NASA NTRS · 19890027650
An exact inverse method for subsonic flows
Abstract
A new inverse method for the aerodynamic design of airfoils is presented for subcritical flows. The pressure distribution in this method can be prescribed as a function of the arclength of the still unknown body. It is shown that this inverse problem is mathematically equivalent to solving only one nonlinear boundary value problem subject to known Dirichlet data on the boundary.
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Daripa, Prabir. 1988-09-01. An exact inverse method for subsonic flows. https://ntrs.nasa.gov/citations/19890027650
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