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

Credits

3

Lab Hours

0

Lecture Hours

3

Prerequisite

ES 223, MAE 3033 and MAE 323