Art

J-GLOBAL ID：201902260713866737   Reference number：19A1531120

Plasma-Assisted Control of Supersonic Flow over a Compression Ramp

圧縮ランプ上の超音速流のプラズマ支援制御【JST・京大機械翻訳】

Author (4)： Watanabe Yasumasa (Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, IN 46556, USA) ,  Watanabe Yasumasa (Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo 113-8656, Japan) ,  Houpt Alec (Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, IN 46556, USA) ,  Leonov Sergey B. (Department of Aerospace and Mechanical Engineering, University of Notre Dame, Notre Dame, IN 46556, USA)
Material： Aerospace (Web)
Volume： 6  Issue： 3  Page： 35  Publication year： 2019 
JST Material Number： U7127A  ISSN： 2226-4310  Document type： Article
Article type： 原著論文  Country of issue： Switzerland (CHE)  Language： ENGLISH (EN)

Abstract/Point： This study considers the effec...

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Thesaurus term： flow structure ,  shock (mechanics) ,  high speed camera ,  supersonic wind tunnel ,  leading edge ,  Reynolds number ,  visualization ,  pressure distribution ,  enthalpy ,  effectiveness ,  *supersonic flow ,  pressure fluctuation ,  *plasma ,  *supersonic speed

Author keywords (3)： plasma-assisted flow control ,  supersonic airflow ,  compression ramp

JST classification (1)： Electronic navigation in general  (ND14010O)

Reference (25)：

• Verma, S.B.; Hadjadj, A. Supersonic flow control. Shock Waves 2015, 25, 443-449.
• [Green Version] Holden, H.; Babinsky, H.H. Effect of Microvortex Generators on Separated Normal Shock/Boundary Layer Interactions. J. Aircraft 2007, 44, 170-174.
• Saad, M.R.; Zare-Behtash, H.; Che-Idris, A.; Kontis, K. Micro-Ramps for Hypersonic Flow Control. Micromachines 2012, 3, 364-378.
• [Green Version] Settles, G.S.; Fitzpatrick, T.J.; Bogdonoff, S.M. Detailed Study of Attached and Separated Compression Corner Flowfields in High Reynolds Number Supersonic Flow. AIAA J. 1979, 17, 579-585.
• Settles, G.S.; Vas, I.E.; Bogdonoff, S.M. Details of a Shock-Separated Turbulent Boundary Layer at a Compression Corner. AIAA J. 1976, 14, 1709-1715.

Terms in the title (4)： ランプ ,  超音速流 ,  プラズマ ,  支援