Thrust is the force which moves any aircraft through the air. Thrust is generated by the propulsion system of the aircraft. Different propulsion systems develop thrust in different ways, but all thrust is generated through some application of Newton's third law of motion. For every action there is an equal and opposite reaction. In any propulsion system, a working fluid is accelerated by the system and the reaction to this acceleration produces a force on the system. A general derivation of the thrust equation shows that the amount of thrust generated depends on the mass flow through the engine and the exit velocity of the gas.
During and following World War II, there were a number of rocket- powered aircraft built to explore high speed flight. The X-1A, used to break the "sound barrier", and the X-15 were rocket-powered airplanes. In a rocket engine , fuel and a source of oxygen, called an oxidizer, are mixed and exploded in a combustion chamber. The combustion produces hot exhaust which is passed through a nozzle to accelerate the flow and produce thrust. For a rocket, the accelerated gas, or working fluid, is the hot exhaust produced during combustion. This is a different working fluid than you find in a turbine engine or a propeller powered aircraft. Turbine engines and propellers use air from the atmosphere as the working fluid, but rockets use the combustion exhaust gases. In outer space there is no atmosphere so turbines and propellers can not work there. This explains why a rocket works in space but a turbine engine or a propeller does not work.
There are two main categories of rocket engines; liquid rockets and solid rockets. In a liquid rocket, the propellants, the fuel and the oxidizer, are stored separately as liquids and are pumped into the combustion chamber of the nozzle where burning occurs. In a solid rocket, the propellants are mixed together and packed into a solid cylinder. Under normal temperature conditions, the propellants do not burn; but they will burn when exposed to a source of heat provided by an igniter. Once the burning starts, it proceeds until all the propellant is exhausted. With a liquid rocket, you can stop the thrust by turning off the flow of propellants; but with a solid rocket, you have to destroy the casing to stop the engine. Liquid rockets tend to be heavier and more complex because of the pumps and storage tanks. The propellants are loaded into the rocket just before launch. A solid rocket is much easier to handle and can sit for years before firing.
On this slide, we show a picture of an X-15 rocket-powered airplane at the upper left and a picture of a rocket engine test at the lower right. For the picture at the right, we only see the outside of the rocket nozzle, with the hot gas exiting out the bottom. The X-15 was powered by a liquid rocket engine and carried a single pilot to a height of more than 60 miles above the earth. The X-15 flew more than six times the speed of sound nearly 40 years ago. The speed record for a piloted aircraft is only exceeded today by the Space Shuttle. The altitude record is only topped by the Space Shuttle and the recent Space Ship 1, which also used rocket propulsion.
Thursday, September 3, 2009
aircraft propulsion
Thrust is the force which moves any aircraft through the air. Thrust is generated by the propulsion system of the aircraft. Different propulsion systems develop thrust in different ways, but all thrust is generated through some application of Newton's third law of motion. For every action there is an equal and opposite reaction. In any propulsion system, a working fluid is accelerated by the system and the reaction to this acceleration produces a force on the system. A general derivation of the thrust equation shows that the amount of thrust generated depends on the mass flow through the engine and the exit velocity of the gas.
During World War II, a new type of airplane engine was developed independently in Germany and in England. This engine was called a gas turbine engine. We sometimes call this engine a jet engine. Early gas turbine engines worked much like a rocket engine creating a hot exhaust gas which was passed through a nozzle to produce thrust. But unlike the rocket engine which must carry its oxygen for combustion, the turbine engine gets its oxygen from the surrounding air. A turbine engine does not work in outer space because there is no surrounding air. For a gas turbine engine, the accelerated gas, or working fluid, is the jet exhaust. Most of the mass of the jet exhaust comes from the surrounding atmosphere. Most modern, high speed passenger and military aircraft are powered by gas turbine engines. Because gas turbine engines are so important for modern life, we will be providing a lot of information about turbine engines and their operation.
Turbine engines come in a wide variety of shapes and sizes because of the many different aircraft missions. All gas turbine engines have some parts in common, however. On the slide we see pictures of four different aircraft equipped with gas turbine engines. Each aircraft has a unique mission and therefore a unique propulsion requirement. At the upper left is a DC-8 airliner. Its mission is to carry large loads of passengers or cargo for a long distance at high speed. It spends most of its life in high speed cruise. At the lower left is an F-14 fighter plane. Its mission is to shoot down other aircraft in air-to-air combat. It spends most of its life in cruise, but needs high acceleration when in combat. At the lower right is a C-130 cargo aircraft. Like the DC-8, it carries cargo a long distance, but it does not have the high speed requirement of the DC-8. At the upper right is a T-38 trainer. It is used to teach pilots how to fly jet aircraft and does not have the acceleration requirements of the F-14. The DC-8 is powered by four high-bypass turbofan engines, the F-14 by two afterburning low-bypass turbofans, the C-130 by four turboprop engines, and the T-38 by two turbojet engines.
EngineSim is an interactive Java applet which allows you to study different types of jet engines. You can learn the fundamentals of turbine engine propulsion with the EngineSim simulator. RangeGames is an interactive Java applet which allows you to study how different types of aircraft use different types of engines to meet their mission.
During World War II, a new type of airplane engine was developed independently in Germany and in England. This engine was called a gas turbine engine. We sometimes call this engine a jet engine. Early gas turbine engines worked much like a rocket engine creating a hot exhaust gas which was passed through a nozzle to produce thrust. But unlike the rocket engine which must carry its oxygen for combustion, the turbine engine gets its oxygen from the surrounding air. A turbine engine does not work in outer space because there is no surrounding air. For a gas turbine engine, the accelerated gas, or working fluid, is the jet exhaust. Most of the mass of the jet exhaust comes from the surrounding atmosphere. Most modern, high speed passenger and military aircraft are powered by gas turbine engines. Because gas turbine engines are so important for modern life, we will be providing a lot of information about turbine engines and their operation.
Turbine engines come in a wide variety of shapes and sizes because of the many different aircraft missions. All gas turbine engines have some parts in common, however. On the slide we see pictures of four different aircraft equipped with gas turbine engines. Each aircraft has a unique mission and therefore a unique propulsion requirement. At the upper left is a DC-8 airliner. Its mission is to carry large loads of passengers or cargo for a long distance at high speed. It spends most of its life in high speed cruise. At the lower left is an F-14 fighter plane. Its mission is to shoot down other aircraft in air-to-air combat. It spends most of its life in cruise, but needs high acceleration when in combat. At the lower right is a C-130 cargo aircraft. Like the DC-8, it carries cargo a long distance, but it does not have the high speed requirement of the DC-8. At the upper right is a T-38 trainer. It is used to teach pilots how to fly jet aircraft and does not have the acceleration requirements of the F-14. The DC-8 is powered by four high-bypass turbofan engines, the F-14 by two afterburning low-bypass turbofans, the C-130 by four turboprop engines, and the T-38 by two turbojet engines.
EngineSim is an interactive Java applet which allows you to study different types of jet engines. You can learn the fundamentals of turbine engine propulsion with the EngineSim simulator. RangeGames is an interactive Java applet which allows you to study how different types of aircraft use different types of engines to meet their mission.
4
V SEMESTER
MANAGEMENT & ENTREPRENEURSHIP
Subject Code : 06AL51 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART - A
MANAGEMENT
UNIT - 1
MANAGEMENT: Introduction - Meaning - nature and characteristics of
Management, Scope and functional areas of Management - Management as a
Science, Art or Profession Management & Administration - Roles of
Management, Levels of Management, Development of Management
Thought-Early Management Approaches-Modern Management Approaches.
7 Hours
UNIT - 2
PLANNING: Nature, importance and purpose of planning process -
Objectives - Types of plans (Meaning only) - Decision making - Importance
of planning - steps in planning & planning premises - Hierarchy of plans.
6 Hours
UNIT - 3
ORGANISING AND STAFFING: Nature and purpose of organization -
Principles of organization - Types of organization - Departmentation -
Committees – Centralisation Vs Decentralisation of authority and
responsibility - Span of control - MBO and MBE (Meaning only) Nature and
importance of Staffing - Process of Selection & Recruitment (in brief).
6 Hours
UNIT - 4
DIRECTING & CONTROLLING: Meaning and nature of directing -
Leadership styles, Motivation Theories, Communication - Meaning and
importance – Coordination, meaning and importance and Techniques of Co -
ordination. Meaning and steps in controlling - Essentials of a sound control
system - Methods of establishing control.
7 Hours
5
PART - B
ENTREPRENEURSHIP
UNIT - 5
ENTREPRENEUR: Meaning of Entrepreneur; Evolution of the Concept,
Functions of an Entrepreneur, Types of Entrepreneur, Intrapreneur - an
emerging Class. Concept of Entrepreneurship - Evolution of
Entrepreneurship, Development of Entrepreneurship; Stages in
entrepreneurial process; Role of entrepreneurs in Economic Development;
Entrepreneurship in India; Entrepreneurship – its Barriers.
6 Hours
UNIT - 6
SMALL SCALE INDUSTRY: Definition; Characteristics; Need and
rationale: Objectives; Scope; role of SSI in Economic Development.
Advantages of SSI Steps to start an SSI - Government policy towards SSI;
Different Policies of S.S.I.; Government Support for S.S.I. during 5 year
plans, Impact of Liberalization, Privatization, Globalization on S.S.I., Effect
of WTO/GATT Supporting Agencies of Government for S.S.I Meaning;
Nature of Support; Objectives; Functions; Types of Help; Ancillary Industry
and Tiny Industry (Definition only).
