aeronautical v visem new

8/8/2019 Aeronautical v VISEM New

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SEMESTER VI

Code No. Course Title L T P M C

Aircraft General Engineering andMaintenance Practices *

3 0 0 100 3

Propulsion-II 3 0 0 100 3

Heat Transfer 3 0 0 100 3

Experimental Stress Analysis 3 0 0 100 3

Aircraft Stability And Control 3 0 0 100 3

Elective I 3 0 0 100 3

PRACTICAL

Aircraft Design Lab - I 0 0 3 50 1.5

CAD Lab 0 0 3 100 1.5Propulsion Lab 0 0 3 100 1.5

Presentation Skills and TechnicalSeminar

0 0 3 0 1.5

*Revised Syllabus

ELECTIVES I FOR VI SEMESTER

Code No. Course Title L T P M C

Theory of Elasticity 3 0 0 100 3

Space Mechanics 3 0 0 100 3

Principles of Management 3 0 0 100 3

Wind Tunnel Techniques 3 0 0 100 3

Intellectual Property Rights (IPR) 3 0 0 100 3

Indian Constitution and Society 3 0 0 100 3


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SEMESTER V

AIRCRAFT RULES AND REGULATIONSL T P M C3 0 0 100 3

OBJECTIVE

To teach the civil air rules and regulations which are being followed byDirectorate General of Civil Aviation.

1. C.A.R. SERIES A PROCEDURE FOR CIVIL AIR WORTHINESSREQUIREMENTS AND RESPONSIBILITY OPERATORS Vis--vis AIRWORTHINESS DIRECTORATE 8

Responsibilities of operators / owners- Procedure of CAR issue, amendmentsetc., Objectives and targets of airworthiness directorate; Airworthinessregulations and safety oversight of engineering activities of operators.

C.A.R. SERIES B ISSUE APPROVAL OF COCKPIT CHECK LIST, MEL,CDL: Deficiency list (MEL & CDL); Preparation and use of cockpit checklist andemergency list.

2. C.A.R. SERIES C DEFECT RECORDING, MONITORING,INVESTIGATION AND REPORTING 7

Defect recording, reporting, investigation, rectification and analysis; Flight report;

Reporting and rectification of defects observed on aircraft; Analytical study of in-flight readings & recordings; Maintenance control by reliability Method.

C.A.R. SERIES D AND AIRCRAFT MAINTENANCE PROGRAMMESReliability Programmes (Engines); Aircraft maintenance programme & theirapproval; On condition maintenance of reciprocating engines; TBO Revisionprogramme; Maintenance of fuel and oil uplift and consumption records Lightaircraft engines; Fixing routine maintenance periods and component TBOs Initial & revisions.

3. C.A.R. SERIES E APPROVAL OF ORGANISATIONS 10

Approval of organizations in categories A, B, C, D, E, F, & G - Requirements ofinfrastructure at stations other than parent base.

C.A.R. SERIES F AIR WORTHINESS AND CONTINUED AIRWORTHINESS: Procedure relating to registration of aircraft; Procedure for issue

/ revalidation of Type Certificate of aircraft and its engines / propeller; Issue /revalidation of Certificate of Airworthiness; Requirements for renewal ofCertificate of Airworthiness.


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4. C.A.R. SERIES L&M 8

Issue of AME Licence, its classification and experience requirements, MandatoryModifications / Inspections.

5. C.A.R. SERIES T&X 12

Flight testing of (Series) aircraft for issue of C of A; Flight testing of aircraft for

which C of A had been previously issued. Registration Markings of aircraft;Weight and balance control of an aircraft; Provision of first aid kits & Physicianskit in an aircraft; Use furnishing materials in an aircraft; Concessions; Aircraft logbooks; Document to be carried on board on Indian registered aircraft; Procedurefor issue of tax permit; Procedure for issue of type approval of aircraftcomponents and equipment including instruments.

TOTAL : 45TEXT BOOKS

1. Civil Aviation Requirements with latest Amendment (Section 2Airworthiness) Published by DGCA, The English Book Store, 17-1,Connaught Circus, New Delhi 2000.

2. Aeronautical Information Circulars (relating to Airworthiness) from DGCA2000.

REFERENCES

1. Aircraft Manual (India) Volume Latest Edition, the English Book Store,17-1, Connaught Circus, New Delhi.

2. Advisory Circulars from DGCA 2003.


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AIRCRAFT PERFORMANCEL T P M C3 0 0 100 3

1 .LIFT AND DRAG ON FLIGHT PERFORMANCE 12

Streamlined and bluff bodies, aerofoil classification, Aerofoil characteristics,Pressure distribution around aerofoils.. Types of drag, Effects of Reynoldsnumber on skin friction and pressure drag, Drag reduction of airplanes. , Induceddrag,Chordwise and span wise pressure distribution. Aspect ratio, Camber andplan form characteristics, drag polar.

2. STEADY FLIGHT: 8

Steady level flight, Thrust/power, available and required with altitude Estimationof maximum level flight speed, conditions for minimum drag and minimum powerrequired.

3. GLIDING, CLIMBINGAND TURINGPERFORMANCE: 12

Maximum range, Minimum rate of skin a glide, Shallow angle of climb, Rate ofclimb, time to climb and ceilings, Glide hodograph. Bank angle and load factor,Limitations on turn, Pull up and push over, the v-n diagram.

4. SPECIAL PERFORMANCE: 6

Range and endurance of jet and propeller type of airplanes,estimatioin of take-off

and landing distance. High lift devices, Use of thrust augmentation and reversethrust.

5. PROPELLERS: 7

Froude momentum and blade element theories, Propeller coefficients, Use ofpropeller charts, performance of fixed and variable pitch propeller.

