On the Detached Shock wave in front of a Body of Revolution moving with Supersonic Speeds

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概要

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• The uniform supersonic flow Past a body of revolution with a finite radius of curvature at its nose is studied. Various hydrodynamical quantities are expanded in power series of the coordinates in the neighbourhood of the stagnation point of the body. The coeffieients of the series are determined by the boundary conditions, at the surface of the body as well as by the shock wave conditions. at the shock wave. Numerical results are compared with the existing experiments as well as with the theoretical results obtained previously by the writer.

• 社団法人日本物理学会の論文
• 1952-10-25

著者

• Kawamura Toru

  Shiga Prefectural Junior College

関連論文

• On the Detached Shock wave in front of a Body of Revolution moving with Supersonic Speeds

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