7 Hours
UNIT - 7
INSTITUTIONAL SUPPORT: Different Schemes; TECKSOK; KIADB;
KSSIDC; KSIMC; DIC Single Window Agency: SISI; NSIC; SIDBI; KSFC.
6 Hours
UNIT - 8
PREPARATION OF PROJECT: Meaning of Project; Project
Identification; Project Selection; Project Report; Need and Significance of
Report; Contents; formulation; Guidelines by Planning Commission for
Project report; Network Analysis; Errors of Project Report; Project
Appraisal. Identification of Business Opportunities - Market Feasibility
Study; Technical Feasibility Study; Financial Feasibility Study & Social
Feasibility Study.
7 Hours
TEXT BOOKS:
1. Principles of Management - P. C. Tripathi, P. N. Reddy; Tata
McGraw Hill.
2. Dynamics of Entrepreneurial Development & Management -
Vasant Desai Himalaya Publishing House.
3. Entrepreneurship Development - Small Business Enterprises -
Poornima M Charantimath - Pearson Education – 2006.
6
REFERENCE BOOKS:
1. Management Fundamentals - Concepts, Application, Skill
Development Robert Lusier – Thomson.
2. Entrepreneurship Development - S S Khanka - S Chand & Co.
3. Management - Stephen Robbins - Pearson Education /PHI -17th
Edition, 2003.
7
ELEMENTS OF AERONAUTICS
Subject Code : 06AE52 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART - A
UNIT – 1
HISTORICAL DEVELOPMENTS IN AEROSPACE: Early airplanes,
biplanes and monoplanes, Developments in aerodynamics, materials,
structures and propulsion over the years.
6 Hours
UNIT – 2
AIRCRAFT CONFIGURATIONS: Different types of flight vehicles and
classifications. Components of an airplane and their functions. Airfoils,
wings and other shapes.
6 Hours
UNIT – 3
PRINCIPLES OF ATMOSPHERIC FLIGHT: Physical properties and
structure of the atmosphere, The Standard Atmosphere, Temperature,
Pressure and Altitude relationships, Evolution of lift, drag and moment,
Airfoils, Mach number, Maneuvers, Concepts of stability and control.
8 Hours
UNIT – 4
INTRODUCTION TO SPACE FLIGHT: Introduction to basic concepts,
The upper atmosphere, Differential equations, Lagrange’s equation, Orbit
equation, Space vehicle trajectories-some basic concepts, Kepler’s Laws of
planetary motion.
6 Hours
PART - B
UNIT – 5
AIRCRAFT STRUCTURES AND AIRCRAFT MATERIALS: General
types of construction, Monocoque, semi-monocoque and geodesic
construction, typical wing and fuselage structure. Metallic and non-metallic
materials for aircraft application.
6 Hours
8
UNIT – 6
AIRCRAFT 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.
8 Hours
UNIT – 7
AIRCRAFT SYSTEMS: MECHANICAL: Description of different
airplane systems and their components: Hydraulics, Pneumatic, Oxygen
System, Environmental Control System, Fuel System.
6 Hours
UNIT – 8
AIRCRAFT SYSTEMS: ELECTRICAL: Flight Control System, Aircraft
Electrical System, Aircraft Instruments, Navigation System, Communication
System.
6 Hours
TEXT BOOKS:
1. Introduction to Flight, ,Anderson, J.D., McGraw-Hill, 1995.
2. Fundamentals of Flight Vol. IV Aircraft Systems, Lalit Gupta
and Dr. O. P. Sharma., Himalayan Books, 2006
REFERENCE:
1. Flight without Formulae, Kermode, A.C., McGraw-Hill, 1997.
2. Introduction to Aircraft Basic Science, Kroes, Michael J and
Rardon, JamesR”, 7th Edition, Macmillan / McGraw Hill, 1993.
3. Space Vehicle Design, 2nd Edition AIAA Education Series,
Michael D. Griffin, James R. French by Michael D.
4. Mechanics of Flight, (Revised by RH Bernard & DR Philpott),
Kermode, A.C., LPE, Pearson Education, 2005.
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
9
DYNAMICS OF MACHINES
Subject Code : 06AE53 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
STATIC FORCE ANALYSIS: Static force analysis: Introduction: Static
equilibrium. Equilibrium of two and three force members. Members with two
forces and torque, Free body diagrams, principle of virtual work. Static force
analysis of four bar mechanism and slider-crank mechanism with and without
friction.
6 Hours
UNIT – 2
DYNAMIC FORCE ANALYSIS: D’Alembert’s principle, Inertia force,
inertia torque, Dynamic force analysis of four-bar mechanism and slider
crank mechanism. Dynamically equivalent systems. Turning moment
diagrams and flywheels, Fluctuation of Energy. Determination of size of
flywheels.
8 Hours
UNIT – 3
FRICTION AND BELT DRIVES: Definitions: Types of friction: laws of
friction, Friction in pivot and collar bearings. Belt drives: Flat belt drives,
ratio of belt tensions, centrifugal tension, power transmitted.
6 Hours
UNIT – 4
BALANCING OF ROTATING MASSES: Static and dynamic balancing,
Balancing of single rotating mass by balancing masses in same plane and in
different planes. Balancing of several rotating masses by balancing masses in
same plane and in different planes.
6 Hours
PART – B
UNIT – 5
BALANCING OF RECIPROCATING MASSES: Inertia effect of crank
and connecting rod, single cylinder engine, balancing in multi cylinder-inline
10
engine primary & Secondary forces, V-type engine; Radial engine – Direct
and reverse crank method.
8 Hours
UNIT – 6
GOVERNORS: Types of governors; force analysis of Porter and Hartnell
governors. Controlling force, stability, sensitiveness, isochronism, effort and
power.
6 Hours
UNIT – 7
GYROSCOPE: Vectorial representation of angular motion, Gyroscopic
couple. Effect of gyroscopic couple on ship, plane disc, aeroplane, stability of
two wheelers and four wheelers.
6 Hours
UNIT – 8
ANALYSIS OF CAMS: Analysis of Tangent cam with roller follower and
Circular arc cam operating flat faced and roller followers, Undercutting in
Cams.
6 Hours
TEXT BOOKS:
1. Theory of Machines: Sadhu Singh, Pearson Education, 2nd edition,
2007.
2. Theory of Machines: Rattan S.S. Tata McGraw Hill Publishing
Company Ltd., New Delhi, 2nd Edition, 2006.
REFERENCE BOOKS:
1. Theory of Machines by Thomas Bevan, CBS Publication 1984.
2. Design of Machinery by Robert L. Norton, McGraw Hill, 2001.
3. Mechanisms and Dynamics of Machinery by J. Srinivas, Scitech
Publications, Chennai, 2002.
4. Dynamics of machinery by J. B. K. Das & P. L. S. Murthy.
11
AERODYNAMICS - I
Subject Code : 06AE54 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
REVIEW OF BASIC FLUID MECHANICS: Continuity, momentum and
energy equation, units and dimensions, inviscid and viscous flows,
compressibility, Mach number regimes.
6 Hours
UNI1 – 2
DESCRIPTION OF FLUID MOTION: Euler and Lagrangian
descriptions, control volume approach to continuity and momentum
equations, pathlines, streamlines and streaklines, angular velocity, vorticity,
circulation, stream function, velocity potential and relationship between
them.
6 Hours
UNIT – 3
AIRFOIL CHARACTERISTICS : Fundamental aerodynamic variables,
airfoil section geometry and wing planform geometry, aerodynamic forces
and moments, centre of pressure, pressure coefficient, calculation of airfoil
lift and drag from measured surface pressure distributions, typical airfoil
aerodynamic characteristics at low speeds.
6 Hours
UNIT – 4
TWO-DIMENSIONAL INVISCID INCOMPRESSIBLE FLOWS:
Bernoulli’s equation, pitot-tube measurement of airspeed, condition on
velocity for incompressible flow, Eulers equations of motion, Governing
equations for irrotational, incompressible flow, Laplace equation and
boundary conditions. Two-dimensional source, sink, doublet and vortex
flows.
8Hours
12
PART – B
UNIT – 5
FLOW OVER CIRCULAR CYLINDERS: Non-lifting flow over a twodimensional
circular cylinder, Lifting flow over a two-dimensional circular
cylinder, Kutta-Joukowski theorem and generation of lift, D’Alembert’s
paradox.
6 Hours
UNIT – 6
INCOMPRESSIBLE FLOW OVER AIRFOILS: Kelvin’s circulation
theorem and the starting vortex, vortex sheet, Kutta condition, Classical thin
airfoil theory for symmetric and cambered airfoils.
6 Hours
UNIT – 7
INTRODUCTION TO VISCOUS FLOWS:
Navier-Stokes equations, boundary layer concept, displacement, momentum
thickness and wall skin friction, viscous flow over two-dimensional
streamlined and bluff bodies and drag characteristics, aspects of boundary
layer separation and airfoil stall.
6 Hours
UNIT – 8
INTRODUCTION TO AERODYNAMIC TESTING:
Principles of wind tunnel flow simulation, open and closed circuit wind
tunnels, Major features of low speed, transonic and supersonic wind tunnels,
smoke and tuft flow visualization techniques, Pressure and Aerodynamic load
measurements on a model, total drag determination of two-dimensional
bodies using wake survey at low speeds.
8 Hours
TEXT BOOKS:
1. Fundamentals of Aerodynamics, Anderson, Jr. J.D. Tata McGraw-
Hill Publishing Co. Ltd., New Delhi, 2007. (Special Indian Edition).
