Experimental Investigation of a Gas Dynamic Thrust Vector Control for Hypersonic Space Planes
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概要
- 論文の詳細を見る
The feasibility and performance of a gas dynamic thrust vector control for advanced space planes using wall bleeding were investigated experimentally in the form of a parameter variation. In these studies, attempts were made to minimize the required control mass flows taken from the forebody boundary layer or intake. Furthermore, a semiempirical method for the design of the bleeding channel and geometry is presented, as well as a possible application of the results to flight mechanics.
- 一般社団法人日本機械学会の論文
- 1996-02-15
著者
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Setoguchi T
Saga Univ. Saga Jpn
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Setoguchi Toshiaki
Saga Univ
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Setoguchi Toshiaki
Department Of Mechanical Engineering Saga University
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Zeutzius M
Saga Univ
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Matsuo Shigeru
Department Of Mechanical Engineering Saga University
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Matsuo Shigeru
Saga Univ
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ZEUTZIUS Michael
Department of Mechanical Engineering, Saga University
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BEYLICH Alfred
Stosswellenlabor, RWTH Aachen
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Matsuo Satoshi
Saga Univ
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Beylich Alfred
Stosswellenlabor Rwth Aachen
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Zeutzius Michael
Department Of Mechanical Engineering Saga University
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