Theoretical Consideration on Laminar-To-Turbulent Transitions over an Ablating Reentry Capsule
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概要
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The mechanism of early transition phenomena over an ablating reentry capsule has been examined. A two-equation turbulence model (kappa-epsilon model) coupled with Reynolds averaged Navier-Stokes equations has been employed. Low-Reynolds-number effects on
- 宇宙航空研究開発機構の論文
著者
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Komurasaki Kimiya
Department Of Aeronautics And Astronautics University Of Tokyo
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Komurasaki Kimiya
Department Of Advanced Energy The University Of Tokyo
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Candler Graham
Department of Aerospace Engineering and Mechanics, University of Minnesota
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Candler Graham
Department Of Aerospace Engineering And Mechanics University Of Minnesota
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