2. Aerodynamics for Engineering Students, Houghton E.L and
Carpenter P.W., CBS Publications and Distributors, 1993. (4th
Edition).
13
REFERENCE BOOKS:
1. Low Speed Wind Tunnel testing, ,Pope A. and Harper, J J John
Wiley Inc. New York, 1966.
2. Introduction to Flight, Anderson, Jr. J.D., Tata McGraw-Hill
Publishing Co. Ltd., New Delhi, 2007. (Special Indian Edition).
3. Boundary Layer Theory, Schlichting, H. Mc Graw Hill, New
York, 2004.
4. Mechanics of Fluids, Duncan WJ, Thom AS and Young AD.,
Second Edition, Edward Arnold Printers Ltd, London, 1981.
5. High Speed Wind Tunnel Testing, Pope A. and Goin, KL., John
Wiley & Sons Inc. New York, 1965.
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
14
AIRCRAFT PROPULSION
Subject Code : 06AE55 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION: Review of thermodynamic principles, Principles of
aircraft propulsion, Types of power plants, Working principles of internal
combustion engine, Two – stroke and four – stroke piston engines, Gasturbine
engines, Cycle analysis of reciprocating engines and jet engines.
6 Hours
UNIT – 2
FUNDAMENTALS OF GAS TURBINE 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.
7 Hours
UNIT – 3
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.
7 Hours
UNIT – 4
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.
6 Hours
15
PART – B
UNIT – 5
NOZZLES: Theory of flow in isentropic nozzles – Convergent / Convergent
– divergent nozzles; Nozzle throat conditions – Nozzle efficiency – Losses in
nozzles – Over expanded and under – expanded nozzles - Thrust reversal.
7 Hours
UNIT – 6
COMPRESSORS: Principle of operation of centrifugal compressor – Work
done and pressure rise – Velocity diagrams – Diffuser vane design
considerations – Concept of prewhirl – Rotation stall – Elementary theory of
axial flow compressor – Velocity triangles – degree of reaction -Centrifugal
and Axial compressor performance characteristics.
7 Hours
UNIT – 7
INTRODUCTION TO TURBINES: Types of turbines – Design
considerations – Performance parameters - Basics of blade design principles.
6 Hours
UNIT – 8
RAMJET PROPULSION: Operating principle – Sub critical, critical and
supercritical operation – Combustion in ramjet engine – Ramjet performance
– Introduction to scramjet – Preliminary concepts in supersonic
combustion.
6 Hours
TEXT BOOKS:
1. Gas Turbine, V. Ganesan, , Tata McGraw Hill Pub. Co. Ltd., 1996.
2. Mechanics & Thermodynamics of Propulsion, Hill, P.G. &
Peterson, C.R. Addison – Wesley Longman INC, 1999.
REFERENCE BOOKS:
1. Gas Turbine Theory, ,Cohen, H. Rogers, G.F.C. and
Saravanamuttoo, H.I.H. “Longman, 1989.
2. Aero thermodynamics of Aircraft Engine Components, Oates,
G.C., , AIAA Education Series, New York, 1985.
3. Gas Turbine, Jet and Rocket Propulsion, Mathur, M.L. and
Sharma, R.P., , Standard Publishers & Distributors, Delhi, 1999.
16
Scheme of Examination:
One Question to be set from each Unit. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
17
AIRCRAFT STRUCTURES – I
Subject Code : 06AE56 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
LOADS ON AIRCRAFT: Structural nomenclature-types of loads, load
factor, aerodynamic loads, symmetric manoeuvre loads and functions of
structural components.
6 Hours
UNIT – 2
MATERIALS FOR AIRCRAFT STRUCTURES: Metallic and nonmetallic
materials, Use of Aluminium alloy, titanium, stainless steel and
composite materials. Desirable properties for aircraft application.
6 Hours
UNIT – 3
MECHANICAL PROPERTIES OF MATERIAL: Stress – Strain -
Tensile properties – Compression properties – Shear properties – Bearing
properties – Creep and Stress properties – Fracture properties –Fatigue
properties.
6 Hours
UNIT – 4
STATICALLY DETERMINATE AND INTERDETERMINATE
STRUCTURES: Analysis of plane truss – Method of joints – 3 D Truss -
Plane frames Composite beam –Clapeyron's Three Moment Equation -
Moment Distribution Method.
8 Hours
PART – B
UNIT – 5
ENERGY METHODS: Strain Energy due to axial, bending and Torsional
loads - Castigliano's theorem - Maxwell's Reciprocal theorem, Unit load
method - application to beams, trusses, frames, rings, etc.
6 Hours
18
UNIT – 6
COLUMNS: Columns with various end conditions – Euler’s Column curve
– Rankine’s formula - Column with initial curvature - Eccentric loading –
South well plot – Beam column..
6 Hours
UNIT – 7
THEORY OF ELASTICITY: Concept of stress and strain, derivation of
Equilibrium equations, strain-displacement relation, compatibility conditions
and boundary conditions. Plane stress and Plane strain problems in 2-D
elasticity and Airy’s Stress function.
8 Hours
UNIT – 8
FAILURE THEORY: Maximum Stress theory – Maximum Strain Theory –
Maximum Shear Stress Theory – Distortion Theory – Maximum Strain
energy theory – Application to aircraft Structural problems.
6 Hours
TEXT BOOKS:
1. Aircraft Structures for Engineering Students, Megson, T.M.G., ,
Edward Arnold, 1995.
2. Theory of Elasticity, Timoshenko and Godier Mc Graw Hill Co.
REFERENCE BOOKS:
1. Analysis of Aircraft Structures – An Introduction, Donaldson,
B.K., McGraw-Hill, 1993.
2. Strength of Materials, Timoshenko, S., Vol. I and II, Princeton D.
Von Nostrand Co, 1990.
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
19
STRUCTURES LABORATORY
Subject Code : 06AEL57 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 42 Exam Marks : 50
LIST OF EXPERIMENTS
1. Deflection of a Simply Supported Beam.S
2. Verification of Maxwell's Reciprocal Theorem.
3. Determination of Young’s Modulus using strain gages.
4. Poisson Ratio Determination.
5. Buckling Load of Slender Eccentric Columns and Construction of
Southwell Plot
6. Shear failure of Bolted and Riveted Joints.
7. Bending Modulus of a Sandwich Beam
8. Verification of the Superposition Theorem.
20
ENERGY CONVERSION LABORATORY
Subject Code : 06AEL58 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 42 Exam Marks : 50
PART – A
(INDIVIDUAL EXPERIMENTS)
1. Determination of Flash point and Fire point of lubricating oil using Abel
Pensky and Pensky Martins Apparatus.
2. Determination of Caloric value of solid, liquid and gaseous fuels.
3. Determination of Viscosity of lubricating oil using Redwoods, Saybolts
and Torsion Viscometers.
4. Valve, Timing/port opening diagram of an I.C. engine (4 stroke/
2stroke).
5. Use of planimeter.
21 Hours
PART – B
(GROUP EXPERIMENTS)
1. Performance Tests on I.C. Engines, Calculations of IP, BP, Thermal
efficiencies, SFC, FP, heat balance sheet for
(a) Four stroke Diesel Engine
(b) Four stroke Petrol Engine
(c) Multi-cylinder Diesel/Petrol Engine, (Morse test)
(d) Two stroke Petrol Engine
(e) Variable Compression Ratio I.C. Engine
21 Hours
21
VI SEMESTER
INTRODUCTION TO COMPOSITE MATERIALS
Subject Code : 06AE61 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART A
UNIT – 1
INTRODUCTION TO COMPOSITE MATERIALS: Definition,
classification and characteristics of composite materials - fibrous composites,
laminated composites, particulate composites. Properties and types of
Reinforcement and Matrix materials.
6 Hours
UNIT – 2
FIBER REINFORCED PLASTIC PROCESSING: Lay up and curing,
fabricating process - open and closed mould process - hand lay up
techniques structural laminate bag molding, production procedures for bag
molding.
6 Hours
UNIT – 3
ADVANCED PROCESSING TECHNIQUES AND APPLICATION OF
COMPOSITES: Filament winding, pultrusion, pulforming, thermo -
forming, injection, injection molding, liquid molding, blow molding,
Automobile, Aircrafts, missiles, Space hardware, Electrical and electronics,
marine, recreational and Sports equipment, future potential of composites.
8 Hours
UNIT – 4
FABRICATION OF COMPOSITE STRUCTURES: Cutting, machining,
drilling, mechanical fasteners and adhesive bonding, joining, computer-aided
design and manufacturing, tooling, fabrication equipment.
6 Hours
22
PART – B
UNIT – 5
MACRO-MECHANICAL BEHAVIOR OF A LAMINA: Stress-strain
relation for an orthotropic lamina- Restriction on elastic constants-Strengths
of an orthotropic lamina and Failure theories for an orthotropic lamina.
6 Hours
UNIT – 6
MICRO-MECHANICAL BEHAVIOR OF A LAMINA: Determination of
elastic constants-Rule of mixtures, transformation of coordinates, micromechanics
based analysis and experimental determination of material
constants.
6 Hours
UNIT – 7
MACRO-MECHANICAL BEHAVIOR OF A LAMINATE: Classical
plate theory- Stress and strain variation in a laminate- Resultant forces and
moments- A B & D matrices- Strength analysis of a laminate .
