Art

J-GLOBAL ID：201702280470077863   Reference number：17A0156893

Optimizing of the Structural Parameters of an Asymmetric Ramp Micro-Vortex Generator in Supersonic Flow

非定常流路における非対称傾斜渦流発生器の構造パラメータを最適化した。【JST・京大機械翻訳】

Author (4)： Wang Kai (Institute of Engineering Thermophysics, Chinese Academy of Sciences) ,  Zhang Binbin (Institute of Engineering Thermophysics, Chinese Academy of Sciences; Key Laboratory of Light-duty Gas-turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences) ,  Li Jing (Institute of Engineering Thermophysics, Chinese Academy of Sciences; Key Laboratory of Light-duty Gas-turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences) ,  Zhao Qingjun (Institute of Engineering Thermophysics, Chinese Academy of Sciences; Key Laboratory of Light-duty Gas-turbine, Institute of Engineering Thermophysics, Chinese Academy of Sciences)
Material： Gongcheng Rewuli Xuebao  (Journal of Engineering Thermophysics)
Volume： 37  Issue： 11  Page： 2303-2310  Publication year： 2016 
JST Material Number： C2102A  ISSN： 0253-231X  CODEN： KCJPDF  Document type： Article
Article type： 原著論文  Country of issue： China (CHN)  Language： CHINESE (ZH)

Abstract/Point： Based on the orthogonal test d...

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Thesaurus term： eddy current ,  *structural parameter ,  incompressibility ,  *asymmetry ,  *optimization ,  form factor ,  *vortex flow ,  shock wave ,  orthogonality ,  interference ,  boundary layer ,  *unsteady flow
Semi thesaurus term： 境界層厚さ ,  数値シミュレーション ,  *再生器 , 【Automatic Indexing@JST】

Author keywords (3)： micro-vortex generators ,  orthogonal experiment ,  shock/boundary layer interaction

JST classification (3)： Laminar flows,turbulent flows and boundary layers  (BC02030C) ,  High-speed aerodynamics  (BC03000C) ,  Aerodynamics of aircrafts  (QK02010T)

Terms in the title (6)： 非定常流 ,  非対称 ,  渦流 ,  発生器 ,  構造パラメータ ,  最適化