value of money- Interest - Simple and compound, nominal and effective rate of interest, Cash flow diagrams, Principles of economic equivalence. Evaluation of engineering projects-Present worth method, Future worth method, Annual worth method, Internal rate of return method, Cost benefit analysis for public projects . Depreciation- Depreciation of capital assert, Causes of depreciation, Methods of calculating depreciation (Straight line method, Declining balance method), After tax comparison of project. Text Books
10
Riggs, Bedworth and Randhwa, “Engineering Economics”, McGraw Hill Education India Principles of Economics, Deviga Vengedasalam; Karunagaran Madhavan, Oxford University Press. Engineering Economy by William G.Sullivan, Elin M.Wicks, C. Patric Koelling, Pearson R.Paneer Seelvan, “ Engineering Economics”, PHI Ahuja,H.L., “Principles of Micro Economics” , S.Chand & Company Ltd Jhingan,M.L., “Macro Economic Theory” Macro Economics by S.P.Gupta, TMH
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1. 2. 3. 4. 5. 6. 7.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
POB3E002 ORGANIZATIONAL BEHAVIOUR Credit- 3 Class Hours - 40 Objectives: 1. To develop an understanding of the behavior of individuals and groups inside organizations 2. To enhance skills in understanding and appreciating individuals, interpersonal, and group process for increased effectiveness both within and outside of organizations. 3. To develop theoretical and practical insights and problem-solving capabilities for effectively managing the organizational processes. MODULE I Fundamentals of OB: Definition, scope and importance of OB, Relationship between OB and the individual, Evolution of OB, Theoretical framework (cognitive), behavioristic and social cognitive), Limitations of OB. MODULE II Attitude: Importance of attitude in an organization, Right Attitude, Components of attitude, Relationship between behavior and attitude, Developing Emotional intelligence at the workplace, Job attitude, Barriers to changing attitudes.
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MODULE IV Organizational Culture : Meaning & Definition of Organizational Culture, creating & Sustaining Organizational Culture, Types of Culture (Strong vs. Weak Culture, Soft Vs. Hard Culture & Formal vs. Informal Culture), Creating Positive Organizational Culture, Concept of Workplace Spirituality. Organizational Change: Meaning, Definition & Nature of Organizational Change, Types of Organizational Change, Forces that acts as stimulants to change. Implementing Organizational Change : How to overcome the Resistance to Change, Approaches to managing Organizational Change, Kurt Lewin’s-Three step model, Seven Stage model of Change & Kotter’s Eight-Step plan for Implementing Change, Leading the Change Process, Facilitating Change, Dealing with Individual & Group Resistance, Intervention Strategies for Facilitating Organizational Change, Methods of Implementing Organizational Change, Developing a Learning Organization. 7
11
MODULE III Personality and values: Definition and importance of Personality for performance, The Myers-Briggs Type Indicator and The Big Five personality model, Significant personality traits suitable to the workplace (personality and job – fit theory), Personality Tests and their practical applications. Perception: Meaning and concept of perception, Factors influencing perception, Selective perception, Attribution theory, Perceptual process, Social perception (stereotyping and halo effect). Motivation: Definition & Concept of Motive & Motivation, The Content Theories of Motivation (Maslow’s Need Hierarchy & Herzberg’s Two Factor model Theory), The Process Theories (Vroom’s expectancy Theory & Porter Lawler model), Contemporary Theories – Equity Theory of Work Motivation.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
3rd Semester
Page
12
Reference Books 1. Understanding Organizational Behaviour, Parek, Oxford 2. Organizational Behaviour, Robbins, Judge, Sanghi, Pearson. 3. Organizational Behaviour, K. Awathappa,HPH. 4. Organizational Behaviour, VSP Rao, Excel 5. Introduction to Organizational Behaviour, Moorhead, Griffin, Cengage. 6. Organizational Behaviour, Hitt, Miller, Colella, Wiley.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
Fourth Semester Theory
Practical
Code
Course Name
Hours/Week L/T
Credit Theory
University Marks
Internal Evaluation
HS
Applied Mathematics III
3-0
3
100
50
PC
Aerodynamics-I
3-0
3
100
PC
Aircraft Materials Production
3-0
3
PC
Aircraft Structures-I
3-0
PC
Propulsion-I
HS
Engineering Economics/ Organizational Behaviour *Skill Project and Hands on
&
Total
Hours/ Week L/T
Credit Practical
Marks
50
2
1
50
100
50
2
1
50
3
100
50
2
1
50
3-0
3
100
50
2
1
50
2-1
3
100
50 6
3
100
14
7
300
18
18
600
300
4
4
100
50
Page
Total Credits: 25 Honours Airframe Repair & Maintenance/ Boundary Layer Theory/Theory of Plates & Shells Minor Aerodynamics-I
18
Total Marks: 1200
Semester : 4th -------------1. PAE4D001 Honours(O2) 2. PAE4D002 Honours(O2) 3. PAE4D003 Honours(O2) 4. PAE4E001 HS(CP)
Airframe Repair & Maintenance Boundary Layer Theory Theory of Plates & Shells Applied Mathematics III
4-0-0 4-0-0 4-0-0 3-0-0
4 4 4 3
5. 6. 7. 8. 9. 10. 11. 12.
Engineering Economics Organizational Behavior Aerodynamics-I Aerodynamics-I Aircraft Materials & Production Aircraft Structures-I Propulsion - I Skill Project and Hands on
3-0-0 3-0-0 4-0-0 3-0-1 3-0-1 3-0-1 3-0-1 0-0-3
3 3 4 4 4 4 4 3 --29 ---
PEK4E002 POB4E003 PAE4G001 PAE4I101 PAE4I102 PAE4I103 PAE4I104 PAE4I201
HS(O1) HS(O1) Minor(CP) PC(CP) PC(CP) PC(CP) PC(CP) PC(CP)
19
4th Semester
Page
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
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
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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
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
21
2. 3.
Houghton, E.L., and Carruthers, N.B., “Aerodynamics for Engineering students”, Edward Arnold Publishers Ltd., London, 1989. Milne Thomson, L.H., “Theoretical aerodynamics”, Macmillan, 1985. Clancey, L.J., “Aerodynamics”, Pitman, 1986
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1.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
RODYNAMICS – 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..
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10. Force measurement using wind tunnel balance of airfoil
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
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 applicationsUNIT 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
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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)
23
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.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
PRODUCTION TECHNOLOGY LABORATORY
LIST OF EXPERIMENTS
1.
