Drag Reduction In Supersonic Profiles
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Abstract
Drag reduction for aerial vehicle has a wide range of positive benefits when the aircraft speed is higher than speed of sound, performance of aircraft will change due to air conditions that are different from the lower speed. In this project, the primary aim is to learn and analyse the performance of drag on supersonic airfoil and various types of drag and drag reduction techniques .the objective of this study is to develop a supersonic airfoil for different types of flows with different parameter using ansys .The parameter which gives more efficiently by reducing drag is used for drag is used for drag reduction.
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