Hypersonic Rarefied Flows Around a Circular Disk Perpendicular to the Stream
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概要
- 論文の詳細を見る
Rarefied gas flows around a circular disk in a hypersonic stream are analysed by the direct simulation Monte Carlo method. The domain of calculation is fully three-dimensional. The rarefaction effect upon the flow field, the drag and heat transfer coefficients, and the recovery temperature is shown for Kn=0.1-20 at the wall to stagnation temperature ratios of 0.5 and 1. The drag coefficient is in good agreement with the experimental data for argon by Legge. The cell network proposed here can easily be applied to more general lifting flows.
- 宇宙航空研究開発機構の論文
著者
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NANBU Kenichi
Institute of Fluid Science, Tohoku University
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Watanabe Y
Department Of Bioresources Faculty Of Agriculture Ehime University
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Nanbu Kenichi
Institute Of Fluid Science Tohoku University
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IGARASHI Saburo
Institute of High Speed Mechanics, Tohoku University
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WATANABE Yasuo
Institute of High Speed Mechanics, Tohoku University
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Igarashi Saburo
Institute Of High Speed Mechanics Tohoku University
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Watanabe Y
Department Of Cell Physiology Faculty Of Medicine Kagawa University
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Nanbu K
Institute Of High Speed Mechanics Tohoku University
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Watanabe Yasuo
Institute Of High Speed Mechanics Tohoku University
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Nanbu Kenichi
Institute For Fluid Science Tohoku University
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Watanabe Yasuo
Institute of Space and Astronautical Science
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