Investigations of Mach Reflection of a Shock Wave: (Part 3, Strength of a Reflected Shock Wave)

Kazuyasu Matsuo, Toshiyuki Aoki, Hiroyuki Hirahara, Nobuaki Kondoh, Kousei Kuriwaki

研究成果: Contribution to journalArticle査読

抄録

The reflection phenomena of a plane moving shock wave at a wedge surface have been investigated by many researchers, and four different types of reflection have been observed in previous shock tube experiments. The authors reported in the previous reports on the domains and boundaries of these four types of reflection and the shape of a reflected shock wave. In the present paper, the distribution of the strength of a reflected shock wave along its wave front has been calculated from its shape obtained by optical observations, and the relation between the strength and the shape of a reflected shock wave has been discussed detail. Furthermore, the flow properties around the triple point in the case of Mach reflection have been calculated using experimental data, and the validity of the three shock theory has been examined.

本文言語英語
ページ(範囲)1941-1946
ページ数6
ジャーナルNihon Kikai Gakkai Ronbunshu, B Hen/Transactions of the Japan Society of Mechanical Engineers, Part B
51
466
DOI
出版ステータス出版済み - 1985

All Science Journal Classification (ASJC) codes

  • 凝縮系物理学
  • 機械工学

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