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AE6401 Aerodynamics - I -Semester IV-AERO-BE-Anna University

ae6401-aerodynamics-i-semester-iv-aero-be-anna-universityAE6401 Aerodynamics - I -Semester IV-AERO-BE-Anna University 
AERO SEM IV Syllabus, AERO SYLLABUS

 
 
 
 
 
AE6401                                             AERODYNAMICS - I                                                     L  T  P  C
3 0  0   3
OBJECTIVES:
<ul>
<li>To introduce  the  concepts  of  mass,  momentum  and  energy  conservation  relating  to aerodynamics.</li>
<li>To make the student understand the concept of vorticity, irrotationality, theory of airfoils and wing sections.</li>
<li>To introduce the basics of viscous flow.</li>
</ul>
 
UNIT I             INTRODUCTION TO LOW SPEED FLOW                                                                     9
Euler  equation,  incompressible  bernoulli’s  equation.  circulation  and  vorticity,  green’s  lemma  and stoke’s theorem, barotropic flow, kelvin’s theorem, streamline, stream function, irrotational flow, potential function, equipontential lines, elementary flows and their combinations.
 
UNIT II            TWO DIMENSIONAL INVISCID INCOMPRESSIBLE FLOW                                        9
Ideal Flow over a circular cylinder, D’Alembert’s paradox, magnus effect, Kutta joukowski’s theorem, starting vortex, kutta condition,  real flow over smooth and rough cylinder.
 
UNIT III           AIRFOIL THEORY                                                                                                          9
Cauchy-riemann relations, complex potential, methodology of conformal transformation, kutta- joukowski transformation and its applications, thin airfoil theory and its applications.
 
UNIT IV          SUBSONIC WING THEORY                                                                                           9
Vortex filament, biot and savart law, bound vortex and trailing vortex, horse shoe vortex, lifting line theory and its limitations.
 
UNIT V           INTRODUCTION TO BOUNDARY LAYER THEORY                                                    9
Boundary layer and boundary layer thickness, displacement thickness, momentum thickness, energy thickness, shape parameter, boundary layer equations for a steady, two dimensional incompressible flow, boundary layer growth over a flat plate, critical reynolds number, blasius solution, basics of turbulent flow.
 
 
OUTCOMES
<ul>
<li>An ability to apply airfoil theory to predict air foil perform</li>
<li>A knowledge of incompressible flow</li>
<li>An explosive to Boundary layer theory</li>
</ul>
 
TOTAL: 45 PERIODS
 
 
TEXT BOOKS:
<ol>
<li>Houghton, E.L., and Caruthers, N.B., "Aerodynamics for Engineering students", Edward Arnold</li>
</ol>
Publishers Ltd., London, 1989.
<ol start="2">
<li>Anderson, J.D., "Fundamentals of Aerodynamics", MaGraw Hill Book Co., 1999</li>
</ol>
 
REFERENCES:
<ol>
<li>Milne Thomson, L.H., "Theoretical Aerodynamics", Macmillan, 1985</li>
<li>John J Bertin., "Aerodynamics for Engineers", Pearson Education Inc, 2002</li>
<li>Clancey, L J.," Aerodynamics", Pitman, 1986</li>
<li>Kuethe, A.M and Chow, C.Y, “Foundations of Aerodynamics”, Fifth Edition, John Wiley & Sons,</li>
</ol>
2000.

AERO SEM IV Syllabus AERO SYLLABUS AE6401 Aerodynamics - I -Semester IV-AERO-BE-Anna University

ae6401-aerodynamics-i-semester-iv-aero-be-anna-universityAE6401 Aerodynamics - I -Semester IV-AERO-BE-Anna University AERO SEM IV Syllabus, AERO SYLLABUS AE6401 AERODYNAMICS - I …

MA6459 Numerical Methods -Semester IV-AERO-BE-Anna University

ma6459-numerical-methods-semester-iv-aero-be-anna-universityMA6459 Numerical Methods -Semester IV-AERO-BE-Anna University 
AERO SEM IV Syllabus, AERO SYLLABUS

 
 
 
 
 
MA6459                                         NUMERICAL  METHODS                                                  L  T  P  C
3 1  0   4
OBJECTIVES
<ul>
<li>This course aims at providing the necessary basic concepts of a few numerical methods and give procedures for solving numerically different kinds of problems occurring in engineering and technology</li>
</ul>
 
UNIT I             SOLUTION OF EQUATIONS AND EIGENVALUE PROBLEMS                             10+3
Solution of algebraic and transcendental equations - Fixed point iteration method – Newton Raphson method- Solution of linear system of equations - Gauss elimination method – Pivoting - Gauss Jordan method – Iterative methods of Gauss Jacobi and Gauss Seidel - Matrix Inversion by Gauss Jordan method - Eigenvalues of a matrix by Power method.
 