L: 45 TOTAL: 45

TEXT BOOK:John D. Anderson,Jr Aircraft performance and design

REFERENCE:1. L.J.Clancy, Aerodynamics, Pitman, 1986.2. Houghton,E.L., and Carruthers, N.B., Aerodynamics for engineering

students, Edward Amold Publishers,1988.3. Kuethe, A.M., and Chow, C.Y., Foundations of Aerodynamics, John Wiley

& Sons, 1982.4. J.J. Bertin,Aerodynamics for engineers, Prentice-hall, 1988.5. Schlichting, E., Aerodynamics of the Airplane, McGraw-Hill, 1979.


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AIRCRAFT STRUCTURES IIL T P M C3 1 0 100 4

OBJECTIVE

To study the behavior of various aircraft structural components under different

types of loads.

1. UNSYMMETRICAL BENDING 8+3

Bending stresses in beams of unsymmetrical sections Bending of symmetricsections with skew loads.

2. SHEAR FLOW IN OPEN SECTIONS 10+3

Thin walled beams, Concept of shear flow, shear centre, Elastic axis. With oneaxis of symmetry, with wall effective and ineffective in bending, unsymmetricalbeam sections.

3. SHEAR FLOW IN CLOSED SECTIONS 10+3

Bredt Batho formula, Single and multi cell structures. Approximate methods.Shear flow in single & multicell structures under torsion. Shear flow in single andmulticell under bending with walls effective and ineffective.

4. BUCKLING OF PLATES 10+3

Introduction to theory of plates & shells. Rectangular sheets under compression,Local buckling stress of thin walled sections, Crippling stresses by Needhamsand Gerards methods, Thin walled column strength. Sheet stiffener panels.

Effective width, inter rivet and sheet wrinkling failures.

5. STRESS ANALYSIS IN WING AND FUSELAGE 7+3

Procedure Shear and bending moment distribution for semi cantilever andother types of wings and fuselage, thin webbed beam. With parallel and nonparallel flanges, Shear resistant web beams, Tension field web beams(Wagners).

TOTAL: 60TEXT BOOK

1. Peery, D.J., and Azar, J.J., Aircraft Structures, 2

nd

edition, McGrawHill,N.Y., 1993.

REFEENCES

1. Megson, T.M.G., Aircraft Structures for Engineering Students,Edward Arnold, 1995.

2. Bruhn. E.H. Analysis and Design of Flight vehicles Structures, Tri state off set company, USA, 1985.

3. Rivello, R.M., Theory and Analysis of Flight Structures, McGraw-Hill,1993.


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AERODYNAMICS IIL T P M C3 0 0 100 3

OBJECTIVE

To understand the behaviour of airflow both internal and external in compressibleflow regime with particular emphasis on supersonic flows.

1. ONE DIMENSIONAL COMPRESSIBLE FLOW 7

Energy, Momentum, continuity and state equations, velocity of sound, Adiabaticsteady state flow equations, Flow through converging, diverging passages,Performance under various back pressures.

2. NORMAL, OBLIQUE SHOCKS AND EXPANSION WAVES 15

Prandtl equation and Rankine Hugonoit relation, Normal shock equations, Pitotstatic tube, corrections for subsonic and supersonic flows, Oblique shocks andcorresponding equations, Hodograph and pressure turning angle, shock polars,

flow past wedges and concave corners, strong, weak and detached shocks,Rayleigh and Fanno Flow. Flow past convex corners, Expansion hodograph,Reflection and interaction of shocks and expansion, waves, Families of shocks,Methods of Characteristics, Two dimensional supersonic nozzle contours.

3. DIFFERENTIAL EQUATIONS OF MOTION FOR STEADYCOMPRESSIBLE FLOWS 9

Small perturbation potential theory, solutions for supersonic flows, Mach wavesand Mach angles, Prandtl-Glauert affine transformation relations for subsonicflows, Linearised two dimensional supersonic flow theory, Lift, drag pitchingmoment and center of pressure of supersonic profiles.

4. AIRFOIL IN HIGH SPEED FLOWS 6

Lower and upper critical Mach numbers, Lift and drag divergence, shock inducedseparation, Characteristics of swept wings, Effects of thickness, camber andaspect ratio of wings, Transonic area rule, Tip effects.

5. HIGH SPEED WIND TUNNELS 8

Blow down, indraft and induction tunnel layouts and their design features,Transonic, supersonic and hypersonic tunnels and their peculiarities, Helium andgun tunnels, Shock tubes, Optical methods of flow visualization.

TOTAL : 45


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TEXT BOOK

1. Rathakrishnan, E., Gas Dynamics, Prentice Hall of India, 2003.

REFERENCES

1. Shapiro, A.H., Dynamics and Thermodynamics of Compressible FluidFlow, Ronold Press, 1982.

2. Zucrow, M.J. and Anderson, J.D., Elements of gas dynamics, McGraw-Hill Book Co., New York, 1989.

3. Mc Cornick. W., Aerodynamics, Aeronautics and Flight Mechanics, JohnWiley, New York, 1979.

4. Anderson Jr., D., Modern compressible flows, McGraw-Hill Book Co.,New York 1999.


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CONTROL ENGINEERINGL T P M C3 0 0 100 3

OBJECTIVE

To understand the basic concepts of flight control system.

1. INTRODUCTION 6Historical review - Simple pneumatic, hydraulic and thermal systems, Series andparallel systems, Analogies - Mechanical and electrical components,Development of flight control systems.

2. OPEN AND CLOSED LOOP SYSTEMS 6

Feedback control systems Block diagram representation of control systems,Reduction of block diagrams, Output to input ratios, Signal flow graph.

3. CHARACTERISTIC EQUATION AND FUNCTIONS 10

Lap lace transformation, Response of systems to different inputs viz., Step input,impulse, ramp, parabolic and sinusoidal inputs, Time response of first andsecond order systems, steady state errors and error constants of unity feedbackcircuit.

