Undergraduate Catalog

AERO 336 Aerodynamics II

Introduction to compressible flows. Compressibility effects on airfoil and wing aerodynamics. Normal Shock Waves. Oblique Shock and Expansion Waves. Compressible Flow through Nozzles, Diffusers, and Wind Tunnels. Subsonic Compressible Flow over Airfoils: Linear Theory, Linearized Supersonic Flow. Elements of Hypersonic Flow.

Credits

3

Prerequisite

AERO 240, AERO 335

Offered

Fall Spring