UNIT II            INTERPOLATION  AND  APPROXIMATION                                                             8+3
Interpolation with unequal intervals - Lagrange's interpolation – Newton’s divided difference interpolation – Cubic Splines - Interpolation with equal intervals - Newton’s forward and backward difference formulae.
 
UNIT III           NUMERICAL  DIFFERENTIATION  AND  INTEGRATION                                        9+3
Approximation   of   derivatives   using   interpolation   polynomials   -   Numerical   integration   using Trapezoidal,  Simpson’s  1/3  rule  –  Romberg’s  method  -  Two  point  and  three  point  Gaussian quadrature formulae – Evaluation of double integrals by Trapezoidal and Simpson’s 1/3 rules.
 
UNIT IV           INITIAL  VALUE  PROBLEMS  FOR  ORDINARY  DIFFERENTIAL
EQUATIONS                                                                                                              9+3
Single Step methods - Taylor’s series method - Euler’s method - Modified Euler’s method - Fourth order Runge-Kutta method for solving first order equations - Multi step methods - Milne’s and Adams- Bashforth predictor corrector methods for solving first order equations.
 
UNIT V           BOUNDARY  VALUE  PROBLEMS IN ORDINARY  AND  PARTIAL
DIFFERENTIAL  EQUATIONS                                                                                   9+3
Finite difference methods for solving two-point linear boundary value problems - Finite difference techniques for the solution of two dimensional Laplace’s and Poisson’s equations on rectangular domain – One dimensional heat flow equation by explicit and implicit (Crank Nicholson) methods – One dimensional wave equation by explicit method.
 
 
OUTCOMES
 
TOTAL (L:45+T:15): 60 PERIODS
 
<ul>
<li>The students will have a clear perception of the power of numerical techniques, ideas and would be able to demonstrate the applications of these techniques to problems drawn from industry, management and other engineering fields.</li>
</ul>
 
TEXT BOOKS
<ol>
<li>Grewal. B.S., and Grewal. J.S., " Numerical  methods  in  Engineering  and  Science", Khanna</li>
</ol>
Publishers, New Delhi, 9th Edition, 2007.
<ol start="2">
<li>Gerald. C. F., and Wheatley. P. O., " Applied  Numerical  Analysis", Pearson Education, Asia, New Delhi, 6th Edition, 2006.</li>
</ol>
 
REFERENCES
<ol>
<li>Chapra.  S.C.,   and   Canale.R.P.,   "Numerical   Methods   for   Engineers,   5th     Edition,   Tata</li>
</ol>
McGraw - Hill, New Delhi, 2007.
<ol start="2">
<li>Brian Bradie. "A friendly introduction to Numerical analysis", Pearson Education, Asia, New Delhi,</li>
</ol>
2007.
<ol start="3">
<li>Sankara Rao. K., "Numerical methods for Scientists and Engineers", 3rd Edition, Prentice Hall of</li>
</ol>
India Private Ltd., New Delhi, 2007.

AERO SEM IV Syllabus AERO SYLLABUS MA6459 Numerical Methods -Semester IV-AERO-BE-Anna University

ma6459-numerical-methods-semester-iv-aero-be-anna-universityMA6459 Numerical Methods -Semester IV-AERO-BE-Anna University AERO SEM IV Syllabus, AERO SYLLABUS MA6459 NUMERICAL METHODS …

AE6312 CAM and Manufacturing Laboratory -Semester III-AERO-BE-Anna University

ae6312-cam-and-manufacturing-laboratory-semester-iii-aero-be-anna-universityAE6312 CAM and Manufacturing Laboratory -Semester III-AERO-BE-Anna University 
AERO SEM III Syllabus, AERO SYLLABUS

 
 
AE6312                         CAM AND MANUFACTURING LABORATORY                             L  T   P  C
0   0 3   2
OBJECTIVES
<ul>
<li>To teach and train the students in the lab about the design and drafting of aero components</li>
</ul>
 