6 Hours
UNIT – 8
METAL MATRIX COMPOSITES: Reinforcement materials, types,
characteristics and selection of base metals. Application of MMC’s.
8 Hours
TEXT BOOKS:
1. Composites Science and Engineering, K.K Chawla, Springer
Verlag, 1998
2. Mechanics of Composite Materials, R M Jones,”, McGraw-Hill,
New York, 1975
REFERENCE BOOKS:
1. Composite materials hand book, Meing Schwaitz, ", McGraw Hill
Book Company. 1984
2. Introduction to Composite materials, Hull and Clyne, Cambridge
University Press, 2nd Edition, 1990.
3. Forming Metal handbook, 9th edition, ASM handbook, V15.
1988, P327 338.
4. Mechanics of composites by Artar Kaw, CRC Press. 2002.
23
Scheme of Examination:
One Question to be set from each Unit. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
24
AIRCRAFT STRUCTURES- II
Subject Code : 06AE62 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION TO AIRCRAFT STRUCTURAL DESIGN: Structural
layout of the Airplane and components, Structural design V-n diagram, loads
acting on major components such as wing, fuselage, tails, landing gear etc.,
Concept of allowable stress and margin of safety.
6 Hours
UNIT – 2
UNSYMMETRICAL BENDING: Bending stresses in beams of
unsymmetrical sections – Bending of symmetric sections with skew loads .
6 Hours
UNIT – 3
SHEAR FLOW IN OPEN SECTIONS:06Hrs
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.
6 Hours
UNIT – 4
SHEAR FLOW IN CLOSED SECTIONS: Bredt – Batho formula, Single
and multi – cell structures, Approximate methods, Shear flow in single &
multi-cell structures under torsion. Shear flow in single and multi-cell under
bending with walls effective and ineffective.
8 Hours
PART – B
UNIT – 5
BUCKLING OF PLATES: Rectangular sheets under compression, Local
buckling stress of thin walled sections, Crippling stresses by Needham’s and
25
Gerard’s methods, Thin walled column strength. Sheet – stiffener panels.
Effective width, inter rivet and sheet wrinkling failures.
6 Hours
UNIT – 6
STRESS ANALYSIS IN WING AND FUSELAGE: Procedure – Shear
and bending moment distribution for semi cantilever and other types of wings
and fuselage, thin webbed beam. With parallel and non parallel flanges,
Shear resistant web beams, Tension field web beams (Wagner’s).
8 Hours
UNIT – 7
DESIGN OF AIRCRAFT STRUCTURE: Design criteria – Safety
Factor – Design life criteria – Analysis method – Life Assessment
procedures – Design Principle – Future Airworthiness Requirements –
Two bay crack criteria – Widespread Fatigue damage.
6 Hours
UNIT – 8
JOINTS AND FITTINGS AND INTRODUCTION TO POST
BUCLKING: General theory for the design of fittings, Estimation of
fitting design loads, design of riveted, bolted and welding joints, post
buckling of structures, concept of effective width.
6 Hours
TEXT BOOKS:
1. “Aircraft Structures for Engineering Students, Megson, T.M.G.,,
Edward Arnold, 1995.
2. Aircraft Structures, Peery, D.J., and Azar, J.J., 2nd edition,
McGraw–Hill, N.Y., 1993.
REFEENCE BOOKS:
1. “Analysis and Design of Flight vehicles Structures, Bruhn. E.H.,
Tri – state off set company, USA, 1985.
2. “Theory and Analysis of Flight Structures, Rivello, R.M.,
McGraw-Hill, 1993.
3. An Introduction to the Theory of Aircraft Structures, D
Williams & Edward Arnold.
Scheme of Examination:
One Question to be set from each Unit. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
26
AERODYNAMICS - II
Subject Code : 06AE63 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION TO TWO-DIMENSIONAL PANEL METHODS:
Non-lifting flows over arbitrary bodies, source panel method, lifting flows
over arbitrary bodies, vortex panel method, some examples.
6 Hours
UNIT – 2
INCOMPRESSIBLE FLOWS OVER FINITE WINGS: Downwash,
Induced drag, vortex filament, the Biot-Savart Law, Prandtl’s lifting line
theory and its limitations, Elliptic lift distribution.
8 Hours
UNIT – 3
SUBSONIC LINEARIZED FLOW OVER AIRFOILS: Full velocity
potential equation, linearized velocity potential equation and boundary
condition, Prandtl-Glauret compressibility correction.
6 Hours
UNIT – 4
EFFECTS OF COMPRESSIBILITY: Critical Mach number; Dragdivergence
Mach number, Sound Barrier, Transonic area rule, Introduction to
shock-free airfoils.
6 Hours
PART – B
UNIT – 5
APPLICATIONS OF FINITE WING THEORY: Simplified horse-shoe
vortex model, formation flight, influence of downwash on tail plane, ground
effects.
6 Hours
27
UNIT – 6
BODIES OF REVOLUTION: Introduction to slender body theory,
cylindrical coordinates, boundary conditions, pressure coefficient, Subsonic
flow past a axially symmetric body at zero incidence and solution for a
slender cone.
6 Hours
UNIT – 7
SWEPT WINGS AND HIGH-LIFT SYSTEMS: Introduction to sweep
effects, swept wings, pressure coefficient, typical aerodynamic
characteristics, Subsonic and Supersonic leading edges. Introduction to highlift
systems, flaps, leading-edge slats and typical high - lift characteristics.
6 Hours
UNIT – 8
VISCOUS FLOWS: Derivation of Navier-Stokes equation for twodimensional
flows, boundary layer approximations, laminar boundary
equations and boundary conditions, Blasius solution, qualitative features of
boundary layer flow under pressure gradients, Integral method, aspects of
transition to turbulence, turbulent boundary layer properties over a flat plate
at low speeds.
8 Hours
EXT BOOKS:
1. Fundamentals of Aerodynamics, Anderson, Jr. J.D, Tata McGraw-
Hill Publishing Co. Ltd., New Delhi, 2007. (Special Indian Edition).
2. Boundary layer theory, Schlichting, H,”, McGraw Hill, New York
2004
REFERENCE BOOKS:
1. Aerodynamics for Engineers, Bertin, John J., Pearson Education
Inc., 2002.
2. Fluid Mechanics, White, F.M., Mc Graw Hill Inc. New York, 1986
3. Aerodynamics for Engineering Students, Houghton E.L and
Carpenter P.W., CBS Publications and Distributors,8 1993. (4th
Edition).
Scheme of Examination:
One Question to be set from each Unit (FOUR Questions from Part A and
Four Questions from Part B). Students have to answer any FIVE full
questions out of EIGHT questions, choosing at least TWO questions from
Part A and TWO questions from Part B.
28
FINITE ELEMENT ANALYSIS
Subject Code : 06AE64 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION: BASIC CONCEPTS, BACKGROUND REVIEW:
Theory of Elasticity, Matrix displacement formulation, Energy concepts,
Equilibrium and energy methods for analysing structures. Rayleigh - Ritz
Method, Galerkin's Method, Simple applications in structural Analysis.
6 Hours
UNIT – 2
FUNDAMENTALS OF FINITE ELEMENT METHOD: Displacement
function and natural coordinates, construction of displacement functions for 2
D truss and beam elements, applications of FEM for the analysis of truss,
continuous beam and simple frame problems.
6 Hours
UNIT – 3
DISCRETE ELEMENTS:Bar elements, uniform Bar elements, uniform
section, mechanical and thermal loading, varying section, truss analysis,
Frame element, Beam element, problems for various loadings and boundary
conditions, Free vibration, longitudinal and lateral vibration, Use of local and
natural coordinates.
8 Hours
UNIT – 4
CONTINUUM ELEMENTS: Plane stress, Plane strain and
axisymmetric problems, constant and linear strain, triangular elements,
stiffness matrix, axisymmetric load vector.
6 Hours
PART – B
UNIT – 5
ANALYSIS OF 2 D CONTINUUM PROBLEMS: Elements and shape
functions, Triangular, rectangular and quadrilateral elements, different types
29
of elements, their characteristics and suitability for application, polynomial
shape functions, Lagrange's and Hermitian polynomials, compatibility and
convergence requirements of shape functions.
8 Hours
UNIT – 6
THEORY OF ISOPARAMETRIC ELEMENTS: Isoparametric, sub
parametric and super-parametric elements, characteristics of Isoparametric
quadrilateral, elements, structure of computer program for FEM analysis,
description of different modules, pre and post processing.
6 Hours
UNIT – 7
FIELD PROBLEMS: Heat transfer problems, Steady' state fin problems,
Derivation of element matrices for two dimensional problems, Torsion
problems.
6 Hours
UNIT – 8
INTRODUCTION TO FINITE ELEMENT METHOD :Construction or
discrete models - sub domains and nodes - simple elements for the FEM -
Simplex, complex and multiples elements Polynomial selection - illustrative
examples.
6 Hours
TEXT BOOKS:
1. Finite Element analysis - Theory and Programming, C.S.
Krishnamurthy -, Tata McGraw Hill Co. Ltd, New Delhi.
2. Chandrupatla, T R and Belegundu, A.D - Introduction to Finite
elements in Engineering”, Printice Hall, Newyork, 2002.
REFERENCE BOOKS:
1. Finite element analysis in engineering design, Rajasekharan. S -
Wheeler Publishers
2. Finite Element Procedures, Bathe. KJ , PHI Pvt. Ltd., New Delhi
3. The Finite Element Method, Zienkiewicz. O.C., Tata McGraw
Hill Co. Ltd, New Delhi.
