Introduction, definitions, influence of aeroelastic phenomena on design,comparison of wing critical speeds, deformations of airplane structures under staticloads, deformations of airplane structures under dynamic loads, approximate methodsof computing natural mode shapes and frequencies, static aeroelasticity: model forapplication to aileron reversal, uniform lifting surface: equilibrium equation, torsionaldivergence swept wings, flutter: nature of flutter, flutter of a simple system with twodegrees of freedom of the bending-torsion flutter of a uniform cantilever wing, solutionflutter methods, testing techniques.
