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MECH 581 Low Speed Aerodynamics
Circulation, vorticity and Kelvin's Theorem. Potential flow theory and the Kutta-Joukowski Law 2D Vortex Panel. Method. Laminar and turbulent boundary layer computations. Lifting line theory. Vortex Lattice Method. High lift devices. Total airplane drag. Credit cannot be obtained for both MECH 581 and MECH 481.
- This course is restricted to students in one of these faculties: GRAD
- Choose one section from all 2 activity types. (e.g. Lecture and Laboratory)
|Status||Section||Activity||Term||Interval||Days||Start Time||End Time||Comments|
|MECH 581 101||Lecture||1||Mon Wed||13:00||14:00|
|Blocked||MECH 581 L1A||Laboratory||1||Fri||13:00||14:00|