Consider a two-dimensional steady, inviscid flow over some airfoil in a uniform unbounded free stream of velocity V. and

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Consider a two-dimensional steady, inviscid flow over some airfoil in a uniform unbounded free stream of velocity V. and

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Consider A Two Dimensional Steady Inviscid Flow Over Some Airfoil In A Uniform Unbounded Free Stream Of Velocity V And 1
Consider A Two Dimensional Steady Inviscid Flow Over Some Airfoil In A Uniform Unbounded Free Stream Of Velocity V And 1 (22.24 KiB) Viewed 57 times
Consider a two-dimensional steady, inviscid flow over some airfoil in a uniform unbounded free stream of velocity V. and pressure po.. Treat the flow as incompressible and irrotational. A. (6 points) Provide a complete statement of the boundary value problem for determining the velocity potential of this flow. Include all necessary conditions required to make the solution unique. B. (4 points) Discuss the calculation of the pressure forces acting on the body once the velocity potential has been found.
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