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 vortex shedding, buffeting and stall flutter. Flight testing. Lect: 3 hrs. Prerequisites: AER 403 and AER 606 and AER 621 and EES 512 Course Weight: 1.00 Billing Units: 1
