Institute of Space and Aeroautical Science University of Tokyo
Institute of Space and Aeroautical Science University of Tokyo
Institute of Space and Aeroautical 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
10
号
4_B
ページ
779 - 786
発行年
1974-12
抄録（英）
The shock tube is of simple mechanism, but an ordinary shock tube with diaphragm is not necessarily convenient for quick operations because of both renewal of diaphragm for each operation and contamination by broken segments. To avoid such inconvenience several authors proposed to employ a mechanical or electro-magnetical shock valve instead of the diaphragm. In the present paper a type of the mechanical shock valve for shock tube is proposed, having comparatively simple device of high pressure release. The characteristic performance of the shock tube equipped with this valve is investigated for various modes of the operation; specifically, the process of the shock wave formation is studied by means of the pressure measurements and the streak photographs of the M-Z interferogram.
無隔膜ショック・チューブの特性と衝撃波形成に関する実験
SA0124454.pdf
(818.38KB)
