One of the most important inverse problems in aerodynamics is defined as the problem of finding the wing section contour given the desired surface pressure distribution for a fixed wing planform. This problem can be solved by the 'residual-correction' method based on the transonic integral equations. In this paper, some of the recent applications of the integral equation method using various analysis codes including Navier-Stokes codes is presented.
航空力学における逆問題とその解法
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