4. CONCEPT OF STABILITY 15Necessary and sufficient conditions, Routh Hurwitz criteria of stability, Rootlocus and Bode techniques, Concept and construction, frequency response.

5. SAMPLED DATA SYSTEMS 8

Introduction to digital control system, Digital Controllers and Digital PIDControllers.


1. OGATO, Modern Control Engineering, Prentice Hall of India Pvt. Ltd.New Delhi, 1998.

2. GOPAL.M. Control Systems, Principles and design Tata McGraw-HillPublication, New Delhi, 2000.

REFERENCES

1. Azzo, J.J.D. and C.H. Houpis, Feed back control system analysis andsynthesis, McGraw Hill International, 3rd Edition, 1998.

2. Kuo, B.C., Automatic control systems, Prentice Hall of India Pvt. Ltd.,New Delhi, 1998.

3. Houpis, C.H. and Lamont, G.B., Digital Control Systems, McGraw-HillBook Co. New York, USA 1995.

4. Naresh K. Sinha, Control Systems, New Age International Publishers,New Delhi


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AIRCRAFT ELECTRONICS &

MICROPROCESSOR APPLICATIONSL T P M C

3 0 0 100 3

Objective:To give the in-depth knowledge in Aircraft Electronics and Principles,

Applications of Microprocessors to the students.

1. AIRCRAFT BATTERIES, DIGITAL AIRCRAFT SYSTEMS 7

Aircraft Storage Batteries: Dry Cells and Batteries; Lead Acid Storage Batteries &their maintenance procedures, Installation of Aircraft Batteries. Digital AircraftSystems, Trouble Shooting Digital Circuits.

2. AIRCRAFT LIGHTS, COMMUNICATION, NAVIGATION & WARNINGSYSTEMS 10

Aircraft Lights, Radio Theory: Radio waves, Amplifiers, Functions of aTransmitter & Receivers.Communication & Navigation Systems: VHF Communication Systems, AutomaticDirection Finder Systems.Weather Warning Systems: Radar, Digital Airborne Weather Radar Systems.

3. MICROPROCESSORS 12

Block Diagram of Microprocessors Architecture of Intel 8085, InstructionClassification, Data format and storage, Bus Structure of 8085,Addressingmodes, Overview of the 8085 Instruction Set, Development of Simple AssemblyLanguage Program. Internal architecture and functioning of Intel 8086.

4. MICROPROCESSOR MEMORY, INTERFACING PHERIPERALS 9

RAM, ROM, EPROM, Memory Interfacing, Interfacing Input Devices, MemoryMapped I/O, Basic Concepts in Serial I/O, Interfacing a matrix keyboard,8255,8259,DMA Data transfer & 8237.

5. APPLICATIONS 7

Electronic Flight Systems, Automatic Flight Control Systems, Automatic Flight &Landing Systems, Flight Management System, Ring Laser Gyro.

TOTAL: 45


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TEXT BOOKS

1. Aircraft Electricity & Electronics Thomas K.Eismin Fifth Edition,1994,McGrawhill International Editions. (Unit 1,Unit 2 & Unit 5)

2. Goankar R.S., Microprocessors Architecture. Programming andApplications(Unit 3 & Unit 4)

REFERENCES

1. Introduction to Microprocessors-Aditya P Mathur, Third Edition,Tata McGraw Hill.

2. Aircraft Instruments & Integrated Systems EHJ Pallet, Indian Reprint1996-Longman Scientific & Technical.

3. Aircraft Electrical Systems by EHJ Pallet, Longman Scientific &Technical


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AIRCRAFT STRUCTURES LAB IIL T P M C0 0 3 50 1.5

OBJECTIVE

To experimentally study the unsymmetrical bending of beams, find the location ofshear centre, obtain the stresses in circular discs and beams using photo elastictechniques, calibration of photo elastic materials and study on vibration ofbeams.

LIST OF EXPERIMENTS

1. Determination of Unsymmetrical bending of different materials using bendtest set up.

2. Determination of Shear centre location for open sections3. Determination of Shear centre location for closed sections4. Experiment on Constant strength beam

5. Finding out flexibility matrix for cantilever beam6. Testing of Beam with combined loading7. Calibration of Photo- elastic materials8. Determination of Stresses in circular discs and beams using photoelastic

techniques9. Measurement of Vibrations of beams10. Wagner beam Tension field beam experiments.

TOTAL : 60LIST OF EQUIPMENT

(for a batch of 30 students)

Sl.No. Name of the Equipment QtyExperimentsNumber

1 Beam Test set up 2 1, 2, 3,4

2Unsymmetrical sections like Zsections

2 1, 2, 3

3 Channel section and angle section 2 1, 2, 34 Dial gauges 12 1, 2, 35 Weights 1Kg 10 1, 2, 36 Weights 2 Kg 10 1, 2, 37 Beam Test Set up 2 3, 4

8 Strain indicator and strain gauges One set 4,5,69 Photo elastic apparatus 1 7,810 Amplifier 2 911 Exciter 2 912 Pick up 2 913 Oscilloscope 2 914 Wagner beam 1 1015. Hydraulic Jack 1 10


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AIRCRAFT STRUCTURES REPAIR LABL T P M C0 0 3 50 1.5

OBJECTIVE

To give training on riveting, patchwork, welding and carpentry

LIST OF EXPERIMENTS

1. Patch repair welding using TIG.2. Patch repair welding using MIG.3. Patch repair welding using Plasma Arc.4. Exercise on pipe bending5. Exercise on Riveted joints & repair work.6. Exercise on composites & repair work.7. Repair of Sandwich panels.8. Exercise on Sheet metal forming.9. Exercise on cable swaging

TOTAL : 60

LIST OF EQUIPMENT(for a batch of 30 students)

Sl.No. Name of the Equipment QuantityExperiment

No.1 Shear cutter pedestal type 1 6,8

2 Drilling Machine 1 5,6,83 Bench Vices 1 5,6,84 Radius Bend bars 1 4

5Pipe Flaring Tools / PipeBending Tools

1 9

6 Carbide Gas Plant 1 47 MIG Weld Plant 1 28 TIG Weld Plant 1 19. Plasma welding setup 1 310 Cable And Swaging Block 1 911 Sandwich / Composite Panels 5 6,7


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AERO ENGINE REPAIR AND MAINTENANCE

LABORATORYL T P M C

0 0 3 50 1.5

OBJECTIVE

To introduce the knowledge of the maintenance and repair of both piston and jetaero engines and the procedures followed for overhaul of aero engines.

