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A METHOD OF COMPUTING SUBSONIC FLOWS AROUND GIVEN AIRFOILS

机译:一种计算机翼周围的声子流的方法

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An extremely simple computational method is established for obtaining circulatory flows around given bodies to a high degree of accuracy for flows satisfying the linear pressure and specific-volume equation of state. The method depends not on an integral equation hut on the transformation from the hodograph to the physical plane involving the determination of an arbitrary analytic function. The determination of the arbitrary analytic function by elementary means results in a close approximation of the given body.

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