AE2251 AERODYNAMICS – I SYLLABUS 3 0 0 3
OBJECTIVE
To understand the behaviour of airflow over bodies with particular emphasis on airfoil
sections in the incompressible flow regime.
1. REVIEW OF BASIC FLUID MECHANICS 4
Continuity, momentum and energy equations.
2. TWO DIMENSIONAL FLOWS 12
Basic flows – Source, Sink, Free and Forced vortex, uniform parallel flow. Their
combinations, Pressure and velocity distributions on bodies with and without circulation
in ideal and real fluid flows.
3. GENERATION OF LIFT 8
Kutta Joukowski’s theorem. Kutta condition. Blasius theorem.
4. AIRFOIL AND WING THEORY 12
Joukowski, Karman - Trefftz, Profiles - Thin aerofoil theory and its applications. Vortex
line, Horse shoe vortex, Biot and Savart law, Lifting line theory and its limitations.
5. VISCOUS FLOW 9
Newton’s law of viscosity, Boundary Layer, Navier-Stokes equation, displacement,
Momentum thickness, Flow over a flat plate, Blasins solution.
TOTAL : 45
TEXT BOOKS
1. Anderson, J.D., “Fundamentals of Aerodynamics”, McGraw-Hill Book Co., New
York, 1998. (VISIT http://aimforhigh.blogspot.com)
REFERENCES
1. Houghton, E.L., and Carruthers, N.B., “Aerodynamics for Engineering students”,
Edward Arnold Publishers Ltd., London, 1989.
2. Milne Thomson, L.H., “Theoretical aerodynamics”, Macmillan, 1985.
3. Clancey, L.J., “Aerodynamics”, Pitman, 1986
No comments:
Post a Comment
HI FRIENDS FEEL FREE TO COMMENT IN THIS BLOG