LIST OF EXPERIMENTS
<ol>
<li>Design and modeling of rectangular plate with hole.</li>
<li>Design and modeling of spar components.</li>
<li>Design and modeling of aerofoil sections.</li>
<li>Design and modeling of cut section for wings.</li>
<li>Design and modeling of machine component.</li>
<li>Design and modeling of bulk head.</li>
<li>Design and analysis of a truss.</li>
<li>Design and analysis of beam distributed load.</li>
<li>Facing and Turning (Taper, Step) operations in CNC.</li>
<li>Drilling operations in CNC.</li>
</ol>
 
OUTCOMES
 
 
 
 
 
 
 
 
 
 
 
 
 
 
 
TOTAL: 45 PERIODS
 
Ability to design and model difficult aero component and perform structural analysis using available software packages
 
LIST OF EQUIPMENTS FOR A BATCH OF 30 STUDENTS
<table>
<tbody>
<tr>
<td width="63">
Sl.No.
</td>
<td width="244">
Name of the Equipment
</td>
<td width="110">
Quantity
</td>
<td width="161">
Experiment No.
</td>
</tr>
<tr>
<td width="63">
1
</td>
<td width="244">
Computer nodes
</td>
<td width="110">
30
</td>
<td width="161">
1 to 8
</td>
</tr>
<tr>
<td width="63">
2
</td>
<td width="244">
Modeling Packages
</td>
<td width="110">
30 licenses
</td>
<td width="161">
1 to 6
</td>
</tr>
<tr>
<td width="63">
3
</td>
<td width="244">
FEA&CAM SOFTWARE
</td>
<td width="110">
30 licenses
</td>
<td width="161">
7 & 8
</td>
</tr>
<tr>
<td width="63">
4
</td>
<td width="244">
UPS
</td>
<td width="110">
1
</td>
<td width="161">
1 to 8
</td>
</tr>
<tr>
<td width="63">
5.
</td>
<td width="244">
CNC Machine
</td>
<td width="110">
1
</td>
<td width="161">
9,10
</td>
</tr>
<tr>
<td width="63">
5
</td>
<td width="244">
Printer
</td>
<td width="110">
2
</td>
<td width="161">
All
</td>
</tr>
</tbody>
</table>

AERO SEM III Syllabus AERO SYLLABUS AE6312 CAM and Manufacturing Laboratory -Semester III-AERO-BE-Anna University

AE6311 Thermodynamics Laboratory -Semester III-AERO-BE-Anna University

ae6311-thermodynamics-laboratory-semester-iii-aero-be-anna-universityAE6311 Thermodynamics Laboratory -Semester III-AERO-BE-Anna University 
AERO SEM III Syllabus, AERO SYLLABUS

 
 
 
AE6311                                THERMODYNAMICS LABORATORY                                            L  T P  C
0   0 3  2
OBJECTIVES
<ul>
<li>To enhance the basic knowledge in applied thermodynamics</li>
</ul>
 
LIST OF EXPERIMENTS
<table>
<tbody>
<tr>
<td width="37">
1.
</td>
<td width="478">
Performance test on a 4-stroke engine
</td>
<td rowspan="10" width="152">
 
</td>
</tr>
<tr>
<td width="37">
2.
</td>
<td width="478">
Valve timing of a 4 – stroke engine and port timing of a 2 stroke engine
</td>
</tr>
<tr>
<td width="37">
3.
</td>
<td width="478">
Determination of effectiveness of a parallel flow heat exchanger
</td>
</tr>
<tr>
<td width="37">
4.
</td>
<td width="478">
Determination of effectiveness of a counter flow heat exchanger
</td>
</tr>
<tr>
<td width="37">
5.
</td>
<td width="478">
Determination of heating value of a fuel
</td>
</tr>
<tr>
<td width="37">
6.
</td>
<td width="478">
Determination of specific heat of solid
</td>
</tr>
<tr>
<td width="37">
7.
</td>
<td width="478">
Determination of thermal conductivity of solid.
</td>
</tr>
<tr>
<td width="37">
8.
</td>
<td width="478">
Determination of thermal resistance of a composite wall.
</td>
</tr>
<tr>
<td width="37">
9.
</td>
<td width="478">
COP test on a vapour compression refrigeration test rig
</td>
</tr>
<tr>
<td width="37">
10.
</td>
<td width="478">
COP test on a vapour compression air-conditioning test rig
</td>
</tr>
<tr>
<td width="37">
 