Scheme of Examination:
One Question to be set from each Unit (FOUR Questions from Part A and
Four Questions from Part B). Students have to answer any FIVE full
questions out of EIGHT questions, choosing at least TWO questions from
Part A and TWO questions from Part B.
30
THEORY OF VIBRATIONS
Subject Code : 06AE65 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION: Types of vibrations, S.H.M, principle of super position
applied to Simple Harmonic Motions. Beats, Fourier theorem and simple
problems.
6 Hours
UNIT – 2
UNDAMPED FREE VIBRATIONS: Single degree of freedom systems.
Undamped free vibration,natural frequency of free vibration, Spring and
Mass elements, effect of mass of spring, Compound Pendulum.
7 Hours
UNIT – 3
DAMPED FREE VIBRATIONS: Single degree of freedom systems,
different types of damping, concept of critical damping and its importance,
study of response of viscous damped systems for cases of under damping,
critical and over damping, Logarithmic decrement.
7 Hours
UNIT – 4
FORCED VIBRATION: Single degree of freedom systems, steady state
solution with viscous damping due to harmonic force. Solution by Complex
algebra, reciprocating and rotating unbalance, vibration isolation,
transmissibility ratio. due to harmonic exitation and support motion.
6 Hours
PART – B
UNIT – 5
VIBRATION MEASURING INSTRUMENTS & WHIRLING OF
SHAFTS: Vibrometer meter and accelerometer. Whirling of shafts with and
without air damping. Discussion of speeds above and below critical speeds.
6 Hours
31
UNITL – 6
SYSTEMS WITH TWO DEGREES OF FREEDOM: Introduction,
principle modes and Normal modes of vibration, co-ordinate coupling,
generalized and principal co-ordinates, Free vibration in terms of initial
conditions. Geared systems. Forced Oscillations-Harmonic excitation.
Applications:
a) Vehicle suspension.
b) Dynamic vibration absorber.
c) Dynamics of reciprocating Engines.
8 Hours
UNIT – 7
CONTINUOUS SYSTEMS: Introduction, vibration of string, longitudinal
vibration of rods, Torsional vibration of rods, Euler’s equation for beams.
6 Hours
UNIT – 8
NUMERICAL METHODS FOR MULTI-DEGREE FREEDOM
SYSTEMS: Introduction, Influence coefficients, Maxwell reciprocal
theorem, Dunkerley’s equation. Orthogonality of principal modes, Method of
matrix iteration-Method of determination of all the natural frequencies using
sweeping matrix and Orthogonality principle. Holzer’s method, Stodola
method.
8 Hours
TEXT BOOKS:
1. Theory of Vibration with Applications: W.T. Thomson and Marie
Dillon Dahleh, Pearson Education 5th edition, 2007.
2. Mechanical Vibrations: V.P. Singh, Dhanpat Rai & Company Pvt.
Ltd., 3rd edition, 2006
REFERENCE BOOKS:
1. Mechanical Vibrations: S.S. Rao, Pearson Education Inc, 4th
Edition, 2003.
2. Mechanical Vibrations: S. Graham Kelly, Schaum’s Outline
Series, Tata McGraw Hill, Special Indian edition, 2007.
3. Theory & Practice of Mechanical vibrations: J.S. Rao & K.
Gupta, New Age International Publications, New Delhi, 2001.
4. Elements of Vibrations Analysis: Leonanrd Meirovitch, Tata
McGraw Hill, Special Indian edition, 2007.
32
Scheme of Examination:
Four Questions from Part A and FOUR questions from Part B (One Question
to be set from each Unit) Students have to answer any FIVE full questions
out of EIGHT questions, choosing at least TWO questions from Part A and
TWO questions from Part B.
VI Semester
Electives: 06AE66*
* Elective - I: (Group A)
Sub Code Title
06AE661 Numerical Methods
06AE662 Aircraft Materials
06AE663 Combustion
06AE664 Reliability Engineering
06AE665 Industrial Management
33
NUMERICAL METHODS
(ELECTIVE GROUP – A)
Subject Code : 06AE661 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
NUMERICAL COMPUTATION: Motivation and Objectives/ Number
Representation/ Machine Precision/ Round-of - Error/ Truncation Error/
Random Number Generation.
6 Hours
UNIT – 2
LINEAR ALGEBRAIC SYSTEMS: Motivation and Objectives/ Gauss-
Jordan Elimination/ Gaussian Elimination/ LU Decomposition/ IIIConditioned
Systems/ Iterative Methods.
6 Hours
UNIT – 3
INTERPOLATION AND APPROXIMATION: Lagrangian Polynomials -
Divided differences Interpolating with a cubic spline - Newton's forward and
backward difference formulas.
6 Hours
UNIT – 4
EIGEN VALUES AND EIGENVECTORS: Motivation and Objectives/
The characteristics Polynominal/ Power Methods / Jacobi’s Method/
Householder Transformation/ QR Method/ Danilevsky’s Method/
Polynominal Roots.
8 Hours
34
PART – B
UNIT – 5
NUMERICAL DIFFERENTIATION AND INTEGATION: Derivative
from difference tables - Divided differences and finite differences -
Numerical integration by trapezoidal and Simpson's 1/3 and 3/8 rules - Two
and Three point Gaussian quadrature formulas - Double integrals using
trapezoidal and Simpson's rules.
8 Hours
UNIT – 6
CURVE FITTING: Motivation and objectives/ Interpolation/ Newton’s
Difference Formula/ Cubic Splines/ Least Square/ Two-Dimensional
Interpolation.
6 Hours
UNIT – 7
ROOT FINDING: Motivation and Objectives/ Bracketing methods/
Contraction Mapping Method/ Se cant Method/ Muller’s Method/ Newton’s
Method/ Polynomial Roots/ Nonlinear Systems of Equations.
6 Hours
UNIT – 8
OPTIMIZATION: Motivation and Objectives/ Local and Global Minima /
Line Searches / Steepest Descent Method / Conjugate-Gradient Method /
Quasi-Newton Methods / Penalty Functions / Simulated Annealing.
6 Hours
TEXT BOOKS:
1. Applied Numerical methods for Engineers Using Mat Lab and
C-Robert Schilling and Sandra Harris, Thomson Learning, 2002.
2. Applied Numerical Analysis – Gerald and Wheatley, Pearson
Education, 2002.
REFERENCE BOOK:
1. Numerical Recipes in C – William Press et. Al., 2e, Cambridge
University Press.
35
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
36
AIRCRAFT MATERIALS
(ELECTIVE GROUP – A)
Subject Code : 06AE662 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION TO AIRCRAFT MATERIALS: General properties of
materials, Definition of terms, Requirements of aircraft materials, Testing of
aircraft materials, Inspection methods, Application and trends in usage in
aircraft structures and engines, Introduction to smart materials and nanomaterials;
Selection of materials for use in aircraft.
6 Hours
UNIT – 2
AIRCRAFT METAL ALLOYS AND SUPERALLOYS: Aluminum
alloys, Magnesium alloys, Titanium alloys, Plain carbon and Low carbon
Steels, Corrosion and Heat resistant steels, Maraging steels, Copper alloys,
Producibility and Surface treatments aspects for each of the above; General
introduction to superalloys, Nickel based superalloys, Cobalt based
superalloys, and Iron based superalloys, manufacturing processes associated
with superalloys, Heat treatment and surface treatment of superalloys.
8 Hours
UNIT – 3
COMPOSITE MATERIALS: Definition and comparison of composites
with conventional monolithic materials, Reinforcing fibers and Matrix
materials, Fabrication of composites and quality control aspects, Carbon -
Carbon Composites production, properties and applications, inter metallic
matrix composites, ablative composites based on polymers, ceramic matrix,
metal matrix composites based on aluminum, magnesium, titanium and
nickel based composites for engines.
6 Hours
37
UNIT – 4
POLYMERS, POLYMERIC MATERIALS & PLASTICS AND
CERAMICS & GLASS : Knowledge and identification of physical
characteristics of commonly used polymeric material: plastics and its
categories, properties and applications; commonly used ceramic, glass and
transparent plastics, properties and applications, adhesives and sealants and
their applications in aircraft.
6 Hours
PART – B
UNIT – 5
ABLATIVE AND SUPER CONDUCTING MATERIALS: Ablation
process, ablative materials and applications in aerospace; Phenomenon of
super conduction, super conducting materials and applications in aerospace.
6 Hours
UNIT – 6
AIRCRAFT WOOD, RUBBER, FABRICS & DOPE AND PAINT:
Classification and properties of wood, Seasoning of wood, Aircraft woods,
their properties and applications, Joining processes for wood, Plywood;
Characteristics and definition of terminologies pertaining to aircraft fabrics
and their applications, Purpose of doping and commonly used dopes; Purpose
of painting, Types of aircraft paints, Aircraft painting process.
7 Hours
UNIT – 8
CORROSION AND ITS PREVENTION: Knowledge of the various
methods used for removal of corrosion from common aircraft metals and
methods employed to prevent corrosion.
6 Hours
UNIT – 8
HIGH ENERGY MATERIALS: Materials for rockets and missiles. Types
of propellants and its general and desirable properties, Insulating materials
for cryogenic engines. Types of solid propellants: Mechanical
characterization of solid propellants using uni-axial, strip-biaxial and tubular
tests.
7 Hours
38
TEXT BOOKS:
1. Handbook of Aircraft materials Interline publishers, C G
Krishnadas Nair, , Bangalore, 1993.