LATHE 1.1. 1.2. 1.3. 1.4. 1.5.
2.
SHAPER AND SLOTTER 2.1. 2.2. 2.3.
3.
Machining a V- block (in a Shaper) Machining hexagonal shape (in a Shaper) Machining internal key-way (in a slotter)
DRILLING 3.1 3.2.
4.
Facing, plain turning and step turning Taper turning using compound rest. Taper turning using taper turning attachment Single start V thread, cutting and knurling Boring and internal thread cutting.
Drilling 4 or 6 holes at a given pitch circle on a plate Drilling, reaming and tapping
MILLING 4.1. Plain Milling Exercise 4.2. Gear Milling Exercise GRINDING
24
Cylindrical Grinding Exercise
Page
5.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
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 theoremsMaxwell'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
Page
25
1. Timoshenko, S., “Strength of Materials”, Vol. I and II, Princeton D. Von Nostrand Co, 1990.
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
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
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.
Page
4.
26
materials
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
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” Longman INC, 1999. 2. James Award, "Aerospace Propulsion System"
Addison – Wesley
Page
27
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
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
Page
28
10. Wall pressure distribution in subsonic Nozzle
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
4th Semester
PAE4G001 AERODYNAMICS – I (MINOR) 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
29
2. 3.
Houghton, E.L., and Carruthers, N.B., “Aerodynamics for Engineering students”, Edward Arnold Publishers Ltd., London, 1989. Milne Thomson, L.H., “Theoretical aerodynamics”, Macmillan, 1985. Clancey, L.J., “Aerodynamics”, Pitman, 1986
Page
1.
30
4th Semester
Page
B.Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
Fifth Semester Credit Theory
University Marks
Internal Evaluation
Hours/ Week L/T
Credit Practical
Marks
PC
Aircraft Structures-II
PC
Aerodynamics-II
PC
Aircraft Performance
100 100 100 100
50 50 50 50
1 1 1
50 50 50
Finite Element Method/Experimental stress Analysis/Computational fluid Dynamics Total Quality Management/Production Management/Operational Research Advance Lab-I
3 3 3 4
2 2 2
PE
3-0 3-0 3-0 3-1
3-1
4
100
50
17
17
500
250
8 14
4 7
200 350
4
4
100
50
OE
PC
Total Total Marks: 1100 Total Credits: 24 Fatique & Honours
Minor
Fracture Mechanics/ Finite Element Method/ Computational Fluid Dynamics Propulsion - I
29
Practical
Hours/ Week L/T
Page
Theory Code Course Name
Fatique & Fracture Mechanics Finite Element Method Computational Fluid Dynamics Propulsion - I Total Quality Management Production Management Operational Research Aircraft Structures-II Aerodynamics-II Aircraft Performance Advance Lab - I Finite Element Method Experimental Stress Analysis Computational fluid Dynamics
4-0-0 4-0-0 4-0-0 4-0-0 4-0-0 4-0-0 4-0-0 3-0-1 3-0-1 3-0-1 0-0-4 4-0-0 4-0-0 4-0-0
4 4 4 4 4 4 4 4 4 4 4 4 4 4 --28 ---
30
Semester : 5th -------------1. PAE5D001 Honours(O4) 2. PAE5D002 Honours(O4) 3. PAE5D003 Honours(O4) 4. PAE5G001 Minor(CP) 5. PAE5H001 OE(O2) 6. PAE5H002 OE(O2) 7. PAE5H003 OE(O2) 8. PAE5I101 PC(CP) 9. PAE5I102 PC(CP) 10. PAE5I103 PC(CP) 11. PAE5I201 PC(CP) 12. PAE5J001 PE(O3) 13. PAE5J002 PE(O3) 14. PAE5J003 PE(O3)
5th Semester
Page
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
PAE5I101 Aircraft Structures – II(3-0-1)
Module – I
UNSYMMETRICAL BENDING
Principal axis and neutral axis methods- bending stresses in beams of symmetric sections with skew loadsbending 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.
Page
31
2. Rivello, R.M., “Theory and Analysis of Flight Structures”, McGraw-Hill, 1993.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
PAE5I102 Aerodynamics – II(3-0-1) 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.,
1999.
Page
3. Anderson Jr., D., – “Modern compressible flows”, McGraw-Hill Book Co., New York
32
New York, 1989.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
PAE5I103 AIRCRAFT PERFORMANCE(3-0-1) 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.
4. Anderson, Jr., J.D. Introduction to Flight, McGraw-Hill International Edition, 1999
Page
3. L.J. Clancey, Aerodynamics, Pitman, 1986
33
2. J.J.Bertin, Aerodynamics for Engineers, Prentice-Hall, 1988.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
PAE5D002 FINITE ELEMENT METHOD(4-0-0)
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.
Prentice Hall of India, 1985.
Page
3. Bathe, K.J. and Wilson, E.L., “Numerical Methods in Finite Elements Analysis”,
34
2. Krishnamurthy, C.S., “Finite Element Analysis”, Tata McGraw-Hill, 2000.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
PAE5J002 EXPERIMENTAL STRESS ANALYSIS (4-0-0)
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.
3. Pollock A.A., “Acoustic Emission in Acoustics and Vibration Progress”, Ed. Stephens R.W.B., Chapman and Hall, 1993
Page
New York, 1972.
35
2. Hetyenyi, M., “Hand book of Experimental Stress Analysis”, John Wiley and Sons Inc.,
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
PAE5J003 COMPUTATIONAL FLUID DYNAMICS (4-0-0) 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,
Page
36
Springer - Verlag, Berlin, 1988.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
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.
