Study on flow structure around hypersonic TSTO launch vehicle

Flow structures around hypersonic TSTO launch vehicle were investigated by utilizing the electrical discharge method. First, boundary layers near the orbiter surface were observed by a visualization technique of boundary layers. Subsequently, lateral and cross-sectional shock shapes around TSTO laun...

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Published inNihon Kikai Gakkai rombunshuu. B hen Vol. 16; no. 2; pp. 325 - 331
Main Authors Nishio, M, Sezaki, S, Nakamura, H, Yamamoto, Y
Format Journal Article
LanguageJapanese
Published 01.02.2004
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Abstract Flow structures around hypersonic TSTO launch vehicle were investigated by utilizing the electrical discharge method. First, boundary layers near the orbiter surface were observed by a visualization technique of boundary layers. Subsequently, lateral and cross-sectional shock shapes around TSTO launch vehicle were observed by a visualization technique of shock waves. From these results, it was confirmed that a separation shock wave was generated near the orbiser surface. In this study, the visualizations were carried out at Mach 10.
AbstractList Flow structures around hypersonic TSTO launch vehicle were investigated by utilizing the electrical discharge method. First, boundary layers near the orbiter surface were observed by a visualization technique of boundary layers. Subsequently, lateral and cross-sectional shock shapes around TSTO launch vehicle were observed by a visualization technique of shock waves. From these results, it was confirmed that a separation shock wave was generated near the orbiser surface. In this study, the visualizations were carried out at Mach 10.
Author Sezaki, S
Nakamura, H
Nishio, M
Yamamoto, Y
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  surname: Yamamoto
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Snippet Flow structures around hypersonic TSTO launch vehicle were investigated by utilizing the electrical discharge method. First, boundary layers near the orbiter...
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