2. Aicraft Material and Processes, Titterton G F, , English Book
Store, New Delhi, 1998
REFERENCE:
1. Advanced Aerospace Material, H Buhl, Spring Berlin 1992
2. Aerospace material Vol. 1,2,3 ARDB, Balram Gupta, S Chand &
Co 1996
3. Materials for Missiles and Space, Parker E R, John Wiley.
4. The Materials of Aircraft Construction, Hill E T, Pitman
London.
5. AIAA Journal of Propulsion and Power, 2001
39
COMBUSTION
(ELECTIVE GROUP – A)
Subject Code 06AE663 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART A
UNIT – 1
REVIEW OF BASIC CONCEPTS: Laws of thermodynamics, Multicomponent
mixtures, simple thermo chemical equations and heat of
combustion, properties of real gases, transport phenomena, Rankine-
Hugoniot curves, ideas of deflagration and detonation.
6 Hours
UNIT – 2
CHEMICAL EQUILIBRIUM AND KINETICS: Concept of chemical
equilibrium in multicomponent mixtures, Elements of adiabatic flame
temperature calculation, Chemical kinetics – rates and order of reactions,
Reaction mechanism and chain reactions.
6 Hours
UNIT – 3
DIFFUSION FLAMES: Differences between premixed and diffusion
flames, gas diffusion flames in parallel flow – jet flames and Burke
Schumann flames, Liquid droplet combustion.
6 Hours
UNIT – 4
PREMIXED FLAMES: Mechanistic description of premixed flames,
Burning velocity and parametric dependences, Experimental methods of
measuring burning velocity, Simple one-dimensional thermal theory of
flame, concepts of minimum ignition energy, quenching distance, stability
limits and flame stabilization.
8 Hours
40
PART – B
UNIT – 5
COMBUSTION IN PISTON ENGINES: Review of operation of
reciprocating engines, Description of the combustion process in piston
engines, Combustion efficiency and factors affecting it, detonation in
reciprocating engines and preventive methods.
6 Hours
UNIT – 6
COMBUSTION IN GAS-TURBINE ENGINES: Description of different
types of combustion chambers in gas-turbine engines, primary requirements
of the combustor, Flow structure, recirculation and flame stabilization in
main combustion chamber, afterburners.
7 Hours
UNIT – 7
COMBUSTION IN ROCKET ENGINES: Combustion of carbon
particle, boundary layer combustion, basic principles of combustion solid
propellants, extension of droplet combustion to liquid propellant rockets.
7 Hours
UNIT – 8
EMISSIONS: Flame radiation, pollutants - unburnt hydrocarbons, oxides of
nitrogen and carbon monoxide, methods of reducing pollutants, Principle of
exhaust gas analysis.
6 Hours
TEXT BOOKS:
1. Introduction to Combustion by Stephen Turns.
2. Combustion fundamentals by Roger Strehlow
REFERENCE BOOKS:
1. Industrial Combustion by Charles E. Baukal.
2. Heat Transfer in Industrial Combustion by CE Baukal Jr
3. Combustion, Fossil Power Systems by G. Singer. 4th Ed. 1966 Ed
Pub.
4. Fuels and Combustion, Sharma, S.P., and Chandra Mohan , Tata
Me. Graw Hill Publishing Co.,Ltd., New Delhi, 1987.
5. Gas Turbine, Jet and Rocket Propulsion, Mathur, M.L., and
Sharma, R.P., ,' Standard Publishers and Distributors, Delhi, 1988
41
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
42
RELIABILITY ENGINEERING
(ELECTIVE GROUP – A)
Subject Code : 06AE664 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
INTRODUCTION: Reliability concepts and definitions, probability
distribution functions and their application in reliability Evaluation,
Reliability Evaluation in Engineering systems using Markov Models.
7 Hours
UNIT – 2
FAILURE ANALYSIS: Causes of failure, concept of hazard failure models,
Bath Tub curve, MTTF, MTBF.
7 Hours
UNIT – 3
RELIABILITY MODELING: System reliability for various configurations
and combinational aspects, Weibull analysis on reliability.
6 Hours
UNIT – 4
RELIABILITY STUDIES: Reliability improvement, redundancy,
reliability-cost trade-off.
PART – B
UNIT – 5
MAINTAINABILITY AND AVAILABILITY CONCEPTS: System
Safety analysis.
6 Hours
43
UNIT – 6
MAINTENANCE CONCEPTS: Types of Maintenance, Modern trends in
Maintenance Philosophy like BITE, IRAN, HUM, TPM etc.
7 Hours
UNIT – 7
FAILURE INVESTIGATION PROCESS AND METHODOLOGIES
LIKE FTA, FMEA
6 Hours
UNIT – 8
RELIABILITY AND QUALITY IMPROVEMENT techniques like,
Bench Marking, JIT, Quality Circles, Quality Audit, TQM, Kaizan etc.
7 Hours
TEXT BOOK:
1. Introduction to Reliability Engineering, E.E. Lewis, John Wiley.
REFERENCE BOOKS:
1. Probability and statistics with Reliability, Queuing and
Computer, K.S. Trivedi,
2. Science Applications, PHI.
3. Reliability Engineering, E Balagurswamy, Tata McGraw Hill
Publications.
Scheme of Examination:
Four questions from Part A and Four questions from Part B to be set Students
have to answer any FIVE full questions out of EIGHT questions, choosing at
least TWO questions from part A and TWO questions from part B
44
INDUSTRIAL MANAGEMENT
(ELECTIVE GROUP – A)
Subject Code : 06AE665 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
Note:
As per the decision of Chairman BOS, VTU the relevant detailed revised
syllabus may be incorporated by VTU.
'.. .
45
AERODYNAMICS LABORATORY
Subject Code : 06AEL67 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 42 Exam Marks : 50
LIST OF EXPERIMENTS
1. Calibration of a subsonic wind tunnel: test section static pressure and
total head distributions.
2. Smoke flow visualization studies on a two-dimensional circular cylinder
at low speeds.
3. Smoke flow visualization studies on a two dimensional airfoil at
different angles of incidence at low speeds
4. Tuft flow visualization on a wing model at different angles of incidence
at low speeds: identify zones of attached and separated flows.
5. Surface pressure distributions on a two-dimensional circular cylinder at
low speeds and calculation of pressure drag.
6. Surface pressure distributions on a two-dimensional symmetric airfoil at
zero incidence at low speeds.
7. Surface pressure distributions on a two-dimensional cambered airfoil at
different angles of incidence and calculation of lift and pressure drag.
8. Calculation of total drag of a two-dimensional circular cylinder at low
speeds using pitot-static probe wake survey.
9. Calculation of total drag of a two-dimensional cambered airfoil at low
speeds at incidence using pitot-static probe wake survey.
10. Measurement of a typical boundary layer velocity profile on the tunnel
wall (at low speeds) using a pitot probe and calculation of boundary
layer displacement and momentum thickness.
46
PROPULSION LABORATORY
Subject Code : 06AEL68 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 42 Exam Marks : 50
(Wind Tunnel is required)
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 an aircraft jet engine (Includes study of assembly of sub
systems, various components, their functions and operating principles)
3. Study of forced convective heat transfer over a flat plate.
4. Cascade testing of a model of axial compressor blade row.
5. Study of performance of a propeller.
6. Determination of heat of combustion of aviation fuel.
7. Study of free jet
8. Measurement of burning velocity of a premixed flame.
9. Fuel-injection characteristics
10. Measurement of nozzle flow.
4
V SEMESTER
MANAGEMENT & ENTREPRENEURSHIP
Subject Code : 06AL51 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART - A
MANAGEMENT
UNIT - 1
MANAGEMENT: Introduction - Meaning - nature and characteristics of
Management, Scope and functional areas of Management - Management as a
Science, Art or Profession Management & Administration - Roles of
Management, Levels of Management, Development of Management
Thought-Early Management Approaches-Modern Management Approaches.
7 Hours
UNIT - 2
PLANNING: Nature, importance and purpose of planning process -
Objectives - Types of plans (Meaning only) - Decision making - Importance
of planning - steps in planning & planning premises - Hierarchy of plans.
6 Hours
UNIT - 3
ORGANISING AND STAFFING: Nature and purpose of organization -
Principles of organization - Types of organization - Departmentation -
Committees – Centralisation Vs Decentralisation of authority and
responsibility - Span of control - MBO and MBE (Meaning only) Nature and
importance of Staffing - Process of Selection & Recruitment (in brief).
6 Hours
UNIT - 4
DIRECTING & CONTROLLING: Meaning and nature of directing -
Leadership styles, Motivation Theories, Communication - Meaning and
importance – Coordination, meaning and importance and Techniques of Co -
ordination. Meaning and steps in controlling - Essentials of a sound control
system - Methods of establishing control.
7 Hours
5
PART - B
ENTREPRENEURSHIP
UNIT - 5
ENTREPRENEUR: Meaning of Entrepreneur; Evolution of the Concept,
Functions of an Entrepreneur, Types of Entrepreneur, Intrapreneur - an
emerging Class. Concept of Entrepreneurship - Evolution of
Entrepreneurship, Development of Entrepreneurship; Stages in
entrepreneurial process; Role of entrepreneurs in Economic Development;
Entrepreneurship in India; Entrepreneurship – its Barriers.
6 Hours
UNIT - 6
SMALL SCALE INDUSTRY: Definition; Characteristics; Need and
rationale: Objectives; Scope; role of SSI in Economic Development.
