高速度における翼型のまはりの速度分布について,II.圓柱及び圓弧翼

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§12. On the basis of a new method of M^2-expansion, analytical formulae are obtained, which give the velocity distribution on an arbitrary wing section placed in a uniform flow of a compressible fluid exactly to the order of M^4, M being the MACH number of the undisturbed stream. These formulae would be of particular value for the purely numerical work, though in some cases they will also enable us to find analytical expressions for the velocity distribution. Examples of the application of the formulae, both analytical and numerical, will be given in forthcoming papers.
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