Visualization of shock tube airfoil flow with a sharp focusing schlieren method

Author(s):  
Masashi Kashitani ◽  
Yutaka C. Yamaguchi
2000 ◽  
Vol 20 (77) ◽  
pp. 158-164
Author(s):  
Yutaka YAMAGUCHI ◽  
Masashi KASHITANI ◽  
Shinichi WADA ◽  
Teruo SAITO

2018 ◽  
Vol 910 ◽  
pp. 143-148
Author(s):  
Ryohei Takemura ◽  
Hiroshi Fukuoka ◽  
Shinichi Enoki ◽  
Shigeto Nakamura ◽  
Kazuki Hiro

The unsteady supersonic jet and the shock wave injected by the small volume shock tube are experimentally studied in this paper. The experimental was performed by the background oriented schlieren method. The main parameters for the jet are the pressure ratio by the high pressure chamber/ a back pressure 10.9-53.0 and the length of high pressure chamber/diameter ratio 1 and 10. The velocity of the shock wave and supersonic jet were estimated by using the principle of the background oriented schlieren method. The results showed that the influence of the length of the high pressure chamber on the velocity of the jet.


2012 ◽  
Vol 21 (5) ◽  
pp. 435-440 ◽  
Author(s):  
Masashi Kashitani ◽  
Keita Miura ◽  
Shinichiro Nakao ◽  
Yutaka Yamaguchi

1974 ◽  
Vol 60 (11) ◽  
pp. 4170-4174 ◽  
Author(s):  
Gerald J. Diebold ◽  
Robert J. Santoro ◽  
George J. Goldsmith

2006 ◽  
Vol 134 ◽  
pp. 783-787 ◽  
Author(s):  
S. Ouellet ◽  
D. Frost ◽  
A. Bouamoul

1972 ◽  
Vol 22 (3) ◽  
pp. 303-317 ◽  
Author(s):  
D. H. Napier ◽  
N. Subrahmanyam
Keyword(s):  

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