Page
37
4. Anderson, Jr.D., “Fundamentals of Aerodynamics”, McGraw-Hill, 2000.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
Page
38
Total Quality Management/Production Management/Operational Research common to other branch
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
AIRCRAFT STRUCTURES LAB – II LABORATORY
LIST OF EXPERIMENTS
39
Unsymmetrical bending of beams Shear centre location for open sections Shear centre location for closed sections Constant strength beam Flexibility matrix for cantilever beam Beam with combined loading Calibration of Photo- elastic materials Stresses in circular discs and beams using photoelastic techniques Vibrations of beams Wagner beam – Tension field beam
Page
1. 2. 3. 4. 5. 6. 7. 8. 9. 10.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
AERODYNAMICS – II LABORATORY LIST OF EXPERIMENTS
Page
40
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
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
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
Fatique & Fracture Mechanics/ Finite Element Method/ Computational Fluid Dynamics PAE5D001 Fatigue & Fracture Mechanics(4-0-0)
Page
UNIT I FATIGUE OF STRUCTURES S.N. curves - Endurance limits - Effect of mean stress, Goodman, Gerber and Soderberg relations and diagrams - Notches and stress concentrations - Neuber’s stress concentration factors - Plastic stress concentration factors - Notched S.N. curves. UNIT II STATISTICAL ASPECTS OF FATIGUE BEHAVIOUR Low cycle and high cycle fatigue - Coffin - Manson’s relation - Transition life - cyclic strain hardening and softening - Analysis of load histories - Cycle counting techniques Cumulative damage - Miner’s theory - Other theories. UNIT III PHYSICAL ASPECTS OF FATIGUE AND FRACTURE Phase in fatigue life - Crack initiation - Crack growth - Final Fracture - Dislocations fatigue fracture surfaces - Strength and stress analysis of cracked bodies - Potential energy and surface energy - Griffith’s theory - Irwin - Orwin extension of Griffith’s theory
41
OBJECTIVE To study the concepts of estimation of the endurance and failure mechanism of Components
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
to ductile materials - Effect of thickness on fracture toughness - stress intensity factors for typical geometries. UNIT IV FATIGUE DESIGN ANDTESTINIG Safe life and Fail-safe design philosophies - Importance of Fracture Mechanics in aerospace structures - Application to composite materials and structures. UNIT V FUNDAMENTALS OF FAILURE ANALYSIS Common causes of failure. Principles of failure analysis. Fracture mechanics approach to failure problems. Techniques of failure analysis. Service failure mechanisms - ductile and brittle fracture, fatigue fracture, wear failures, fretting failures, environment induced
TEXT BOOKS 1. Prasanth Kumar – “Elements of fracture mechanics” – Wheeter publication, 1999. 2. Barrois W, Ripely, E.L., “Fatigue of aircraft structure”, Pe/gamon press. Oxford, 1983. REFERENCES 1. Sin, C.G., “Mechanics of fracture” Vol. I, Sijthoff and w Noordhoff International Publishing Co., Netherlands, 1989. 2. Knott, J.F., “Fundamentals of Fracture Mechanics”, Buterworth& Co., Ltd., London, 1983 3. Subra suresh, “Fatigue of materials” , II edition, 1998. 4. T. L. Anderson, “Fracture mechanics: Fundamentals and applications”, III edition, 2004
PAE5J001 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.
Page
ISOPARAMETRIC ELEMENTS
42
Module – IV
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
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. 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.
Structured grids. Types and transformations. Generation of structured grids. Unstructured grids. Delany triangulation.
Page
GRID GENERATION
43
Module-III
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
5th Semester
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.
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.
Page
44
4. Anderson, Jr.D., “Fundamentals of Aerodynamics”, McGraw-Hill, 2000.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
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 Propulsion-II
3-0
3
100
50
2
1
50
3-0 3-1
3 4
100 100
50 50
2
1
50
3-1
4
3-0
3
2-0
1
50
3 4
1 2
50 100
2 13
1 6
50 300
PE 100
MC & GS OE
Composite Material & Structure/NonDestructive Testing/High Temperature Materials Aircraft General Engineering & Maintenance/Flight Schedule & Operation/Airport Planning &Management Environmental Science & Engineering Industrial Lecture #
HS
Business Communication & Skill for Interview # #
MC
Yoga
Total Total Marks: 1100 Total Credits: 24 Aero engine Honours
Minor
Repair & Maintenance/ NonDestructive Testing/ Industrial Aerodynamics Aircraft Structures-I
50
100
50
19
18
500
300
4
4
100
50
43
PE
Page
PC
5. 6. 7. 8. 9. 10. 11. 12.
PAE6G001 PAE6H301 PAE6I101 PAE6I102 PAE6J001 PAE6J002 PAE6J003 PAE6J004
Minor(CP) OE(CP) PC(CP) PC(CP) PE(O1) PE(O1) PE(O1) PE(O2)
13. 14.
PAE6J005 PE(O2) PAE6J006 PE(O2)
Aero engine Repair & Maintenance Non-Destructive Testing Industrial Aerodynamics Business Communication & Skill for Interview Aircraft Structures-I Industrial Lecture # Aircraft Stability & Control Propulsion - II Composite Material & Structure Non-Destructive Testing High Temperature Materials Aircraft General Engineering & Maintenance Flight Schedule & Operation Airport Planning & Management
4-0-0 4-0-0 4-0-0 1-0-2
4 4 4 3
4-0-0 0-0-1 3-0-1 3-0-1 4-0-0 4-0-0 4-0-0 4-0-0
4 1 4 4 4 4 4 4
4-0-0 4-0-0
4 4 --28 ---
44
Semester : 6th -------------1. PAE6D001 Honours(O3) 2. PAE6D002 Honours(O3) 3. PAE6D003 Honours(O3) 4. PAE6E101 HS(CP)
6th Semester
Page
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6I101 AIRCRAFT STABILITY & CONTROL (3-0-1) OBJECTIVE: To make the student understand the concepts of stable and nonstable configuration of airplanes. To introduce the concepts of control of airplanes under various operating conditions. Module – I STATIC LONGITUDINAL STABILITY AND CONTROL General concepts-Degrees of freedom of a rigid body, Static and dynamic stability, Need for stability in an airplane, inherently and marginally stable airplanes, Stability and Controllability, Requirements of control surfaces, criteria for longitudinal static stability, contribution to stability by wing, tail, fuselage, wing fuselage combination, Total longitudinal stability, Neutral point-Stick fixed and Stick free aspects, Free elevator factor, static margin, Hinge moment, Power effects on stability-propeller and jet aircrafts, longitudinal control, Movement of centre of gravity, elevator control effectiveness, elevator control power, elevator angle to trim, elevator angle per g, maneuver point, Stick force gradient and stick force per g, Aerodynamic balancing Module – II STATIC DIRECTIONAL STABILITY AND CONTROL Directional stability-yaw and sideslip, Criterion of directional stability, contribution to static directional stability by wing, fuselage, tail, Power effects on directional stabilitypropeller and jet aircrafts, Rudder lock and Dorsal fin, Directional control, rudder control effectiveness, rudder requirements, adverse yaw, asymmetric power condition, spin recovery Module – III STATIC LATERAL STABILTY AND CONTROL Lateral stability-Dihedral effect, criterion for lateral stability, evaluation of lateral stabilitycontribution of fuselage, wing, wing fuselage, tail, total static lateral stability, lateral control, aileron reversal, aileron reversal speed Module – IV DYNAMIC LONGITUDINAL STABILITY Aircraft Equations of motion, small disturbance theory, Estimation of longitudinal stability derivatives stability derivatives, solving the stability quartic, Phugoid motion. Module – V DYNAMIC LATERAL AND DIRECTIONAL STABILITY Dutch roll and spiral instability, Auto rotation and spin, TEXT BOOKS 1. Perkins C.D. & Hage R.E. Airplane performance, stability and control, John Wiley & Sons 1976. 1. Nelson, R.C. Flight Stability & Automatic Control, McGraw Hill, 1998.