1. Disintegration of a aircraft piston engine2. Engine (Piston Engine) - cleaning, visual inspection, NDT checks.3. Study of Piston Engine Components - dimensional checks.4. Engine Piston reassembly.5. Disintegration and study of fuel system of a jet engine6. Identification of components & trouble shooting of Jet Engine.7. NDT checks and dimensional checks of Jet Engine8. Engine starting procedures.

9. Ground running of aircraft.

TOTAL : 60

LIST OF EQUIPMENTS(for a batch of 30 students)

Sl.NoEquipments Qty Experiments No.

1. Piston Engines 2 1,2,3,42. Jet Aero Engines 2 5,6,7,83. Aircraft with serviceable stand 1 1 to 9

4.Precision instruments (Vernier Caliper,Micro meter, Cylinder bore gauge, depthgauge, Bevel Protector and DTI

2 each 3,1,7

5.NDT Equipments (Defectoscope, Dyepenetrant method, Hot oil Chalk Method

1 each 2,7


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COMMUNICATION SKILLS AND TECHNICALSEMINAR

L T P M C0 0 3 50 1.5

OBJECTIVE

During the seminar session each student is expected to prepare and present atopic on engineering/ technology, for a duration of about 8 to 10 minutes. In asession of three periods per week, 15 students are expected to present theseminar. A faculty guide is to be allotted and he / she will guide and monitor theprogress of the student and maintain attendance also.

Students are encouraged to use various teaching aids such as over headprojectors, power point presentation and demonstrative models. This will enablethem to gain confidence in facing the placement interviews.


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SEMESTER VI

CODE

No.Course Title L T P M

C

THEORY

Aircraft General Engineering and

Maintenance Practices*3 0 0 100

3

Propulsion-II 3 0 0 100 3

Heat Transfer 3 0 0 100 3

Experimental Stress Analysis 3 0 0 100 3

Aircraft Stability And Control 3 0 0 100 3

Elective I 3 0 0 100 3

PRACTICAL

Aircraft Design Lab - I 0 0 3 50 1.5

CAD Lab 0 0 3 100 1.5

Propulsion Lab 0 0 3 100 1.5

Presentation Skills and Technical

Seminar0 0 3 0 1.5

*Revised SyllabusELECTIVES I FOR VI SEMESTER

Course Title L T P M C

Theory of Elasticity 3 0 0 100 3

Space Mechanics 3 0 0 100 3

Principles of Management 3 0 0 100 3

Wind Tunnel Techniques 3 0 0 100 3

Intellectual Property Rights

(IPR)3 0 0 100

3

Indian Constitution and

Society3 0 0 100

3


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Aircraft General Engineering and Maintenance Practices* 3 0 0 100

1. Aircraft Maintenance Practices 8 0 0

General knowledge of procedure of jacking, leveling and mooring of aircraft.Knowledge of maintenance and handling of ground equipment such as enginestarting trolley, hydraulic trolley, air condition trolley used in the maintenance of

aircraft. Knowledge of safety and fire precautions to be observed duringmaintenance, refueling and defueling of aircraft. Knowledge of aircraft fireextinguishers Maintenance safety

2. Workshop Practices 8 0 0

Uses of Hand tools in aircraft maintenance, precision measuring instruments.Knowledge and terminology, of aircraft bolts, nuts, rivets, screws, and lockingdevices. Knowledge of various types of gears and bearings, their use andcommon defects. Knowledge of various types of threads, drills, taps, reamers.

3. Aircraft Materials 9 0 0

Principal of Heat treatment of aircraft steel. Heat treatment of non ferrous metalsolution hardening, precipitation hardening, forms of corrosion and factoraffecting corrosion. Process and material used in corrosion control electroplating. Parco lubrizing, alodizing, anodizing.

4. Inspection 6 0 0

Purpose type inspection interval & inspection schedule. Special inspection.FAR Air worthiness directive Type certificate data sheet, service bulletin

5. Aircraft engine, electrical and instrument 14 0 0

Theory & construction of aircraft engines reciprocating and turbojet engine.Knowledge of lead and cadmium Batteries and their maintenance. Knowledge ofprinciple of operation of aircraft fuel flow meter, oil temperature indicator oilpressure indicator.

Total Hours 45


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TEXT BOOKS :1. Air frame & power plant Mechanics (General Hand book EA-AC 65-9A)

2. U S Department of transportation

Air frame & power plant Mechanics (Power plant Hand book EA-AC 65

12A) US Department of transportation

REFERENCES :1. James Anderson, Earl E. Tatro, Shop Theory

2. Larry Reithmaier, Standard Aircraft handbook

3. E H J Pallet, Aircraft Electrical Systems

4. Aircraft materials and processes b Titterton

5. Aviation Maintenance and Technical series

a) General - Dale Crane

b) Power plant - Dale Crane

Published by Aviation supplies and Academic, DC

*Revised Syllabus.