</td>
<td width="478">
 
</td>
<td width="152">
TOTAL: 45 PERIODS
</td>
</tr>
</tbody>
</table>
OUTCOMES
<ul>
<li>Ability to perform test on diesel/petrol engine</li>
<li>Ability to explain the characteristics of the diesel/Petrol engine</li>
<li>Ability to determine the properties of the fuels.</li>
</ul>
 
LIST OF EQUIPMENT FOR A BATCH OF 30 STUDENTS
 
<table>
<tbody>
<tr>
<td width="55">
 
Sl.No
</td>
<td width="349">
 
Details of Equipments
</td>
<td width="62">
Qty
Req.
</td>
<td width="102">
Experiment
No.
</td>
</tr>
<tr>
<td width="55">
1.
</td>
<td width="349">
4 stroke twin cylinder diesel engine
</td>
<td width="62">
1
</td>
<td width="102">
1
</td>
</tr>
<tr>
<td width="55">
2.
</td>
<td width="349">
Cut section model of 4 stroke diesel engine and cut section model of 2 stroke petrol engine
</td>
<td width="62">
1
</td>
<td width="102">
2
</td>
</tr>
<tr>
<td width="55">
3.
</td>
<td width="349">
Parallel and counter flow heat exchanger test rig
</td>
<td width="62">
1
</td>
<td width="102">
3,4
</td>
</tr>
<tr>
<td width="55">
4.
</td>
<td width="349">
Bomb Calorimeter
</td>
<td width="62">
1
</td>
<td width="102">
5
</td>
</tr>
<tr>
<td width="55">
5.
</td>
<td width="349">
Vapour compression refrigeration test rig
</td>
<td width="62">
1
</td>
<td width="102">
9
</td>
</tr>
<tr>
<td width="55">
6.
</td>
<td width="349">
Vapour compression air-conditioning test rig
</td>
<td width="62">
1
</td>
<td width="102">
10
</td>
</tr>
<tr>
<td width="55">
7.
</td>
<td width="349">
Conductive heat transfer set up
</td>
<td width="62">
1
</td>
<td width="102">
7
</td>
</tr>
<tr>
<td width="55">
8.
</td>
<td width="349">
Composite wall
</td>
<td width="62">
1
</td>
<td width="102">
8
</td>
</tr>
</tbody>
</table>

AERO SEM III Syllabus AERO SYLLABUS AE6311 Thermodynamics Laboratory -Semester III-AERO-BE-Anna University

CE6461 Fluid Mechanics and Machinery Laboratory -Semester III-AERO-BE-Anna University

ce6461-fluid-mechanics-and-machinery-laboratory-semester-iii-aero-be-anna-universityCE6461 Fluid Mechanics and Machinery Laboratory -Semester III-AERO-BE-Anna University 
AERO SEM III Syllabus, AERO SYLLABUS

 
 
 
 
 
 
 
CE6461                  FLUID MECHANICS AND MACHINERY LABORATORY                      L  T  P  C
0  0 3  2
OBJECTIVES:
Upon Completion of this subject, the students can able to have hands on experience in flow measurements using different devices and also perform calculation related to losses in pipes and also perform characteristic study of pumps, turbines etc.,
 
LIST OF EXPERIMENTS
<ol>
<li>Determination of the Coefficient of discharge of given Orifice meter.</li>
<li>Determination of the Coefficient of discharge of given Venturi meter.</li>
<li>Calculation of the rate of flow using Rota meter.</li>
<li>Determination of friction factor for a given set of pipes.</li>
<li>Conducting experiments and drawing the characteristic curves of centrifugal pump/ submergible pump</li>
<li>Conducting experiments and drawing the characteristic curves of reciprocating pump.</li>
<li>Conducting experiments and drawing the characteristic curves of Gear pump.</li>
<li>Conducting experiments and drawing the characteristic curves of Pelton wheel.</li>
<li>Conducting experiments and drawing the characteristics curves of Francis turbine.</li>
<li>Conducting experiments and drawing the characteristic curves of Kaplan turbine.</li>
</ol>
TOTAL: 45 PERIODS
OUTCOMES:
<ul>
<li>Ability to use the measurement equipments for flow measurement</li>
<li>Ability to do performance trust on different fluid machinery</li>
</ul>
 