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REFERENCES 1. McCormick, B.W. Aerodynamics, Aeronautics & Flight Mechanics John Wiley, 1995. 1. Babister, A.W. Aircraft Stability and response, Pergamon Press, 1980 2. Etkin, B., Dynamics of Flight Stability and Control, John Wiley, New York, 1982. 3. Pamadi, B.N. Performnce, Stability, Dynamics, and Control of Airplanes, AIAA, Education Series, 2004
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
AIRCRAFT STABILITY & CONTROL LAB LIST OF EXPERIMENTS 1. 2. 3. 4. 5. 6. 7. 8. 9. 10.
Force measurement in an aircraft model using wind tunnel Finding out the CG location of different aircraft model Calculation of Neutral point Density altitudes, and weather situations using a/c simulator Pitching control Rolling Control Yawing control Rudder designing Stick force Calculation of stability
PAE6I102 PROPULSION – II (3-0-1) OBJECTIVE To study in detail about gas turbines, ramjet, fundamentals of rocket propulsion and chemical rockets Module – I
AIRCRAFT GAS TURBINES
Impulse and reaction blading of gas turbines – Velocity triangles and power output – Elementary theory – Vortex theory – Choice of blade profile, pitch and chord – estimation of stage performance – Limiting factors in gas turbine design- Overall turbine performance – Methods of blade cooling. Module – II
RAMJET PROPULSION:
Operating principle – Sub critical, critical and supercritical operation – Combustion in ramjet engine – Ramjet performance – Simple ramjet design calculations – Introduction to scramjet. Module – III
FUNDAMENTALS OF ROCKET PROPULSION
Operating principle – Specific impulse of a rocket – internal ballistics- Rocket nozzle classification – Rocket performance considerations. Module – IV
CHEMICAL ROCKETS
Solid propellant rockets – Selection criteria of solid propellants – Important hardware components of solid rockets – Propellant grain design considerations – Liquid propellant rockets – Selection of liquid propellants. Cooling in liquid rockets – Hybrid rockets. Module – V ADVANCED PROPULSION TECHNIQUES
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Electric rocket propulsion – Ion propulsion techniques – Nuclear rocket – Types – Solar sailPreliminary Concepts in nozzleless propulsion.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
TEXT BOOKS 1. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 5th Edn., 1993. 2. Hill, P.G. & Peterson, C.R. “Mechanics & Thermodynamics of Propulsion” Addison – Wesley Longman INC, 1999. REFERENCES 1. Cohen, H., Rogers, G.F.C. and Saravanamuttoo, H.I.H., “Gas Turbine Theory”, Longman Co., ELBS Ed., 1989. 2. Gorden, C.V., “Aero thermodynamics of Gas Turbine and Rocket Propulsion”, AIAA Education Series, New York, 1989. 3. Mathur, M., and Sharma, R.P., “Gas Turbines and Jet and Rocket Propulsion”, Standard Publishers, New Delhi, 1988.
PROPULSION – II LIST OF EXPERIMENTS
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1.Cascade testing Combustion Studies in a model jet engine combustor. Flame stabilization studies using conical flame holders. Methods of preparing the propellant Study of hybrid rocket propulsion system Burn rate measurements of solid propellants Ignition delay measurements of solid propellants. Velocity and pressure measurements of co-axial jets 9.Flow visualization of secondary injection in a supersonic cross flow Supersonic external flow visualization over a supersonic free jet.
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1. 2. 3. 4. 5. 6. 7. 8. 9. 10.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6J001 COMPOSITE MATERIALS AND STRUCTURES (4-0-0) OBJECTIVE To understand the fabrication, analysis and design of composite materials & structures. Module-I STRESS STRAIN RELATION Introduction- Advantages and application of composite materials, reinforcements and matrices – Generalised Hooke‟s Law – Elastic constants for anisotropic, orthotropic and isotropic materials. Module-II METHODS OF ANALYSIS Micro mechanics – Mechanics of materials approach, elasticity approach to determine material properties – Macro Mechanics – Stress-strain relations with respect to natural axis, arbitrary axis – Determination of material properties. Experimental characterization of lamina. Module-III LAMINATED PLATES Governing differential equation for a general laminate, angle ply and cross ply laminates. Failure criteria for composites. Module-IV SANDWICH CONSTRUCTIONS Basic design concepts of sandwich construction -Materials used for sandwich construction - Failure modes of sandwich panels. Module-V FABRICATION PROCESSES Various Open and closed mould processes. Manufacture of fibers – Types of resins and properties and applications – Netting analysis. TEXT BOOKS 1. Calcote, L R. “The Analysis of laminated Composite Structures”, Von – Noastrand Reinhold Company, New York 1998. 2. Jones, R.M., “Mechanics of Composite Materials”, McGraw-Hill, Kogakusha Ltd., Tokyo, 1998, II edition.
