Inverse Panel Methods -- CFD Online Discussion Forums

July 21, 1999, 16:28	Inverse Panel Methods	#1
Nibo Guest Posts: n/a	Inverse Panel Method in 2D: Specify a Cp distribution, and find the airfoil shape that produces the Cp distribution by solving inversely and iteratively the linear system, resulting from a panel method, w.r.t. the coordinates of the control points(not w.r.t. the singularity strengths). QUESTION: How can I determine the strengths of the singularities for a given Cp distribution? (for example, vortex strength for each panel for constant vortex panel method.) In the literature, no one explains how to do this, but they seem to have done this. Thank you Nibo

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