On the Subsonic Flow of a Compressible Fluid past an Axisymmetric Slender Body
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概要
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Introducing new variables the fundamental equation for compressible fluid flow in the hodograph space is reduced to a form similar to that for incompressible fluid flow. Safely neglecting the variation of the shape of an obstacle caused by the transformation, we can obtain the velocity distribution on the surface of the obstacle for the case of compressible fluid flow from the corresponding distribution on the surface of the same obstacle for the case of incompressible fluid flow (which is known theoretically or experimentally), with the aid of the following relations: [numerical formula] where q_0, q, c and γ denote respectively the magnitudes of fluid velocity in incompressible and compressible fluid flows, the local speed of sound and the ratio of the specific heats. As an example the velocity distributions on the surface of a prolate spheroid with thickness ratio t=0.1 are calculated for various Mach numbers and they are compared with the result obtained by the first approximation of the M^2-expansion method.
- 社団法人日本物理学会の論文
- 1954-08-25
著者
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Kusukawa Ken-ichi
Department Of Physics Faculty Of Science Tokyo Metropolitan University
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Kusukawa Ken-ichi
Department Of Physics Faculty Of Science Tokyo Metroplitan University
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Kusukawa Ken-ichi
Department Of Physics Faculity Of Science Tokyo Metropolitan University
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