MAE 473 Applied Aerodynamics
Properties of the atmosphere. Aerodynamic coefficients and their dependence on Reynolds number and Mach number. Aerodynamics of airfoils, wings, and complete aircraft. Performance analysis of aerospace vehicles in atmospheric flight: range, endurance, climb, descent, takeoff, and landing. Prerequisites:
ES 223,
MAE 3033 and
MAE 323
Lab Hours
0
Lecture Hours
3
Prerequisite
ES 223, MAE 3033 and MAE 323