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REFERENCES 1. Agarwal, B.D., and Broutman, L.J., “Analysis and Performance of Fibre Composites”, John Wiley and sons. Inc., New York, 1995. 2. Lubin, G., “Handbook on Advanced Plastics and Fibre Glass”, Von Nostrand Reinhold Co., New York, 1989.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6J002 NON-DESTRUCTIVE TESTING (4-0-0) UNIT I : INTRODUCTION TO NDT NDT Versus Mechanical testing, Need for Nondestructive testing Relative merits and limitations, Various physical characteristics of materials and their applications in NDT., Visual inspection – Unaided and aidedStandards UNIT II : SURFACE NDE METHODS Liquid Penetrant Testing – Principles, types and properties of liquid penetrants, developers, advantages and limitations of various methods, Testing Procedure, Interpretation of results. Magnetic Particle TestingTheory of magnetism, inspection materials Magnetisation methods, Interpretation and evaluation of test indications, Principles and methods of demagnetization, Residual magnetism. UNIT III : THERMOGRAPHY AND EDDY CURRENT TESTING (ET) Thermography- Principles, Contact and non contact inspection methods, Techniques for applying liquid crystals, Advantages and limitation – infrared radiation and infrared detectors, Instrumentations and methods, applications. Eddy Current Testing-Generation of eddy currents, Properties of eddy currents, Eddy current sensing elements, Probes, Instrumentation, Types of arrangement , Applications, advantages, Limitations, Interpretation/Evaluation. UNIT IV : ULTRASONIC TESTING (UT) AND ACOUSTIC EMISSION (AE) Ultrasonic TestingPrinciple, Transducers, transmission and pulse-echo method, straight beam and angle beam, instrumentation, data representation, A-Scan, B-Scan, C-Scan. Phased Array Ultrasound, Time of Flight Diffraction. Acoustic Emission Technique –Principle, AE parameters, Applications. UNIT V : RADIOGRAPHY (RT) Principle, interaction of X-Ray with matter, imaging, film and film less techniques, types and use of filters and screens, geometric factors, Inverse square law, characteristics of films – graininess, density, speed, contrast, characteristic curves, Penetrameters, Exposure charts, Radiographic equivalence. Fluoroscopy- Xero-Radiography, Computed Radiography, Computed Tomography- Gamma ray Radiography, Safety in X- ray and gamma ray radiography. TEXT BOOKS: 1. Baldev Raj, T.Jayakumar, M.Thavasimuthu “Practical Non-Destructive Testing”, Narosa Publishing House, 2009. 2. Ravi Prakash, “Non-Destructive Testing Techniques”, 1st Revised Edition, New Age International Publishers, 2010
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REFERENCES: 1. ASM Metals Handbook,”Non-Destructive Evaluation and Quality Control”, American Society of Metals, Metals Park, Ohio, USA, 200, Volume-17. 2. Paul E Mix, “Introduction to nondestructive testing: a training guide”, 2nd Edition, Wiley, New Jersey, 2005 3. Charles, J. Hellier,“ Handbook of nondestructive evaluation”, McGraw Hill, New York 2001. 4. ASNT, American Society for Non Destructive Testing, Columbus, Ohio, NDT Handbook, Vol. 1, Leak Testing, Vol. 2, Liquid Penetrant Testing, Vol. 3, Infrared and Thermal Testing Vol. 4, Radiographic Testing, Vol. 5, Electromagnetic Testing, Vol. 6, Acoustic Emission Testing, Vol. 7, Ultrasonic Testing.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6J003 HIGH TEMPERATURE MATERIALS (4-0-0) OBJECTIVE To learn damage mechanism and failure of components of elevated temperatures UNIT I CREEP Factors influencing functional life of components at elevated temperatures, definition of creep curve, various stages of creep, metallurgical factors influencing various stages, effect of stress, temperatures and strain rate. UNIT II DESIGN FOR CREEP RESISTANCE Design of transient creep time, hardening, strain hardening, expressions of rupture life of creep, ductile and brittle materials, Monkman-Grant relationship. UNIT III FRACTURE Various types of fracture, brittle to ductile from low temperature to high temperature, cleavage fracture due to micro void coalescence – diffusion controlled void growth; fracture maps for different alloys and oxides. UNIT IV OXIDATION AND HOT CORROSION Oxidation, Pilling, Bedworth ratio, kinetic laws of oxidation – defect structure and control of Oxidation by alloy additions, hot gas corrosion deposit, modified hot gas corrosion, fluxing mechanisms, effect of alloying elements on hot corrosion, interaction of hot corrosion and creep, methods of combat hot corrosion. UNIT V SUPER ALLOYS AND OTHER MATERIALS Iron base, Nickel base abd Cobalt base super alloys, composition control, solid solution strengthening, precipitation hardening by gamma prime, grain boundary strengthening, TCP phase, embrittlement, solidfication of single crystals, Intermetallics, high temperature ceramics. TEXT BOOKS 1. Raj. R., “Flow and Fracture at Elevated Temperatures”,American Society for Metals USA, 1985. 2. Hertzberg R.W., “Deformation and Fracture Mechanics of Engineering materials”, 4th Edition, John Wiley, USA, 1996. 3. Courtney T .H, “Mechanical Behaviour of Materials”,McGraw-Hill, USA, 1990.
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REFERENCES 1. Boyle J.T, Spencer J, “Stress Analysis for Creep” ,Butterworths, UK, 1983. 2. Bressers.J., “Creep and Fatigue in High Temperature Alloys”, Applied Science, 1981. 3. McLean D., “Directionally Solidified Materials for High Temperature Service”, The Metals Society, USA, 1985.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6J004 AIRCRAFT GENERAL ENGINEERING AND MAINTENANCE (4-0-0) OBJECTIVE To teach the students about the basic concepts of aircraft general engineering and maintenance practices. UNIT I AIRCRAFT GROUND HANDLING AND SUPPORT EQUIPMENT Mooring, jacking, leveling and towing operations – Preparation – Equipment – precautions – Engine starting procedures – Piston engine, turboprops and turbojets – Engine fire extinguishing – Ground power unit. UNIT II GROUND SERVICING OF VARIOUS SUB SYSTEMS Air conditioning and pressurization – Oxygen and oil systems – Ground units and their maintenance. UNIT III MAINTENANCE OF SAFETY Shop safety – Environmental cleanliness – Precautions UNIT IV INSPECTION Process – Purpose – Types – Inspection intervals – Techniques – Checklist – Special inspection – Publications, bulletins, various manuals – FAR Air worthiness directives – Type certificate Data sheets – ATA Specifications. UNIT V AIRCRAFT HARDWARE, MATERIALS, SYSTEM PROCESSES Hand tools – Precision instruments – Special tools and equipments in an airplane maintenance shop – Identifiation terminology – Specification and correct use of various aircraft hardware (i.e. nuts, bolts, rivets, screws etc) – American and British systems of specifications – Threads, gears, bearings, etc – Drills, tapes and reamers – Identification of all types of fluid line fittings. Materials, metallic and non-metallic = Plumbing connectors – Cables – Swaging procedures, tests, Advantages of swaging over splicing. TEXT BOOK 1. Kroes Watkins Delp, Aircraft Maintenance and Repair, McGraw Hill, New York, 1993.