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PROPULSION IIL T P M C3 0 0 100 3

OBJECTIVETo study in detail about gas turbines, ramjet, fundamentals of rocket propulsionand chemical rockets

1. AIRCRAFT GAS TURBINES 12Impulse and reaction blading of gas turbines Velocity triangles and poweroutput Elementary theory Vortex theory Choice of blade profile, pitch andchord Estimation of stage performance Limiting factors in gas turbine design-Overall turbine performance Methods of blade cooling Matching of turbineand compressor Numerical problems.2. RAMJET PROPULSION: 10Operating principle Sub critical, critical and supercritical operation Combustion in ramjet engine Ramjet performance Sample ramjet designcalculations Introduction to scramjet Preliminary concepts in supersonic

combustion Integral ram- rocket- Numerical problems.

3. FUNDAMENTALS OF ROCKET PROPULSION 8Operating principle Specific impulse of a rocket internal ballistics- Rocketnozzle classification Rocket performance considerations NumericalProblems.4. CHEMICAL ROCKETS 10Solid propellant rockets Selection criteria of solid propellants Importanthardware components of solid rockets Propellant grain design considerations Liquid propellant rockets Selection of liquid propellants Thrust control in liquidrockets Cooling in liquid rockets Limitations of hybrid rockets Relative

advantages of liquid rockets over solid rockets- Numerical Problems.

5. ADVANTAGES OF PROPULSION TECHNIQUES 5Electric rocket propulsion Ion propulsion techniques Nuclear rocket Types Solar sail- Preliminary Concepts in nozzleless propulsion.

TOTAL : 45TEXT BOOKS1. 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.

REFERENCES1. 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.


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HEAT TRANSFERL T P M C

3 0 0 100 3

OBJECTIVE

To introduce the concepts of heat transfer to enable the students to design

components subjected to thermal loading.1. HEAT CONDUCTION 11

Basic Modes of Heat Transfer One dimensional steady state heat conduction:Composite Medium Critical thickness Effect of variation of thermalConductivity Extended Surfaces Unsteady state.Heat Conduction: Lumped System Analysis Heat Transfer in Semi infinite andinfinite solids Use of Transient Temperature charts Application of numericaltechniques.2. CONVECTIVE HEAT TRANSFER 10

Introduction Free convection in atmosphere free convection on a vertical flat

plate Empirical relation in free convection Forced convection Laminar andturbulent convective heat transfer analysis in flows between parallel plates, overa flat plate and in a circular pipe. Empirical relations, application of numericaltechniques in problem solving.

3. RADIATIVE HEAT TRANSFER 8

Introduction to Physical mechanism Radiation properties Radiation shapefactors Heat exchange between non black bodies Radiation shields.4. HEAT EXCHANGERS 8

Classification Temperature Distribution Overall heat transfer coefficient, Heat

Exchange Analysis LMTD Method and E-NTU Method.

5. HEAT TRANSFER PROBLEMS IN AEROSPACE ENGINEERING 8

High-Speed flow Heat Transfer, Heat Transfer problems in gas turbinecombustion chambers Rocket thrust chambers Aerodynamic heating Ablative heat transfer.


1. Yunus A. Cengel., Heat Transfer A practical approach, Second Edition,Tata McGraw-Hill, 2002.

2. Incropera. F.P.and Dewitt.D.P. Introduction to Heat Transfer, John Wileyand Sons 2002.REFERENCES

1. Lienhard, J.H., A Heat Transfer Text Book, Prentice Hall Inc., 1981.2. Holman, J.P. Heat Transfer, McGraw-Hill Book Co., Inc., New York, 6th

Edn., 1991.3. Sachdeva, S.C., Fundamentals of Engineering Heat & Mass Transfer,

Wiley Eastern Ltd., New Delhi, 1981.4. Mathur, M. and Sharma, R.P. Gas Turbine and Jet and Rocket

Propulsion, Standard Publishers, New Delhi 1988.


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EXPERIMENTAL STRESS ANALYSISL T P M C

3 0 0 100 3

OBJECTIVE

To bring awareness on experimental method of finding the response of the

structure to different types of load.

1. MEASUREMENTS 4

Principles of measurements, Accuracy, Sensitivity and range of measurements.

2. EXTENSOMETERS 6

Mechanical, Optical Acoustical and Electrical extensometers and their uses,Advantages and disadvantages.

3. ELECTRICAL RESISTANCE STRAIN GAUGES 10

Principle of operation and requirements, Types and their uses, Materials forstrain gauge. Calibration and temperature compensation, cross sensitivity,Rosette analysis, Wheastone bridge and potentiometer circuits for static anddynamic strain measurements, strain indicators.

4. PHOTOELASTICITY 10

Two dimensional photo elasticity, Concept of light photoelastic effects, stressoptic law, Interpretation of fringe pattern, Compensation and separationtechniques, Photo elastic materials. Introduction to three dimensional photoelasticity.

5. NON DESTRUCTIVE TESTING 15Fundamentals of NDT, Radiography, ultrasonic, magnetic particle inspection,Fluorescent penetrant technique, Eddy current testing, Acoustic EmissionTechnique, Fundamentals of brittle coating methods, Introduction to Moirtechniques, Holography, ultrasonic C- Scan, Thermograph, Fiber opticSensors.


1. Srinath, L.S., Raghava, M.R., Lingaiah, K., Garagesha, G., Pant B., andRamachandra, K., Experimental Stress Analysis, Tata McGraw-Hill, New

Delhi, 1984.

REFERENCES

1. Dally, J.W., and Riley, W.F., Experimental Stress Analysis, McGraw-HillInc., New York, 1998.

2. Hetyenyi, M., Hand book of Experimental Stress Analysis, John Wileyand Sons Inc., New York, 1972.

3. Pollock A.A., Acoustic Emission in Acoustics and Vibration Progress, Ed.Stephens R.W.B., Chapman and Hall, 1993.


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AIRCRAFT STABILITY AND CONTROLL T P M C

3 0 0 100 3

1. GENERAL 4

Degrees of freedom of a system, Static and dynamic stability, Need for stability in

an airplane, purpose of controls, Inherently and marginally stable airplanes.

