热科学学报（英文版）2015，Vol.24Issue(6)：510-515,6.DOI:10.1007/s11630-015-0816-9
Shock Wave Boundary Layer Interaction on Suction Side of Compressor Profile in Single Passage Test Section
Shock Wave Boundary Layer Interaction on Suction Side of Compressor Profile in Single Passage Test Section
Pawel Flaszynski 1Piotr Doerffer 1Ryszard Szwaba 1Piotr Kaczynski 1Michal Piotrowicz1
作者信息
- 1. The Szewalski Institute of Fluid-Flow Machinery Polish Academy of Sciences (IMP PAN), Fiszera 14, Gdansk, Poland
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摘要
关键词
transonic flow/shock wave/laminar-turbulent transition/compressor profileKey words
transonic flow/shock wave/laminar-turbulent transition/compressor profile引用本文复制引用
Pawel Flaszynski,Piotr Doerffer,Ryszard Szwaba,Piotr Kaczynski,Michal Piotrowicz..Shock Wave Boundary Layer Interaction on Suction Side of Compressor Profile in Single Passage Test Section[J].热科学学报（英文版）,2015,24(6):510-515,6.
