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.
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Prerequisite:
None
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Corequisite:
None
| Class Hours | 3 |
|---|---|
| Lab Hours | – |
| Clinic, Coop, or Shop Hours | – |
| Credit Hours | 3 |