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Numerical Investigation of Tip Clearance Effects in an Axial Transonic Compressor

R. Ciorciari A. Lesser F. Blaim R. Niehuis

热科学学报（英文版）2012，Vol.21Issue(2)：109-119,11.

热科学学报（英文版）2012，Vol.21Issue(2)：109-119,11.DOI:10.1007/s11630-012-0525-6

Numerical Investigation of Tip Clearance Effects in an Axial Transonic Compressor

R. Ciorciari ¹A. Lesser ¹F. Blaim ¹R. Niehuis¹

作者信息

1. Institute for Jet Propulsion, University of Federal Armed Forces Munich, Werner-Heisenberg-Weg 39, D-85577 Neubiberg
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摘要

关键词

Flow in axial compressor/surge and stall/tip clearance flow/multimode transition model

Key words

Flow in axial compressor/surge and stall/tip clearance flow/multimode transition model

引用本文复制引用

R. Ciorciari,A. Lesser,F. Blaim,R. Niehuis..Numerical Investigation of Tip Clearance Effects in an Axial Transonic Compressor[J].热科学学报（英文版）,2012,21(2):109-119,11.

基金项目

The Investigations were conducted as a part of the Deutsche Forschungsgemeinschaft Joint Research Project FOR-1066. （）

热科学学报（英文版）

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ISSN：1003-2169

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