AVT 2247 Aerodynamics & Flight Mechanics
3.0 Credit Hours
Properties of the Standard Atmosphere. Applies basic physics conservation concepts to incompressible, low-speed aerodynamics to develop analytical equations for lift and drag. Develops methods for basic aircraft performance analysis to include maximum angle and rate of climb, cruise and gliding flight. Discusses basic static and dynamic stability requirements.
Prerequisite: PHY 1141
|(* indicates prerequisite)||(updated hourly)|
|Independent Study Student|