Three dimensional flow structure behind a shock wave discharged from a rectangular cross section shock tube

Author:

Abe A.,Watanabe M.,Suzuki K.

Publisher

Springer Berlin Heidelberg

Reference5 articles.

1. Abe A, Takayama K (1990) Numerical simulation and density measurement of a shock wave discharged from the open end of a shock tube. JSME 33:246–223

2. Merzkirch W (1974) Flow visualization, Academic Press, pp 115

3. Takayama K (1983) Application of holographic interferometry to shock wave research. Proc SPIE 298:174

4. Teshima K (1989) Three-dimensional structure of a supersonic free jet issuing from a rectangular orifice. Int Symp CFD-Nagoya, pp 1144–1149

5. Yee HC (1988) A class of high-resolution explicit and implicit shock capturing methods, NASA TM 101088

Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Shock Wave Diffraction at the Inclined Exit of a Shock Tube;29th International Symposium on Shock Waves 2;2015

2. Shockwave Beyond;28th International Symposium on Shock Waves;2012

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