Advantages of SSI Steps to start an SSI - Government policy towards SSI;
Different Policies of S.S.I.; Government Support for S.S.I. during 5 year
plans, Impact of Liberalization, Privatization, Globalization on S.S.I., Effect
of WTO/GATT Supporting Agencies of Government for S.S.I Meaning;
Nature of Support; Objectives; Functions; Types of Help; Ancillary Industry
and Tiny Industry (Definition only).
7 Hours
UNIT - 7
INSTITUTIONAL SUPPORT: Different Schemes; TECKSOK; KIADB;
KSSIDC; KSIMC; DIC Single Window Agency: SISI; NSIC; SIDBI; KSFC.
6 Hours
UNIT - 8
PREPARATION OF PROJECT: Meaning of Project; Project
Identification; Project Selection; Project Report; Need and Significance of
Report; Contents; formulation; Guidelines by Planning Commission for
Project report; Network Analysis; Errors of Project Report; Project
Appraisal. Identification of Business Opportunities - Market Feasibility
Study; Technical Feasibility Study; Financial Feasibility Study & Social
Feasibility Study.
7 Hours
TEXT BOOKS:
1. Principles of Management - P. C. Tripathi, P. N. Reddy; Tata
McGraw Hill.
2. Dynamics of Entrepreneurial Development & Management -
Vasant Desai Himalaya Publishing House.
3. Entrepreneurship Development - Small Business Enterprises -
Poornima M Charantimath - Pearson Education – 2006.
6
REFERENCE BOOKS:
1. Management Fundamentals - Concepts, Application, Skill
Development Robert Lusier – Thomson.
2. Entrepreneurship Development - S S Khanka - S Chand & Co.
3. Management - Stephen Robbins - Pearson Education /PHI -17th
Edition, 2003.
7
ELEMENTS OF AERONAUTICS
Subject Code : 06AE52 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART - A
UNIT – 1
HISTORICAL DEVELOPMENTS IN AEROSPACE: Early airplanes,
biplanes and monoplanes, Developments in aerodynamics, materials,
structures and propulsion over the years.
6 Hours
UNIT – 2
AIRCRAFT CONFIGURATIONS: Different types of flight vehicles and
classifications. Components of an airplane and their functions. Airfoils,
wings and other shapes.
6 Hours
UNIT – 3
PRINCIPLES OF ATMOSPHERIC FLIGHT: Physical properties and
structure of the atmosphere, The Standard Atmosphere, Temperature,
Pressure and Altitude relationships, Evolution of lift, drag and moment,
Airfoils, Mach number, Maneuvers, Concepts of stability and control.
8 Hours
UNIT – 4
INTRODUCTION TO SPACE FLIGHT: Introduction to basic concepts,
The upper atmosphere, Differential equations, Lagrange’s equation, Orbit
equation, Space vehicle trajectories-some basic concepts, Kepler’s Laws of
planetary motion.
6 Hours
PART - B
UNIT – 5
AIRCRAFT STRUCTURES AND AIRCRAFT MATERIALS: General
types of construction, Monocoque, semi-monocoque and geodesic
construction, typical wing and fuselage structure. Metallic and non-metallic
materials for aircraft application.
6 Hours
8
UNIT – 6
AIRCRAFT 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.
8 Hours
UNIT – 7
AIRCRAFT SYSTEMS: MECHANICAL: Description of different
airplane systems and their components: Hydraulics, Pneumatic, Oxygen
System, Environmental Control System, Fuel System.
6 Hours
UNIT – 8
AIRCRAFT SYSTEMS: ELECTRICAL: Flight Control System, Aircraft
Electrical System, Aircraft Instruments, Navigation System, Communication
System.
6 Hours
TEXT BOOKS:
1. Introduction to Flight, ,Anderson, J.D., McGraw-Hill, 1995.
2. Fundamentals of Flight Vol. IV Aircraft Systems, Lalit Gupta
and Dr. O. P. Sharma., Himalayan Books, 2006
REFERENCE:
1. Flight without Formulae, Kermode, A.C., McGraw-Hill, 1997.
2. Introduction to Aircraft Basic Science, Kroes, Michael J and
Rardon, JamesR”, 7th Edition, Macmillan / McGraw Hill, 1993.
3. Space Vehicle Design, 2nd Edition AIAA Education Series,
Michael D. Griffin, James R. French by Michael D.
4. Mechanics of Flight, (Revised by RH Bernard & DR Philpott),
Kermode, A.C., LPE, Pearson Education, 2005.
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
9
DYNAMICS OF MACHINES
Subject Code : 06AE53 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
STATIC FORCE ANALYSIS: Static force analysis: Introduction: Static
equilibrium. Equilibrium of two and three force members. Members with two
forces and torque, Free body diagrams, principle of virtual work. Static force
analysis of four bar mechanism and slider-crank mechanism with and without
friction.
6 Hours
UNIT – 2
DYNAMIC FORCE ANALYSIS: D’Alembert’s principle, Inertia force,
inertia torque, Dynamic force analysis of four-bar mechanism and slider
crank mechanism. Dynamically equivalent systems. Turning moment
diagrams and flywheels, Fluctuation of Energy. Determination of size of
flywheels.
8 Hours
UNIT – 3
FRICTION AND BELT DRIVES: Definitions: Types of friction: laws of
friction, Friction in pivot and collar bearings. Belt drives: Flat belt drives,
ratio of belt tensions, centrifugal tension, power transmitted.
6 Hours
UNIT – 4
BALANCING OF ROTATING MASSES: Static and dynamic balancing,
Balancing of single rotating mass by balancing masses in same plane and in
different planes. Balancing of several rotating masses by balancing masses in
same plane and in different planes.
6 Hours
PART – B
UNIT – 5
BALANCING OF RECIPROCATING MASSES: Inertia effect of crank
and connecting rod, single cylinder engine, balancing in multi cylinder-inline
V SEMESTER
MANAGEMENT & ENTREPRENEURSHIP
Subject Code : 06AL51 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART - A
MANAGEMENT
UNIT - 1
MANAGEMENT: Introduction - Meaning - nature and characteristics of
Management, Scope and functional areas of Management - Management as a
Science, Art or Profession Management & Administration - Roles of
Management, Levels of Management, Development of Management
Thought-Early Management Approaches-Modern Management Approaches.
7 Hours
UNIT - 2
PLANNING: Nature, importance and purpose of planning process -
Objectives - Types of plans (Meaning only) - Decision making - Importance
of planning - steps in planning & planning premises - Hierarchy of plans.
6 Hours
UNIT - 3
ORGANISING AND STAFFING: Nature and purpose of organization -
Principles of organization - Types of organization - Departmentation -
Committees – Centralisation Vs Decentralisation of authority and
responsibility - Span of control - MBO and MBE (Meaning only) Nature and
importance of Staffing - Process of Selection & Recruitment (in brief).
6 Hours
UNIT - 4
DIRECTING & CONTROLLING: Meaning and nature of directing -
Leadership styles, Motivation Theories, Communication - Meaning and
importance – Coordination, meaning and importance and Techniques of Co -
ordination. Meaning and steps in controlling - Essentials of a sound control
system - Methods of establishing control.
7 Hours
5
PART - B
ENTREPRENEURSHIP
UNIT - 5
ENTREPRENEUR: Meaning of Entrepreneur; Evolution of the Concept,
Functions of an Entrepreneur, Types of Entrepreneur, Intrapreneur - an
emerging Class. Concept of Entrepreneurship - Evolution of
Entrepreneurship, Development of Entrepreneurship; Stages in
entrepreneurial process; Role of entrepreneurs in Economic Development;
Entrepreneurship in India; Entrepreneurship – its Barriers.
6 Hours
UNIT - 6
SMALL SCALE INDUSTRY: Definition; Characteristics; Need and
rationale: Objectives; Scope; role of SSI in Economic Development.
Advantages of SSI Steps to start an SSI - Government policy towards SSI;
Different Policies of S.S.I.; Government Support for S.S.I. during 5 year
plans, Impact of Liberalization, Privatization, Globalization on S.S.I., Effect
of WTO/GATT Supporting Agencies of Government for S.S.I Meaning;
Nature of Support; Objectives; Functions; Types of Help; Ancillary Industry
and Tiny Industry (Definition only).
7 Hours
UNIT - 7
INSTITUTIONAL SUPPORT: Different Schemes; TECKSOK; KIADB;
KSSIDC; KSIMC; DIC Single Window Agency: SISI; NSIC; SIDBI; KSFC.
6 Hours
UNIT - 8
PREPARATION OF PROJECT: Meaning of Project; Project
Identification; Project Selection; Project Report; Need and Significance of
Report; Contents; formulation; Guidelines by Planning Commission for
Project report; Network Analysis; Errors of Project Report; Project
Appraisal. Identification of Business Opportunities - Market Feasibility
Study; Technical Feasibility Study; Financial Feasibility Study & Social
Feasibility Study.
7 Hours
TEXT BOOKS:
1. Principles of Management - P. C. Tripathi, P. N. Reddy; Tata
McGraw Hill.
2. Dynamics of Entrepreneurial Development & Management -
Vasant Desai Himalaya Publishing House.
3. Entrepreneurship Development - Small Business Enterprises -
Poornima M Charantimath - Pearson Education – 2006.
6
REFERENCE BOOKS:
1. Management Fundamentals - Concepts, Application, Skill
Development Robert Lusier – Thomson.
2. Entrepreneurship Development - S S Khanka - S Chand & Co.
3. Management - Stephen Robbins - Pearson Education /PHI -17th
Edition, 2003.
