Flight Dynamics


AER-210

This course covers basic and advanced principles of aerodynamic phenomena and fluid flow. Topics include airflow phenomena; lift/weight/thrust/drag; aircraft configuration characteristics, stability, and control; subsonic, transonic, and supersonic flight; critical Mach numbers; and the V-g Diagram. Upon completion, students should be able to explain the elements of applied aerodynamics and aeronautical engineering which relate directly to the problems of flight operations.

  • Prerequisite:
    None
  • Corequisite:
    None
Class Hours 3
Lab Hours
Clinic, Coop, or Shop Hours
Credit Hours 3