Abstract
Aeroelasticity is the study of the mutual interaction that takes place among the inertial, elastic and aerodynamic forces acting on the structural members exposed to an airstream and the influence of this study on the design. This review paper deals with the investigation of the aeroelasticity phenomena. The effect of the aeroelasticity phenomena occurring while designing the wing of the aircraft are stated in detail. Flutter suppression and its techniques are investigated in this paper. The aeroelastic testing techniques available in this field and the efficient methods to solve these problems are discussed. The aeroelastic optimization techniques processes are reported. The fluid and structure interaction of the non-linear flexible wing structure results have been discussed for the various methods. The application of the MSC software and finite element methods are discussed. The aeroelastic applications are also summarized
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