Effect investigation of single-slotted and double-slotted configurations on the corner separation and aerodynamic performance in a high-load compressor cascade-Reference-Cited by-同舟云学术

Effect investigation of single-slotted and double-slotted configurations on the corner separation and aerodynamic performance in a high-load compressor cascade

Published:2023-04 Issue: Volume:135 Page:108203
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Wang Hejian,Mao Xiaochen,Liu Bo,Zhang Botao^ORCID,Yang Zonghao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

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2. Development of fan/compressor techniques and suggestions on further researches;Chen;J. Aerosp. Power,2002

3. Loss reduction in axial-flow compressors through low-speed model testing;Wisler;J. Eng. Gas Turbines Power,1985

4. Three-dimensional flows and loss reduction in axial compressors;Dong;J. Turbomach.,1987

5. Three-dimensional separations in axial compressors;Gbadebo;J. Turbomach.,2005

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