AE6401 - AERODYNAMICS - I (Syllabus) 2013-regulation Anna University
AE6401 - AERODYNAMICS - I (Syllabus) 2013-regulation Anna University
AE6401 |
AERODYNAMICS - I |
LPTC |
---|
3003
OBJECTIVES:
• To introduce the concepts of mass, momentum and energy conservation relating to aerodynamics.
• To make the student understand the concept of vorticity, irrotationality, theory of airfoils and wing sections.
• To introduce the basics of viscous flow.
• To make the student understand the concept of vorticity, irrotationality, theory of airfoils and wing sections.
• To introduce the basics of viscous flow.
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.
TOTAL : 45 PERIODS
OUTCOMES:
• An ability to apply airfoil theory to predict air foil perform
• A knowledge of incompressible flow
• An explosive to Boundary layer theory
• A knowledge of incompressible flow
• An explosive to Boundary layer theory
TEXT BOOKS:
1. Houghton, E.L., and Caruthers, N.B., "Aerodynamics for Engineering students", Edward Arnold Publishers Ltd., London, 1989.
2. Anderson, J.D., "Fundamentals of Aerodynamics", MaGraw Hill Book Co., 1999
2. Anderson, J.D., "Fundamentals of Aerodynamics", MaGraw Hill Book Co., 1999
REFERENCES
1. Milne Thomson, L.H., "Theoretical Aerodynamics", Macmillan, 1985
2. John J Bertin., "Aerodynamics for Engineers", Pearson Education Inc, 2002
3. Clancey, L J.," Aerodynamics", Pitman, 1986
4. Kuethe, A.M and Chow, C.Y, “Foundations of Aerodynamics”, Fifth Edition, John Wiley & Sons, 2000.
2. John J Bertin., "Aerodynamics for Engineers", Pearson Education Inc, 2002
3. Clancey, L J.," Aerodynamics", Pitman, 1986
4. Kuethe, A.M and Chow, C.Y, “Foundations of Aerodynamics”, Fifth Edition, John Wiley & Sons, 2000.
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