Consider the 2d inviscid flow over a body of some known

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Reference no: EM13613115

Consider the 2D inviscid flow over a body of some known shape. Write down general expressions for the total aerodynamic force(per unit depth perpendicular to the plane) and the lift and drag forces(per unit depth perpendicular to the plane) on the body in terms of pressure field p and the unit normal vector field n on the boundary of the body. Assume that the free stream is parallel to the positive x-direction.

Reference no: EM13613115

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