Experimental Studies of Supersonic Flow past a Circular Cylinder

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概要

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• Experimental studies using shock tubes are presented of the mixed Type flow around a circular cylinder placed normal to the general flow of Mach number 1.35, 1.8, 2.7, 3.5, 4.0, and 6.0. With the MachZehnder interferometer and schlieren method the followings were measured: a) shape of detached shock wave, b) distance d of shock wave from the cylinder nose, c)pressure coefficient C_ρon the surface of the cylinder, d) density distribution behind the detached shock, e)streamlines in subsonic region.

• 社団法人日本物理学会の論文
• 1956-04-05

著者

• Kim Chul-soo

  Department Of Physics Faculty Of Science University Of Tokyo

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