<table>
<tbody>
<tr>
<td width="552">
<table width="100%">
<tbody>
<tr>
<td>
<table>
<tbody>
<tr>
<td width="64">
S. No.
</td>
<td width="375">
NAME OF THE EQUIPMENT
</td>
<td width="108">
Qty.
</td>
</tr>
<tr>
<td width="64">
1
</td>
<td width="375">
Orifice meter setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
2
</td>
<td width="375">
Venturi meter setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
3
</td>
<td width="375">
Rotameter setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
4
</td>
<td width="375">
Pipe Flow analysis setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
5
</td>
<td width="375">
Centrifugal pump/submergible pump setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
6
</td>
<td width="375">
Reciprocating pump setup
</td>
<td width="108">
1
</td>
</tr>
</tbody>
</table>
 
</td>
</tr>
</tbody>
</table>
 </td>
</tr>
</tbody>
</table>
LIST OF EQUIPMENT  FOR BATCH OF 30 STUDENTS
 
 
<table>
<tbody>
<tr>
<td width="64">
7
</td>
<td width="375">
Gear pump setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
8
</td>
<td width="375">
Pelton wheel setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
9
</td>
<td width="375">
Francis turbine setup
</td>
<td width="108">
1
</td>
</tr>
<tr>
<td width="64">
10
</td>
<td width="375">
Kaplan turbine setup
</td>
<td width="108">
1
</td>
</tr>
</tbody>
</table>

AERO SEM III Syllabus AERO SYLLABUS CE6461 Fluid Mechanics and Machinery Laboratory -Semester III-AERO-BE-Anna University

CE6315 Strength of Materials Laboratory -Semester III-AERO-BE-Anna University

ce6315-strength-of-materials-laboratory-semester-iii-aero-be-anna-universityCE6315 Strength of Materials Laboratory -Semester III-AERO-BE-Anna University 
AERO SEM III Syllabus, AERO SYLLABUS

 
 
 
 
CE6315                         STRENGTH OF MATERIALS LABORATORY                                 L T  P  C
0 0  3 2
OBJECTIVES
To supplement the theoretical knowledge gained in Mechanics of Solids with practical testing for determining the strength of materials under externally applied loads. This would enable the student to have a clear understanding of the design for strength and stiffness
 
LIST OF EXPERIMENTS
<ol>
<li>Tension test on a mild steel rod</li>
<li>Double shear test on Mild steel and Aluminium rods</li>
<li>Torsion test on mild steel rod</li>
<li>Impact test on metal specimen</li>
<li>Hardness test on metals - Brinnell and Rockwell Hardness Number</li>
<li>Deflection test on beams</li>
<li>Compression test on helical springs</li>
<li>Strain Measurement using Rosette strain gauge</li>
<li>Effect of hardening- Improvement in hardness and impact resistance of steels.</li>
<li>Tempering- Improvement Mechanical properties Comparison</li>
</ol>
(i) Unhardened specimen
(ii) Quenched Specimen and
(iii) Quenched and tempered specimen.
<ol start="11">
<li>Microscopic Examination of</li>
</ol>
(i) Hardened samples and
(ii) Hardened and tempered samples.
 
 
OUTCOMES:
<ul>
<li>Ability to perform different destructive testing</li>
<li>Ability to characteristic materials</li>
</ul>
 
TOTAL: 45 PERIODS
 
LIST OF EQUIPMENT FOR BATCH OF 30 STUDENTS
 
<table>
<tbody>
<tr>
<td width="64">
S.No.
</td>
<td width="463">
NAME OF THE EQUIPMENT
</td>
<td width="89">
Qty.
</td>
</tr>
<tr>
<td width="64">
1
</td>
<td width="463">
Universal Tensile Testing machine with double 1 shear attachment –
40 Ton Capacity
</td>
<td width="89">
1
</td>
</tr>
<tr>
<td width="64">
2
</td>
<td width="463">
Torsion Testing Machine (60 NM Capacity)
</td>
<td width="89">
1
</td>
</tr>
<tr>
<td width="64">
3
</td>
<td width="463">
Impact Testing Machine (300 J Capacity)
</td>
<td width="89">
1
</td>
</tr>
<tr>
<td width="64">
4
</td>
<td width="463">
Brinell Hardness Testing Machine
</td>
<td width="89">
1
</td>
</tr>
<tr>
<td width="64">
5
</td>
<td width="463">
Rockwell Hardness Testing Machine
</td>
<td width="89">
1
</td>
</tr>
<tr>
<td width="64">
6
</td>
<td width="463">
Spring Testing Machine for tensile and compressive loads (2500 N)
</td>
<td width="89">
1
</td>
</tr>
<tr>
<td width="64">
7
</td>
<td width="463">
Metallurgical Microscopes
</td>
<td width="89">
3
</td>
</tr>
<tr>
<td width="64">
8
</td>
<td width="463">
Muffle Furnace (800 C)
</td>
<td width="89">
1
</td>
</tr>
</tbody>
</table>

