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J-GLOBAL ID：201702245302267227   Reference number：17A0073605

Investigation on Effects of EndWall Boundary Layer Suction on Transonic Rotor Flow Characteristics

遷音速ロータ翼の流れ特性に及ぼす端部吸引の影響を研究した。【JST・京大機械翻訳】

Author (4)： An Xin (Institute of Engineering Thermophysics,Chinese Academy of Sciences) ,  Sun Xiaolei (Institute of Engineering Thermophysics,Chinese Academy of Sciences) ,  Cui Weiwei (Institute of Engineering Thermophysics,Chinese Academy of Sciences) ,  Zhao Qingjun (Institute of Engineering Thermophysics,Chinese Academy of Sciences, Laboratory of Light-Duty Gas-Turbine,Chinese Academy of Sciences)
Material： Tuijin Jishu  (Journal of Propulsion Technology)
Volume： 37  Issue： 9  Page： 1664-1672  Publication year： 2016 
JST Material Number： C2162A  ISSN： 1001-4055  Document type： Article
Article type： 原著論文  Country of issue： China (CHN)  Language： CHINESE (ZH)

Abstract/Point： The numerical simulations have...

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Thesaurus term： *flow characteristic ,  wing tip ,  boundary layer ,  flow rate ,  control system (computer) ,  *sound velocity ,  reverse flow ,  the National Aeronautics and Space Administration ,  load distribution ,  curvature ,  *rotary wing ,  pressure ratio ,  comparative analysis ,  Numerical Simulation ,  layer
Semi thesaurus term： *吸引 , 【Automatic Indexing@JST】

Author keywords (4)： Transonic rotor ,  Flow control ,  End-wall boundary layer suction ,  Corner separation

JST classification (4)： Gas turbines  (PB02040Y) ,  Laminar flows,turbulent flows and boundary layers  (BC02030C) ,  Convective and radiative heat transfer  (PA02030K) ,  Blowers,compressors,wind turbines  (QD03000U)

Terms in the title (4)： ロータ翼 ,  流れ特性 ,  吸引 ,  研究