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REFERENCES: 1. A&P Mechanics, Aircraft Hand Book, F A A Himalayan Book House, New Delhi, 1996 2. A&P Mechanics, General Hand Book, F A A Himalayan Bok House, New Delhi, 1996
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6J005 FLIGHT SCHEDULE AND OPERATION (4-0-0) MODULE 1 : Introduction Duties and responsibilities of FOO/OCO Organisation of an air carrier, operational process description Safety, Regularity, Economy and Punctuality (role of dispatch/operations control) Safety and Quality Management System introduction, Dispatch Etiquette MODULE 2: Air Law General International bodies (ICAO, FAA, EASA, IATA, CAAs), Warsaw, Chicago conventions, freedoms of the air, ICAO Annexes, CAAs (Role, regulations, sovereignty, overflight/landing permissions, power of authority), EU OPS Air Carrier's Operations Manual (OM A, B. C.D), Eurocontrol MODULE 3: Flight Scheduling Feasibility of the flight Flight time/Block time considerations, Airport slots (coordinated airports, IATA SSIM, messages, SCR, SMA) Airport restrictions, adequacy and suitability, of aerodromes, airport categorisation Sector limitations, Fuel stop considerations, Crew duty and rest time regulations, Airport ground handling and fuel services, MODULE 4: ATC and Air Traffic ATC services (ATC, AIS/ARO, segments and units, CLR, GRD, TWR, APP/DEP, ACC) Airspace (airways, special use of airspace, airspace classification, flight rules) ICAO ATS Flight Plan, NOTAMs, Eurocontrol, Air Traffic Management, ATC Slots, Capacity management Airports RVSM Oceanic control
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MODULE 5: Flight Planning Introduction to flight planning, Route and profile planning, Time, speed and fuel calculations, Weather considerations. Aircraft performance considerations, Aircraft technical status considerations, Operational Flight Plan, Alternate airports selection, Practical flight planning exercises. Advanced dispatch techniques introduction
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6J006 AIRPORT PLANNING AND MNAGEMENT (4-0-0) MODULE 1 : Aviation industry & its regulatory authorities: Intorduction, history of aviation-evolution, development, growth, challenges. Aerospace industry, air transportion industry-economic impact- types and causes. Airline Industry-structure and economic characteristics. The bredth of regulation- ICAO, IATA, national authorities (DGCA, FAA). Safety regulations-risk assessment-human factors and safety, security regulations, envioronmental regulations. MODULE 2: THE SYSTEM ELEMENTS – AIRCRAFT The system elements – the aircraft, airlines, airports, airspace. Aircraft - costs, compatibility with objectives, and operational infrastructure, direct and indirect operating costs, safety, security, efficiency and effectiveness. AIRLINES – OBJECTIVES, PLANNING, OPERATIONS – PROCEDURES Route selection and development, fleet planning and acquisition, airline schedule development, fleet assignment, aircraft routing, gate assignment, flight operations - irregular operations, schedule recovery and robustness. Maintenance of aircraft and equipment. Airline operating costs and measure of productivity.
MODULE 3: Airport: Setting up an airport-airport demand, airport siting, runway chracteristics-length, declared distances, aerodrome areas, obstacle safegurarding. Runway capacity- evaluating runway capacity -sustainablerunway capacity. Runway pavement length, Manoeuvring area- airfield lighting, aprons, Passenger terminalsterminal sizing and configuration. Airport demand, capacity and delay. Air traffic control and surveillance facilities located on the airfield. The basics of air traffic control. MODULE 4: Airport operation and Financial Management Airport operations management under FAR Part 139- Introduction; Pavement management; Aircraft rescue and fire fighting (ARFF); Snow and ice control; Safety inspection programs; Airport financial managementIntroduction; Airport financial accounting ;Revenue strategies at commercial airports ;Pricing of airport facilities and services ; Variation in the sources of operating revenues; Rise in airport financial burdens ;Airport funding ;Grant programs ;Airport financing. MODULE 5: Airport operation and Financial Management Categories of airspac-separation minima, airspace sectors-capacity, demand and delay. Evolution of air traffic control system-procedural ATC system, procedural ATC with radar assistance, first generation „automated‟ ATC system, current generation radar and computer-based ATC systems. Aerodrome air traffic control equipment and operation-ICAO future air-navigation system servise provides as businesses. TEXT BOOKS 1. Hirst, M., The Air Transport System,Woodhead Publishing Ltd,Cambridge, England, 2008. 2.
AIRPORT PLANNING AND MANAGEMENT BY Alexander T. Wells, Seth B. Young.
3.
AIRPORT PLANNING AND DESIGN BY S. K. Khanna, M. G. Arora
Belobaba,P.,Odoni,A.and Barnhart,C.,Global Airline Industry, Wiley,2009.
3.
M.Bazargan,M., Airline operations and Scheduling Ashgate, 2004.
4.
Nolan,M.s., Fundamentals of Air Traffic Control,fourth edn., Thomson Learning, 2004.
5.
Wells, A. and young, S.,Airport Planning and Management, fifth edn., McGraw-Hill, 1986.
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REFERENCES 1. Wensven, J.G.,Air Transportion:A Management Perspective, Ashgate, 2007.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PMG6M001 ENVIRONMENTAL SCIENCE AND ENGINEERING (3-0-0)
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Module II Ecosystems Concept of an ecosystem. Structure and function of an ecosystem. Producers, consumers and decomposers. Energy flow in the ecosystem. Ecological succession. Food chains, food webs and ecological pyramids. Introduction, types, characteristic features, structure and function of the following ecosystem :a) Forest ecosystem b) Grassland ecosystem c) Desert ecosystem d) Aquatic ecosystems (ponds, streams, lakes, rivers, oceans, estuaries) Environmental Pollution Definition Cause, effects and control measures of :a) Air pollution b) Water pollution c) Soil pollution d) Marine pollution e) Noise pollution f) Thermal pollution g) Nuclear hazards Solid waste Management: Causes, effects and control measures of urban and industrial wastes. Role of an individual in prevention of pollution.
