AE2251 AERODYNAMICS – I SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 4TH SEM SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY FOURTH SEMESTER BE AERONAUTICAL ENGINEERING DEPARTMENT SYLLABUS, TEXTBOOKS, REFERENCE BOOKS,EXAM PORTIONS,QUESTION BANK,PREVIOUS YEAR QUESTION PAPERS,MODEL QUESTION PAPERS, CLASS NOTES, IMPORTANT 2 MARKS, 8 MARKS, 16 MARKS TOPICS. IT IS APPLICABLE FOR ALL STUDENTS ADMITTED IN THE YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI,TRICHY,MADURAI,TIRUNELVELI,COIMBATORE), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AE2251 AERODYNAMICS – I L T P C
3 0 0 3
OBJECTIVE
To understand the behaviour of airflow over bodies with particular emphasis on airfoil
sections in the incompressible flow regime.
UNIT I REVIEW OF BASIC FLUID MECHANICS 4
Continuity, momentum and energy equations.
UNIT II 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.
UNIT III GENERATION OF LIFT 8
Kutta Joukowski’s theorem. Kutta condition. Blasius theorem.
UNIT IV 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.
UNIT V 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 PERIODS
TEXT BOOKS
1. Anderson, J.D., “Fundamentals of Aerodynamics”, McGraw-Hill Book Co., New York,
1998.
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
AE2251 AERODYNAMICS – I L T P C
3 0 0 3
OBJECTIVE
To understand the behaviour of airflow over bodies with particular emphasis on airfoil
sections in the incompressible flow regime.
UNIT I REVIEW OF BASIC FLUID MECHANICS 4
Continuity, momentum and energy equations.
UNIT II 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.
UNIT III GENERATION OF LIFT 8
Kutta Joukowski’s theorem. Kutta condition. Blasius theorem.
UNIT IV 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.
UNIT V 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 PERIODS
TEXT BOOKS
1. Anderson, J.D., “Fundamentals of Aerodynamics”, McGraw-Hill Book Co., New York,
1998.
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
Any doubt ??? Just throw it Here...