the Institute of Space and Aeronautical Science University of Tokyo
the Institute of Space and Aeronautical Science University of Tokyo
出版者
東京大学宇宙航空研究所
雑誌名
東京大学宇宙航空研究所報告
巻
2
号
2_A
ページ
467 - 475
発行年
1966-04
抄録（英）
This paper is concerned with characteristic features of a high-temperature flow at a shock tuhe driven by means of a free piston compression. In order to analyse high temperature flow caused by this type of shock tube, in particular a light-pulse generator of He-Ne gas laser is developed and applied to the streak Mach-Zehender interferometry by use of a rotating drum camera. The results show that the high temperature flow thus produced is nicely separated from the driver gases and comparatively uniform. It can be expected that its applicability to experimental investigations of high temperature flow phenomena is more promising compared with conventional shock tubes.
自由ピストン衝撃波管の実験 : 特にガスレーザ・パルス光発生とそれによる流れの観察
SA0124860.pdf
(1.05MB)