2. STATIC LONGITUDINAL STABILITY: 14

Stick fixed: Basic equations of equilibrium, Stability criterion, Wing and tailmoments, Effect of fuselage and nacelles, Effect of c.g. location, Power effects,Stabiliser setting and c.g. location, Elevator effects, stick fixed neutral point.Stick free: Hinge moment coefficients, Stick free neutral point symmetricmaneuvers, stick force gradients and stick force per cg. Aerodynamic balancingof control surfaces.

3. STATIC LATERAL STABILITY: 6Dihedral effect, coupling between rolling moment and yawing moment, Adverseyaw, Aileron power, Aileron reversal.

4. SATATIC DIRECTIONAL STABILITY: 6

Weather cocking effect, rudder requirements. One engine inoperative conditions,rudder lock.

5. DYNAMIC LONGITUDINAL STABILITY: 8

Equation of motion, Stability derivatives, Rouths discriminant, solving the stabilityquadratic, Phugoid motion, factors affecting the period and damping.

6. DYNAMIC LATERAL AND DIRECTION STABILITY: 7

Dutch roll and spiral instability Auto rotation and spin, Two control airplane

TOTAL: 45

TEXT BOOK:

Perkins C.D., & Hage.

REFERENCES:1. R.E.Airplane performance, stability and control, Wiley Toppan 1974.2. Babister, A.W. Aircraft stability and response, Pergamon Press, 1980.3. McCormick, B.W., Aerodynamics, Aeronautics & Flight Mechanics John Wiley,

19954. Nelson, R.C. Flight stability & Automatics Control, McGraw Hill, 1989.


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AIRCRAFT DESIGN LAB IL T P M C

3 0 0 100 3

OBJECTIVE

To introduce and develop the basic concept of aircraft design.

Each student is assigned with the design of an Airplane (or Helicopter or anyother flight vehicle), for given preliminary specifications. The following are theassignments to be carried out:

EXPERIMENTS

1. Comparative configuration study of different types of airplanes2. Comparative study on specification and performance details of aircraft3. Preparation of comparative data sheets4. Work sheet layout procedures5. Comparative graphs preparation and selection of main parameters for the

design6. Preliminary weight estimations, selection of main parameters,7. Power plant selection, Aerofoil selection, Wing tail and control surfaces8. Preparation of layouts of balance diagram and three view drawings9. Estimation of various Drag.10. Detailed performance calculations and stability estimates

TOTAL : 60 PERIODS

LIST OF EQUIPMENTS(for a batch of 30 students)

Sl.No. Name of the Equipment QuantityExperiments

Number

1 Engineering Drawing Board 30 32 Engineering Drawing Instruments 30 3


24/34

CAD LABORATORYL T P M C

0 0 3 100 1.5

OBJECTIVE

To teach and train the students in the lab about the design and drafting of aero

components

LIST OF EXPERIMENTS

1. Scaling, rotation, translation, editing, dimensioning Typical CADcommand structure.

2. Wire frame modeling surface modeling3. Solid Modeling4. Advanced modeling5. Flow Simulation Over A Symmetrical Airfoil Using CFD6. Flow Simulation Over A Cambered Airfoil Using CFD7. Flow Simulation Over A Turbine Blade Using CFD

8. Flow Simulation Over A compressor Blade Using CFD9. Stress Analysis Of A Turbine Blade10. Stress Analysis Of Any Aircraft Component

TOTAL : 60

LIST OF EQUIPMENT(for a batch of 30 students)

Sl.No. Name of the Equipment QuantityExperiment

No.1 Computer nodes 30 1 to 10

2 Pro-E -Wildfire,AutoCAD(latest),CATIA,SOLIDWORKS

30 licenses 1 to 10

3ANSYS- 11 with Fluent,NASTRAN ,CFX

30 licenses 1 to 10

4 UPS 10 KVa 3 Phase 1 1 to 10


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PROPULSION LABORATORYL T P M C

0 0 3 100 1.5

Objective

To understand the basic concepts and carry out experiments in AerospacePropulsion

List of Experiments

1. Study of an aircraft piston engine (includes study of assembly sub

systems, various components, their functions and operating principles)

2. Study of an aircraft jet engine (includes study of assembly of sub

systems, various components, their functions and operating principles3. Performance of 2d diffuser a) Stable Flow b) Separated flow

4. Cascade testing of a model axial turbine blade row

5. Cascade testing of a model axial compressor blade row

6. Study of performance of a propeller

7. Determination of heat of combustion of aviation fuel

8. Combustion performance studies in a duct (duct burner)

9. Study of free jet

10. Study of wall jet


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List of Equipment(for a batch of 30 students)

S. No Equipment Quantity ExperimentNo

1 Piston Engine 2 12 Jet Engine 2 2

3 2D Diffuser1 (separatedflow) &

1(stable flow)3

4Axial Turbine Blade RowModel (with pressuretapping)

2 4

5Axial compressor BladeRow Model (withpressure tapping)

2 5

6Water tube manometerswith 20 channels

4 9, 10

7 Cascade Wind Tunnel 1 3, 4 & 58 Propeller Model 1 6

9 2D Traverse Mechanism 43, 4, 5, 9 &10

10 Free Jet Test Setup 2 9

11Aluminum Plates withwall static pressureturbine

1 10

12 Bomb Calorimeter 1 713 Duct Burner 1 814 Compressor (5 bar) 1 8


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PRESENTATION SKILLS AND TECHNICAL

SEMINARL T P M C

0 0 3 100 1.5

OBJECTIVE

During the seminar session each student is expected to prepare and present atopic on engineering/ technology, for a duration of about 8 to 10 minutes. In asession of three periods per week, 15 students are expected to present theseminar. A faculty guide is to be allotted and he / she will guide and monitor theprogress of the student and maintain attendance also.