AERO SEM III Syllabus AERO SYLLABUS CE6315 Strength of Materials Laboratory -Semester III-AERO-BE-Anna University

AE6302 Elements of Aeronautics -Semester III-AERO-BE-Anna University

ae6302-elements-of-aeronautics-semester-iii-aero-be-anna-universityAE6302 Elements of Aeronautics -Semester III-AERO-BE-Anna University 
AERO SEM III Syllabus, AERO SYLLABUS

 
 
 
AE6302                                       ELEMENTS OF AERONAUTICS                                          L  T  P  C
3 0  0 3
OBJECTIVES:
<ul>
<li>To introduce the concepts of flying, International standard atmosphere, structural aspects of airplanes, brief description of systems, instruments and power plants used in airplanes.</li>
</ul>
 
UNIT I             HISTORY OF FLIGHT                                                                                                    8
Balloon flight – ornithopters - early airplanes by wright brothers, biplanes and monoplanes, developments in aerodynamics, materials, structures and propulsion over the years.
 
UNIT II            BASICS OF FLIGHT MECHANICS                                                                               9
Physical properties and structure of the atmosphere, temperature, pressure and altitude relationships, newton’s law of motions applied to aeronautics - evolution of lift, drag and moment. aerofoils, mach number, maneuvers.
 
UNIT III           AIRCRAFT CONFIGURATIONS                                                                                  10
Different types of flight vehicles, classifications. components of an airplane and their functions. conventional control, powered control, basic instruments for flying - typical systems for control actuation.
 
UNIT IV          AIRPLANE STRUCTURES AND MATERIALS                                                              9
General types of construction, monocoque, semi-monocoque and geodesic constructions, typical wing and fuselage structure. metallic and non-metallic materials, use of aluminium alloy, titanium, stainless steel and composite materials. stresses and strains –  hooke’s law – stress - strain diagrams -  elastic constants.
 
UNIT V           POWER PLANTS                                                                                                           9
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.
 
 
OUTCOMES
<ul>
<li>Identify the component of Flight</li>
<li>Identify suitable materials for Aircraft structure</li>
</ul>
 
TOTAL: 45 PERIODS
 
<ul>
<li>Perform basic calculation on Mechanics using Newton law for lift, drag and moment.</li>
</ul>
 
TEXT BOOKS:
<ol>
<li>Anderson, J.D., “Introduction to Flight”, McGraw-Hill, 1995.</li>
<li>Stephen. A. Brandt, "Introduction to Aeronautics: A design perspective" American Institute of</li>
</ol>
Aeronautics & Astronautics,1997
 
REFERENCES:
<ol>
<li>Kermode, A.C., “Mechanics of Flight”, Himalayan Book, 1997</li>
</ol>

AERO SEM III Syllabus AERO SYLLABUS AE6302 Elements of Aeronautics -Semester III-AERO-BE-Anna University

ANNA UNIVERSITY | SYLLABUS | UNIVERSITY QUESTION PAPER | NOTES

AE6401 Aerodynamics - I -Semester IV-AERO-BE-Anna University

MA6459 Numerical Methods -Semester IV-AERO-BE-Anna University

AE6312 CAM and Manufacturing Laboratory -Semester III-AERO-BE-Anna University

AE6311 Thermodynamics Laboratory -Semester III-AERO-BE-Anna University

CE6461 Fluid Mechanics and Machinery Laboratory -Semester III-AERO-BE-Anna University

CE6315 Strength of Materials Laboratory -Semester III-AERO-BE-Anna University

AE6302 Elements of Aeronautics -Semester III-AERO-BE-Anna University

CE6452 Solid Mechanics -Semester III-AERO-BE-Anna University

AE6401 Aerodynamics - I -Semester IV-AERO-BE-Anna University

MA6459 Numerical Methods -Semester IV-AERO-BE-Anna University

AE6312 CAM and Manufacturing Laboratory -Semester III-AERO-BE-Anna University

AE6311 Thermodynamics Laboratory -Semester III-AERO-BE-Anna University

CE6461 Fluid Mechanics and Machinery Laboratory -Semester III-AERO-BE-Anna University

CE6315 Strength of Materials Laboratory -Semester III-AERO-BE-Anna University

AE6302 Elements of Aeronautics -Semester III-AERO-BE-Anna University

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