7
ELEMENTS OF AERONAUTICS
Subject Code : 06AE52 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART - A
UNIT – 1
HISTORICAL DEVELOPMENTS IN AEROSPACE: Early airplanes,
biplanes and monoplanes, Developments in aerodynamics, materials,
structures and propulsion over the years.
6 Hours
UNIT – 2
AIRCRAFT CONFIGURATIONS: Different types of flight vehicles and
classifications. Components of an airplane and their functions. Airfoils,
wings and other shapes.
6 Hours
UNIT – 3
PRINCIPLES OF ATMOSPHERIC FLIGHT: Physical properties and
structure of the atmosphere, The Standard Atmosphere, Temperature,
Pressure and Altitude relationships, Evolution of lift, drag and moment,
Airfoils, Mach number, Maneuvers, Concepts of stability and control.
8 Hours
UNIT – 4
INTRODUCTION TO SPACE FLIGHT: Introduction to basic concepts,
The upper atmosphere, Differential equations, Lagrange’s equation, Orbit
equation, Space vehicle trajectories-some basic concepts, Kepler’s Laws of
planetary motion.
6 Hours
PART - B
UNIT – 5
AIRCRAFT STRUCTURES AND AIRCRAFT MATERIALS: General
types of construction, Monocoque, semi-monocoque and geodesic
construction, typical wing and fuselage structure. Metallic and non-metallic
materials for aircraft application.
6 Hours
8
UNIT – 6
AIRCRAFT 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.
8 Hours
UNIT – 7
AIRCRAFT SYSTEMS: MECHANICAL: Description of different
airplane systems and their components: Hydraulics, Pneumatic, Oxygen
System, Environmental Control System, Fuel System.
6 Hours
UNIT – 8
AIRCRAFT SYSTEMS: ELECTRICAL: Flight Control System, Aircraft
Electrical System, Aircraft Instruments, Navigation System, Communication
System.
6 Hours
TEXT BOOKS:
1. Introduction to Flight, ,Anderson, J.D., McGraw-Hill, 1995.
2. Fundamentals of Flight Vol. IV Aircraft Systems, Lalit Gupta
and Dr. O. P. Sharma., Himalayan Books, 2006
REFERENCE:
1. Flight without Formulae, Kermode, A.C., McGraw-Hill, 1997.
2. Introduction to Aircraft Basic Science, Kroes, Michael J and
Rardon, JamesR”, 7th Edition, Macmillan / McGraw Hill, 1993.
3. Space Vehicle Design, 2nd Edition AIAA Education Series,
Michael D. Griffin, James R. French by Michael D.
4. Mechanics of Flight, (Revised by RH Bernard & DR Philpott),
Kermode, A.C., LPE, Pearson Education, 2005.
Scheme of Examination:
One Question to be set from each chapter. Students have to answer any FIVE
full questions out of EIGHT questions, choosing at least TWO questions
from Part A and TWO questions from Part B.
9
DYNAMICS OF MACHINES
Subject Code : 06AE53 IA Marks : 25
No. of Lecture Hrs/Week : 04 Exam Hours : 03
Total no. of Lecture Hrs. : 52 Exam Marks : 100
PART – A
UNIT – 1
STATIC FORCE ANALYSIS: Static force analysis: Introduction: Static
equilibrium. Equilibrium of two and three force members. Members with two
forces and torque, Free body diagrams, principle of virtual work. Static force
analysis of four bar mechanism and slider-crank mechanism with and without
friction.
6 Hours
UNIT – 2
DYNAMIC FORCE ANALYSIS: D’Alembert’s principle, Inertia force,
inertia torque, Dynamic force analysis of four-bar mechanism and slider
crank mechanism. Dynamically equivalent systems. Turning moment
diagrams and flywheels, Fluctuation of Energy. Determination of size of
flywheels.
8 Hours
UNIT – 3
FRICTION AND BELT DRIVES: Definitions: Types of friction: laws of
friction, Friction in pivot and collar bearings. Belt drives: Flat belt drives,
ratio of belt tensions, centrifugal tension, power transmitted.
6 Hours
UNIT – 4
BALANCING OF ROTATING MASSES: Static and dynamic balancing,
Balancing of single rotating mass by balancing masses in same plane and in
different planes. Balancing of several rotating masses by balancing masses in
same plane and in different planes.
6 Hours
PART – B
UNIT – 5
BALANCING OF RECIPROCATING MASSES: Inertia effect of crank
and connecting rod, single cylinder engine, balancing in multi cylinder-inline
aeronautical scheme and syllabus (vtu)
SCHEME OF TEACHING AND EXAMINATION
B.E. AERONAUTICAL ENGINEERING
V SEMESTER
Sl.
No Sub-Code Title Teachin
g Dept.
Teaching hours
/week Examination
Theory Pract
.
Duratio
n
I.A.
Marks
Theory
/ Pract.
Total
Marks
1 06AL51 Management and
Entrepreneurship @ 04 -- 03 25 100 125
2 06AE52 Elements of Aeronautics AE 04 -- 03 25 100 125
3 06AE53 Dynamics of Machines ME 04 -- 03 25 100 125
4 06AE54 Aerodynamics – I AE 04 -- 03 25 100 125
5 06AE55 Aircraft Propulsion AE 04 -- 03 25 100 125
6 06AE56 Aircraft Structures – I AE 04 -- 03 25 100 125
7 06AEL57 Structures Laboratory AE -- 03 03 25 50 75
8 06AEL58 Energy Conversion Lab AE/ME -- 03 03 25 50 75
TOTAL 24 06 24 200 700 900
Note: One question has to be set for every 6 to 8 hours of teaching.
@ - Indicates that teaching department can be any engineering department /
department of management studies
SCHEME OF TEACHING AND EXAMINATION
B.E. AERONAUTICAL ENGINEERING
VI SEMESTER
Sl.
No Sub-Code Title Teachin
g Dept.
Teaching hours
/week Examination
Theory Pract
.
Duratio
n
I.A.
Marks
Theory/
Pract.
Total
Marks
1 06AE61 Introduction to Composite
Materials ME/IEM 04 -- 03 25 100 125
2 06AE62 Aircraft Structures - II AE 04 -- 03 25 100 125
3 06AE63 Aerodynamics – II AE 04 -- 03 25 100 125
4 06AE64 Finite Element Analysis AE/ME 04 -- 03 25 100 125
5 06AE65 Theory of Vibrations ME 04 -- 03 25 100 125
6 06AE66* * Elective - I: (Group A) AE/IEM 04 -- 03 25 100 125
7 06AEL67 Aerodynamics Laboratory AE -- 03 03 25 50 75
8 06AEL68 Propulsion Laboratory AE -- 03 03 25 50 75
TOTAL 24 06 24 200 700 900
Note: One question has to be set for every 6 to 8 hours of teaching.
*ELECTIVE -1(Group A)
06AE661 Numerical Methods
06AE662 Aircraft Materials
06AE663 Combustion
06AE664 Reliability Engineering
06AE665 Industrial Management
* Students shall register for one subject from Group A Electives
B.E. AERONAUTICAL ENGINEERING
V SEMESTER
Sl.
No Sub-Code Title Teachin
g Dept.
Teaching hours
/week Examination
Theory Pract
.
Duratio
n
I.A.
Marks
Theory
/ Pract.
Total
Marks
1 06AL51 Management and
Entrepreneurship @ 04 -- 03 25 100 125
2 06AE52 Elements of Aeronautics AE 04 -- 03 25 100 125
3 06AE53 Dynamics of Machines ME 04 -- 03 25 100 125
4 06AE54 Aerodynamics – I AE 04 -- 03 25 100 125
5 06AE55 Aircraft Propulsion AE 04 -- 03 25 100 125
6 06AE56 Aircraft Structures – I AE 04 -- 03 25 100 125
7 06AEL57 Structures Laboratory AE -- 03 03 25 50 75
8 06AEL58 Energy Conversion Lab AE/ME -- 03 03 25 50 75
TOTAL 24 06 24 200 700 900
Note: One question has to be set for every 6 to 8 hours of teaching.
@ - Indicates that teaching department can be any engineering department /
department of management studies
SCHEME OF TEACHING AND EXAMINATION
B.E. AERONAUTICAL ENGINEERING
VI SEMESTER
Sl.
No Sub-Code Title Teachin
g Dept.
Teaching hours
/week Examination
Theory Pract
.
Duratio
n
I.A.
Marks
Theory/
Pract.
Total
Marks
1 06AE61 Introduction to Composite
Materials ME/IEM 04 -- 03 25 100 125
2 06AE62 Aircraft Structures - II AE 04 -- 03 25 100 125
3 06AE63 Aerodynamics – II AE 04 -- 03 25 100 125
4 06AE64 Finite Element Analysis AE/ME 04 -- 03 25 100 125
5 06AE65 Theory of Vibrations ME 04 -- 03 25 100 125
6 06AE66* * Elective - I: (Group A) AE/IEM 04 -- 03 25 100 125
7 06AEL67 Aerodynamics Laboratory AE -- 03 03 25 50 75
8 06AEL68 Propulsion Laboratory AE -- 03 03 25 50 75
TOTAL 24 06 24 200 700 900
Note: One question has to be set for every 6 to 8 hours of teaching.
*ELECTIVE -1(Group A)
06AE661 Numerical Methods
06AE662 Aircraft Materials
06AE663 Combustion
06AE664 Reliability Engineering
06AE665 Industrial Management
* Students shall register for one subject from Group A Electives
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