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AER 722
Aeroelasticity
Wing divergence. Control surface effectiveness. Flexibility effects on aircraft stability and control. Quasi-Steady and unsteady aerodynamics. Flutter analysis of two-dimensional wings with discussion of three-dimensional effects. Introduction of other aeroelastic phenomena such as stall flutter and buffeting. Prevention of aeroelastic instabilities. Flight flutter testing.
Weekly Contact: Lecture: 3 hrs.
GPA Weight: 1.00
Course Count: 1.00
Billing Units: 1
Mentioned in the Following Calendar Pages
*List may not include courses that are on a common table shared between programs.
- AER 814 - Aircraft Design Project
- Aerospace Engineering