INVESTIGATIONS OF MACH REFLECTION OF A SHOCK WAVE

(2nd REPORT, SHAPE OF A REFLECTED SHOCK WAVE).

Kazuyasu Matsuo, Toshiyuki Aoki, Nobuaki Kondoh, Hiroyuki Hirahara

研究成果: ジャーナルへの寄稿記事

抄録

Experimental analysis has been carried out to explain and predict the Mach reflection phenomena of a plane moving shock wave from a wedge surface. In the first report, the domains of four types of reflection were shown, in an incident shock Mach number-wedge angle plane, and the transition boundaries between these domains were discussed. In the present paper, the triple point trajectory angle and the location of a kink point of a reflected shock in the case of three types of Mach reflection have been investigated experimentally over a wide range of incident shock Mach numbers and wedge angles. Based on the experimental results, the shape of a reflected shock wave has been explained generally and comprehensibly.

元の言語英語
ページ(範囲)422-427
ページ数6
ジャーナルBulletin of the JSME
29
発行部数248
DOI
出版物ステータス出版済み - 1 1 1986

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Shock waves
Mach number
Trajectories

All Science Journal Classification (ASJC) codes

  • Engineering(all)

これを引用

INVESTIGATIONS OF MACH REFLECTION OF A SHOCK WAVE : (2nd REPORT, SHAPE OF A REFLECTED SHOCK WAVE). / Matsuo, Kazuyasu; Aoki, Toshiyuki; Kondoh, Nobuaki; Hirahara, Hiroyuki.

:: Bulletin of the JSME, 巻 29, 番号 248, 01.01.1986, p. 422-427.

研究成果: ジャーナルへの寄稿記事

Matsuo, Kazuyasu ; Aoki, Toshiyuki ; Kondoh, Nobuaki ; Hirahara, Hiroyuki. / INVESTIGATIONS OF MACH REFLECTION OF A SHOCK WAVE : (2nd REPORT, SHAPE OF A REFLECTED SHOCK WAVE). :: Bulletin of the JSME. 1986 ; 巻 29, 番号 248. pp. 422-427.
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