Students are encouraged to use various teaching aids such as over headprojectors, power point presentation and demonstrative models. This will enablethem to gain confidence in facing the placement interviews.


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ELECTIVES I FOR VI SEMESTER

THEORY OF ELASTICITYL T P M C

3 0 0 100 3

OBJECTIVE

To understand the theoretical concepts of material behaviour with particularemphasis on their elastic property

1. ASSUMPTIONS IN ELASTICITY 4

Definitions- notations and sign conventions for stress and strain, Equations ofequilibrium.

2. BASIC EQUATIONS OF ELASTICITY 15

Strain displacement relations, Stress strain relations, Lames constant

cubical dilation, Compressibility of material, bulk modulus, Shear modulus,Compatibility equations for stresses and strains, Principal stresses and principalstrains, Mohrs circle, Saint Venants principle.

3. PLANE STRESS AND PLANE STRAIN PROBLEMS 8

Airys stress function, Bi-harmonic equations, Polynomial solutions, Simple two-dimensional problems in Cartesian coordinates like bending of cantilever andsimply supported beams, etc.

4. POLAR COORDINATES 10

Equations of equilibrium, Strain displacement relations, Stress strain relations,Axi symmetric problems, Kirsch, Michells and Boussinesque problems.

5. TORSION 8

Naviers theory, St. Venants theory, Prandtls theory on torsion, The semi-

inverse method and applications to shafts of circular, elliptical, equilateral

triangular and rectangular sections.

TOTAL : 45TEXT BOOK

1. Timoshenko, S., and Goodier, T.N., Theory of Elasticity, McGrawHill

Ltd., Tokyo, 1990.

REFERENCES

1. Enrico Volterra & J.H. Caines, Advanced Strength of Materials, PrenticeHall New Jersey, 1991.

2. Wng, C.T., Applied Elasticity, McGrawHill Co., New York, 1993.3. Sokolnikoff, I.S., Mathematical Theory of Elasticity, McGrawHill New

York, 1978.


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SPACE MECHANICS

L T P M C

3 0 0 100 3

OBJECTIVE

To study the basic concepts of orbital Mechanics with particular emphasis oninterplanetary trajectories

1. BASIC CONCEPTS 4

The Solar System References Frames and Coordinate Systems TheCelestial Sphere The Ecliptic Motion of Vernal Equinox Sidereal Time Solar Time Standard Time The Earths Atmosphere.

2. THE GENERAL N-BODY PROBLEM 10

The many body Problem Lagrange Jacobian Identity The Circular RestrictedThree Body Problem Libration Points- Relative Motion in the N-body Problem Two Body Problem Satellite Orbits Relations Between Position and Time

Orbital Elements.

3. SATELLITE INJECTION AND SATELLITE ORBIT PERTURBATIONS 12

General Aspects of satellite Injections Satellite Orbit Transfer Various Cases Orbit Deviations Due to Injection Errors Special and General Perturbations Cowells Method Enckes Method Method of vibrations of Orbital Elements General Perturbations Approach.

4. INTERPLANETARY TRAJECTORIES 6

Two Dimensional Interplanetary Trajectories Fast Interplanetary Trajectories

Three Dimensional Interplanetary Trajectories Launch if InterplanetarySpacecraft Trajectory about the Target Planet.

5. BALLISTIC MISSILE TRAJECTORIES AND MATERIALS 13

The Boost Phase The Ballistic Phase Trajectory Geometry- Optimal Flights Time of Flight Re entry Phase The Position of the Impact Point InfluenceCoefficients. Space Environment Peculiarities Effect of Space Environmenton the Selection of Spacecraft Material.

TOTAL : 45TEXT BOOK

1. Cornelisse, J.W., Rocket Propulsion and Space Dynamic, W.H. Freeman& Co., 1984.

REFERENCES

1. Sutton, G.P., Rocket Propulsion Elements, John Wiley, 1993.2. Van de Kamp, P., Elements of Astromechanics, Pitman, 1979.3. Parker E.R., Materials for Missiles and Spacecraft, McGraw-Hill Book

Co. Inc., 1982.


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PRINCIPLES OF MANAGEMENTL T P M C

3 0 0 100 3

OBJECTIVE

Knowledge on the principles of management is essential for all kinds of people in

all kinds of organizations. After studying this course, students will be able to havea clear understanding of the managerial functions like planning, organizing,staffing, leading and controlling. Students will also gain some basic knowledgeon international aspect of management.

1. HISTORICAL DEVELOPMENT 9

Definition of Management Science or Art Management and Administration Development of Management Thought Contribution of Taylor and Fayol Functions of Management Types of Business Organisation.

2. PLANNING 9Nature & Purpose Steps involved in Planning Objectives Setting Objectives

Process of Managing by Objectives Strategies, Policies & PlanningPremises- Forecasting Decision-making.

3. ORGANISING 9

Nature and Purpose Formal and informal organization Organization Chart Structure and Process Departmentation by difference strategies Line andStaff authority Benefits and Limitations De-Centralization and Delegation ofAuthority Staffing Selection Process - Techniques HRD Managerial

Effectiveness.

4. DIRECTING 9

Scope Human Factors Creativity and Innovation Harmonizing Objectives Leadership Types of Leadership Motivation Hierarchy of needs Motivationtheories Motivational Techniques Job Enrichment Communication Process of Communication Barriers and Breakdown Effective Communication

Electronic media in Communication.