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Module I Multidisciplinary nature of environmental studies Definition, scope and importance, Need for public awareness. Natural Resources: Renewable and non-renewable resources: Natural resources and associated problems. a) Forest resources: Use and over-exploitation, deforestation, case studies. Timber extraction, mining, dams and their effects on forest and tribal people. b) Water resources: Use and over-utilization of surface and ground water, floods, drought, conflicts over water, dams-benefits and problems. c) Mineral resources: Use and exploitation, environmental effects of extracting and using mineral resources, case studies. d) Food resources: World food problems, changes caused by agriculture and overgrazing, effects of modern agriculture, fertilizer-pesticide problems, water logging, salinity, case studies. e) Energy resources: Growing energy needs, renewable and non renewable energy sources, use of alternate energy sources. Case studies. f) Land resources: Land as a resource, land degradation, man induced landslides, soil erosion and desertification. Role of an individual in conservation of natural resources. Equitable use of resoureces for sustainable lifestyles.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
Pollution case studies. Disaster management: floods, earthquake, cyclone and landslides. Module III Social Issues and the Environment From Unsustainable to Sustainable development Urban problems related to energy Water conservation, rain water harvesting, watershed management Resettlement and rahabilitation of people; its problems and concerns. Case Studies Environmental ethics : Issues and possible solutions. Climate change, global warming, acid rain, ozone layer depletion, nuclear accidents and holocaust. Case Studies. Wasteland reclamation. Consumerism and waste products. Environment Protection Act. Air (Prevention and Control of Pollution) Act. Water (Prevention and control of Pollution) Act Wildlife Protection Act Forest Conservation Act Issues involved in enforcement of environmental legislation. Public awareness.
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References 1. Agarwal, K.C. 2001 Environmental Biology, Nidi Publ. Ltd. Bikaner. 2. R. Rajagopalan, Environmental Studies, Oxford University Press. 3. Ajith Sankar, Environmental Management, Oxford University Press. 4. Bharucha Erach, The Biodiversity of India, Mapin Publishing Pvt. Ltd., Ahmedabad – 380 013, India, Email:
[email protected] (R) 5. Brunner R.C., 1989, Hazardous Waste Incineration, McGraw Hill Inc. 480p 6. Clark R.S., Marine Pollution, Clanderson Press Oxford (TB) 7. Cunningham, W.P. Cooper, T.H. Gorhani, E & Hepworth, M.T. 2001, Environmental Encyclopedia, Jaico Publ. House, Mumabai, 1196p 8. De A.K., Environmental Chemistry, Wiley Eastern Ltd. 9. Down to Earth, Centre for Science and Environment (R)
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Module IV Human Population and the Environment Population growth, variation among nations. Population explosion – Family Welfare Programme. Environment and human health. Human Rights. Value Education. HIV/AIDS. Women and Child Welfare. Role of Information Technology in Environment and human health. Case Studies.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PEN6E101 BUSINESS COMMUNICATION AND SKILL FOR INTERVIEW Course Objectives
To develop communication competence in prospective engineers. To enable them to convey thoughts and ideas with clarity and focus. To develop report writing skills. To equip them to face interview & Group Discussion. To inculcate critical thinking process. To prepare them on problem solving skills. To provide symbolic, verbal, and graphical interpretations of statements in a problem description. To understand team dynamics & effectiveness. To create an awareness on Engineering Ethics and Human Values. To install Moral and Social Values, Loyalty and also to learn to appreciate the rights of others. To learn leadership qualities and practice them.
MODULE I Communication Skill: Introduction to Communication, The Process of Communication, Barriers to Communication, Listening Skills, Writing Skills, Technical Writing, Letter Writing, Job Application, Report Writing, Non-verbal Communication and Body Language, Interview Skills, Group Discussion, Presentation Skills, Technology-based Communication. MODULE II Critical Thinking & Problem Solving: Creativity, Lateral thinking, Critical thinking, Multiple Intelligence, Problem Solving, Six thinking hats, Mind Mapping & Analytical Thinking. Teamwork: Groups, Teams, Group Vs Teams, Team formation process, Stages of Group, Group Dynamics, Managing Team Performance & Team Conflicts. MODULE III Ethics, Moral & Professional Values: Human Values, Civic Rights, Engineering Ethics, Engineering as Social Experimentation, Environmental Ethics, Global Issues, Code of Ethics like ASME, ASCE, IEEE. MODULE IV Leadership Skills: Leadership, Levels of Leadership, Making of a leader, Types of leadership, Transactions Vs Transformational Leadership, VUCA Leaders, DART Leadership, Leadership Grid & leadership Formulation.
Communicate effectively. Make effective presentations. Write different types of reports. Face interview & group discussion. Critically think on a particular problem. Solve problems. Work in Group & Teams Handle Engineering Ethics and Human Values. Become an effective leader.
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Expected outcome: The students will be able to
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
References:
1. Barun K. Mitra; (2011), “Personality Development & Soft Skills”, First Edition; Oxford Publishers. 2. Kalyana; (2015) “Soft Skill for Managers”; First Edition; Wiley Publishing Ltd. 3. Larry James (2016); “The First Book of Life Skills”; First Edition; Embassy Books. 4. Shalini Verma (2014); “Development of Life Skills and Professional Practice”; First Edition; Sultan Chand (G/L) & Company 5. John C. Maxwell (2014); “The 5 Levels of Leadership”, Centre Street, A division of Hachette Book Group Inc.
PAE6D001 AERO ENGINE REPAIRS AND MAINTENANCE (HONOR) (4-0-0) AIM: To make the students to familiarize with the Aircraft engine maintenance procedure and practice. Pre-requisite: Must have knowledge of basics of Aeronautics and engine components. UNIT I Classification of piston engines - Principles of operation - Function of components - Materials used - Details of starting the engines - carburetion and Fuel injection systems for small and large engines - Ignition system components - spark plug detail - Engine operating conditions at various altitudes – Engine power measurements – Classification of engine lubricants and fuels – Induction, Exhaust and cooling system - Maintenance and inspection check to be carried out. Inspection and maintenance and trouble shooting - Inspection of all engine components - Daily and routine checks - Overhaul procedures - Compression testing of cylinders - Special inspection schedules - Engine fuel, control and exhaust systems - Engine mount and super charger - Checks and inspection procedures. UNIT II Propeller theory - operation, construction assembly and installation -Pitch change mechanismPropeller axie system- Damage and repair criteria - General Inspection procedures - Checks on constant speed propellers - Pitch setting, Propeller Balancing, Blade cuffs, Governor/Propeller operating conditions – Damage and repair criteria.
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UNIT IV Types of jet engines – Fundamental principles – Bearings and seals - Inlets - compressors- turbinesexhaust section – classification and types of lubrication and fuels- Materials used - Details of control, starting around running and operating procedures – Inspection and Maintenancepermissible limits of damage and repair criteria of engine components- internal inspection of engines- compressor washingfield balancing of compressor fans- Component maintenance procedures – Systems maintenance procedures - use of instruments for online maintenance – Special inspection procedures-Foreign Object Damage - Blade damage .
