Observation of Supersonic Jet Using Small Volume High-Pressure Shock Tube

Ryohei Takemura; Hiroshi Fukuoka; Shinichi Enoki; Shigeto Nakamura; Kazuki Hiro

doi:10.4028/www.scientific.net/MSF.910.143

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HomeMaterials Science ForumMaterials Science Forum Vol. 910Observation of Supersonic Jet Using Small Volume...

Observation of Supersonic Jet Using Small Volume High-Pressure Shock Tube

Abstract:

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.

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Periodical:

Materials Science Forum (Volume 910)

Pages:

143-148

DOI:

https://doi.org/10.4028/www.scientific.net/MSF.910.143

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Online since:

January 2018

Authors:

Ryohei Takemura, Hiroshi Fukuoka*, Shinichi Enoki, Shigeto Nakamura, Kazuki Hiro

Keywords:

BOS Method, Shock Tube, Shock Wave, Supersonic Jet

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