5. CONTROLLING 9

System and process of Controlling Requirements for effective control TheBudget as Control Technique Information Technology in Controlling Use ofcomputers in handling the information Productivity Problems andManagement Control of Overall Performance Direct and Preventive Control Reporting The Global Environment Globalization and Liberalization International Management and Global theory of Management.

TOTAL : 45


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TEXT BOOKS

1. Harold Kooritz & Heinz Weihrich Essentials of Management, TataMcGraw-Hill, 1998

2. Joseph L Massie Essentials of Management, Prentice Hall of India,(Pearson) Fourth Edition, 2003.

REFERENCES

1 Tripathy PC And Reddy PN, Principles of Management, Tata McGraw-Hill, 1999.

2. Decenzo David, Robbin Stephen A, Personnel and Human ReasonsManagement, Prentice Hall of India, 1996

3. JAF Stomer, Freeman R. E and Daniel R Gilbert, Management, PearsonEducation, Sixth Edition, 2004.

4. Fraidoon Mazda, Engineering Management, Addison Wesley, 2000.


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WIND TUNNEL TECHNIQUESL T P M C

3 0 0 100 3

OBJECTIVE

To introduce the basic concepts of measurement of forces and moments on

models during the wind tunnel testing.

1. PRINCIPLES OF MODEL TESTING 6

Buckingham Theorem Non-Dimensional Numbers Scale Effect Types ofSimilartes.

2. WIND TUNNELS 8

Classification Special problems of Testing in Subsonic, Transonic, supersonicand hypersonic speed regions Layouts sizing and design parameters.

3. CALIBRATION OF WIND TUNNELS 11

Test section speed Horizontal buoyancy Flow angularities Turbulencemeasurements Associated instrumentation Calibration of supersonic tunnels.

4. WIND TUNNEL MEASUREMENTS 12

Pressure and velocity measurements Force measurements Three componentand six component balances Internal balances.

5. FLOW VISUALIZATION 8

Smoke and Tuft grid techniques Dye injection special techniques Opticalmethods of flow visualization.

TOTAL : 45TEXT BOOK

1. Rae, W.H. and Pope, A. Low Speed Wind Tunnel Testing, John Wiley

Publication, 1984.

REFERENCE

1. Pope, A., and Goin, L., High Speed wind Tunnel Testing, John Wiley,1985.


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INTELLECTUAL PROPERTY RIGHTS (IPR)

L T P M C

3 0 0 100 3

UNIT I 5Introduction Invention and Creativity Intellectual Property (IP) Importance

Protection of IPR Basic types of property (i. Movable Property ii. ImmovableProperty and iii. Intellectual Property).

UNIT II 10

IP Patents Copyrights and related rights Trade Marks and rights arisingfrom Trademark registration Definitions Industrial Designs and Integratedcircuits Protection of Geographical Indications at national and Internationallevels Application Procedures.

UNIT III 10

International convention relating to Intellectual Property Establishment of WIPO Mission and Activities History General Agreement on Trade and Tariff(GATT).

UNIT IV 10

Indian Position Vs WTO and Strategies Indian IPR legislations commitmentsto WTO-Patent Ordinance and the Bill Draft of a national Intellectual PropertyPolicy Present against unfair competition.

UNIT V 10

Case Studies on Patents (Basumati rice, turmeric, Neem, etc.) Copyright andrelated rights Trade Marks Industrial design and Integrated circuits Geographic indications Protection against unfair competition.

TEXT BOOK

1. Subbaram N.R. Handbook of Indian Patent Law and Practice , S.Viswanathan (Printers and Publishers) Pvt. Ltd., 1998.

REFERENCES

1. Eli Whitney, United States Patent Number : 72X, Cotton Gin, March 14,1794.

2. Intellectual Property Today : Volume 8, No. 5, May 2001,[www.iptoday.com].

3. Using the Internet for non-patent prior art searches, Derwent IP Matters,July 2000. [www.ipmatters.net/features/000707_gibbs.html.


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INDIAN CONSTITUTION AND SOCIETY

L T P M C

3 0 0 100 3

UNIT I 9Historical Background Constituent Assembly of India Philosophicalfoundations of the Indian Constitution Preamble Fundamental Rights

Directive Principles of State Policy Fundamental Duties Citizenship Constitutional Remedies for citizens.

UNIT II 9Union Government Structures of the Union Government and Functions President Vice President Prime Minister Cabinet Parliament SupremeCourt of India Judicial Review.

UNIT III 9State Government Structure and Functions Governor Chief Minister Cabinet State Legislature Judicial System in States High Courts and other

Subordinate Courts.

UNIT IV 9Indian Federal System Center State Relations Presidents Rule Constitutional Amendments Constitutional Functionaries - Assessment ofworking of the Parliamentary System in India.

UNIT V 9Society : Nature, Meaning and definition; Indian Social Structure; Castle,Religion, Language in India; Constitutional Remedies for citizens PoliticalParties and Pressure Groups; Right of Women, Children and Scheduled Castes

and Scheduled Tribes and other Weaker Sections.

TEXT BOOKS1. Durga Das Basu, Introduction to the Constitution of India ,

Prentice Hall of India, New Delhi.2. R.C.Agarwal, (1997) Indian Political System , S.Chand and

Company, New Delhi.3. Maciver and Page, Society: An Introduction Analysis , Mac Milan

India Ltd., New Delhi.4. K.L.Sharma, (1997) Social Stratification in India:

Issues and Themes , Jawaharlal Nehru University, New Delhi.

REFERENCES

1. Sharma, Brij Kishore, Introduction to the Constitution of India:,Prentice Hall of India, New Delhi.

2. U.R.Gahai, (1998) Indian Political System , New AcademicPublishing House, Jalaendhar.

3. R.N. Sharma, Indian Social Problems , Media Promoters andPublishers Pvt. Ltd.

aeronautical v visem new

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