MAE 3220 - Aerodynamics

Effective Date 05/01/2023
Boundary layers: similarity, Blasius and momentum integral methods. Ideal Flows: Kelvin’s circulation theorem; complex potential; superposition; Kutta-Joukowski; thin airfoils; finite wings; lifting lines. Gas dynamics: sound waves; normal and oblique shocks; Prandtl-Meyer expansion; quasi 1D flows; converging-diverging nozzles; choked flows; diffusers; Rayleigh line and Fanno line flows. Prerequisites: MAE 2100 and MAE 3210

Requisites Must have completed MAE 3210 and MAE 2100

Credits: 4