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Control of compression ramp flow separation via vane vortex generator [叶片式涡流发生器对压缩拐角流动分离的控制]
Hu, W.; Yu, J.; Liu, H.; Zhao, Y.; Yan, C.
刊名Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
2018
卷号39
关键词Acoustic streaming Boundary layers Drag Flow separation Hypersonic flow Navier Stokes equations Rotating machinery Shock waves Turbomachine blades Turbulence models Vorticity Boundary-layer separation Compression ramps Shock wave boundary layer interactions Streamwise vortices Vortex generators Vortex flow
ISSN号10006893
DOI10.7527/S1000-6893.2018.22049
URL标识查看原文
收录类别CSCD
内容类型期刊论文
URI标识http://www.corc.org.cn/handle/1471x/5928655
专题北京航空航天大学
推荐引用方式
GB/T 7714
Hu, W.,Yu, J.,Liu, H.,等. Control of compression ramp flow separation via vane vortex generator [叶片式涡流发生器对压缩拐角流动分离的控制][J]. Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,2018,39.
APA Hu, W.,Yu, J.,Liu, H.,Zhao, Y.,&Yan, C..(2018).Control of compression ramp flow separation via vane vortex generator [叶片式涡流发生器对压缩拐角流动分离的控制].Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica,39.
MLA Hu, W.,et al."Control of compression ramp flow separation via vane vortex generator [叶片式涡流发生器对压缩拐角流动分离的控制]".Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica 39(2018).
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