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UNIT III Symptoms of failure - Fault diagnostics - Case studies of different engine systems - Rectification during testing equipments for overhaul: Tools and equipments requirements for various checks and alignment during overhauling - Tools for inspection - Tools for safety and for visual inspection Methods and instruments for non destructive testing techniques - Equipment for replacement of parts and their repair. Engine testing: Engine testing procedures and schedule preparation – Online maintenance.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
UNIT V Engine Overhaul - Overhaul procedures - Inspections and cleaning of components - Repairs schedules for overhaul - Balancing of Gas turbine components. Trouble Shooting: Procedures for trouble shooting - Condition monitoring of the engine on ground and at altitude - engine health monitoring and corrective methods. REFERENCES 1. Kroes & Wild, " Aircraft Power plants ", 7th Edition - McGraw Hill, New York, 1994. 2. Turbomeca, " Gas Turbine Engines ", The English Book Store ", New Delhi, 1993. 3. United Technologies Pratt & Whitney, " The Aircraft Gas turbine Engine and its Operation” The English Book Store, New Delhi.
PAE6D002 NON-DESTRUCTIVE TESTING (HONOR) (4-0-0) UNIT I : INTRODUCTION TO NDT NDT Versus Mechanical testing, Need for Nondestructive testing Relative merits and limitations, Various physical characteristics of materials and their applications in NDT., Visual inspection – Unaided and aidedStandards UNIT II : SURFACE NDE METHODS Liquid Penetrant Testing – Principles, types and properties of liquid penetrants, developers, advantages and limitations of various methods, Testing Procedure, Interpretation of results. Magnetic Particle TestingTheory of magnetism, inspection materials Magnetisation methods, Interpretation and evaluation of test indications, Principles and methods of demagnetization, Residual magnetism. UNIT III : THERMOGRAPHY AND EDDY CURRENT TESTING (ET) Thermography- Principles, Contact and non contact inspection methods, Techniques for applying liquid crystals, Advantages and limitation – infrared radiation and infrared detectors, Instrumentations and methods, applications. Eddy Current Testing-Generation of eddy currents, Properties of eddy currents, Eddy current sensing elements, Probes, Instrumentation, Types of arrangement , Applications, advantages, Limitations, Interpretation/Evaluation. UNIT IV : ULTRASONIC TESTING (UT) AND ACOUSTIC EMISSION (AE) Ultrasonic TestingPrinciple, Transducers, transmission and pulse-echo method, straight beam and angle beam, instrumentation, data representation, A-Scan, B-Scan, C-Scan. Phased Array Ultrasound, Time of Flight Diffraction. Acoustic Emission Technique –Principle, AE parameters, Applications.
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TEXT BOOKS: 3. Baldev Raj, T.Jayakumar, M.Thavasimuthu “Practical Non-Destructive Testing”, Narosa Publishing House, 2009. 4. Ravi Prakash, “Non-Destructive Testing Techniques”, 1st Revised Edition, New Age International Publishers, 2010
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UNIT V : RADIOGRAPHY (RT) Principle, interaction of X-Ray with matter, imaging, film and film less techniques, types and use of filters and screens, geometric factors, Inverse square law, characteristics of films – graininess, density, speed, contrast, characteristic curves, Penetrameters, Exposure charts, Radiographic equivalence. Fluoroscopy- Xero-Radiography, Computed Radiography, Computed Tomography- Gamma ray Radiography, Safety in X- ray and gamma ray radiography.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
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REFERENCES: 5. ASM Metals Handbook,”Non-Destructive Evaluation and Quality Control”, American Society of Metals, Metals Park, Ohio, USA, 200, Volume-17. 6. Paul E Mix, “Introduction to nondestructive testing: a training guide”, 2nd Edition, Wiley, New Jersey, 2005 7. Charles, J. Hellier,“ Handbook of nondestructive evaluation”, McGraw Hill, New York 2001. 8. ASNT, American Society for Non Destructive Testing, Columbus, Ohio, NDT Handbook, Vol. 1, Leak Testing, Vol. 2, Liquid Penetrant Testing, Vol. 3, Infrared and Thermal Testing Vol. 4, Radiographic Testing, Vol. 5, Electromagnetic Testing, Vol. 6, Acoustic Emission Testing, Vol. 7, Ultrasonic Testing.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6D003 INDUSTRIAL AERODYNAMICS (HONOR) (4-0-0) UNIT I ATMOSPHERE Types of winds, Causes of variation of winds, Atmospheric boundary layer, Effect of terrain on gradient height, Structure of turbulent flows. UNIT II WIND ENERGY COLLECTORS Horizontal axis and vertical axis machines, Power coefficient, Betz coefficient by momentum theory. UNIT III VEHICLE AERODYNAMICS Power requirements and drag coefficients of automobiles, Effects of cut back angle, Aerodynamics of trains and Hovercraft. UNIT IV BUILDING AERODYNAMICS Pressure distribution on low rise buildings, wind forces on buildings. Environmental winds in city blocks, Special problems of tall buildings, Building codes, Building ventilation and architectural aerodynamics. UNIT V FLOW INDUCED VIBRATIONS Effects of Reynolds number on wake formation of bluff shapes, Vortex induced vibrations, galloping and stall flutter. TEXT BOOKS 1. M.Sovran (Ed), “Aerodynamics and drag mechanisms of bluff bodies and road vehicles”, Plenum press, New York, 1978. 2. P. Sachs, “Winds forces in engineering”, Pergamon Press, 1978.
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REFERENCES 1. R.D. Blevins, “Flow induced vibrations”, Van Nostrand, 1990. 2. N.G. Calvent, “Wind Power Principles”, Charles Griffin & Co., London, 1979.
B. Tech (Aeronautical Engineering) Syllabus for Admission Batch 2015-16
6th Semester
PAE6G001 AIRCRAFT STRUCTURES – I (MINOR) (4-0-0) UNIT I STATICALLYDETERMINATESTRUCTURES Analysis of plane Truss-Method of joints-3 D Truss-Plane frames-Composite beam. UNIT II
STATICALLY INDETERMINATE STRUCTURES
Propped Cantilever- Fixed-Fixed beams-Clapeyron's Three Moment Equation – Moment Distribution Method. UNIT III
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 IV
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 V
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
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1. Timoshenko, S., “Strength of Materials”, Vol. I and II, Princeton D. Von Nostrand Co, 1990.
