AERO 207 - Aerodynamics for Aircraft Structures

Description
The students will study the gas laws, standard atmosphere, Bernoulli theorem, total and static pressures, true air speed (TAS), indicated air speed (IAS), aero-foils, lift and drag, wings and flaps. Lift and drag coefficients, induced drag, minimum drag and power, gliding, endurance, climb, maneuvers, stability and control, and load factor will also be studied.

1.5 Credits

Time Guidelines
The standard instructional time for this course is 30 hours.