Effect of a blade end slot on supersonic compressor cascade hub-corner separation
Authors:
- Jianci MaJMJianci Ma
- Guang YangGYGuang Yang
- Ling ZhouLZLing Zhou
- Lucheng JiLJLucheng Ji
- Chun ZhangCZChun Zhang
- 1 November 2021
- journal article
- research article
- Published by Elsevier in Aerospace Science and Technology
- Vol. 118
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51406011, 51676015, 51976010)
- Deutsches Zentrum für Luft- und Raumfahrt
- Beijing Institute of Technology Research Fund Program for Young Scholars (2019CX04008)
- National Major Science and Technology Projects of China (2017-II-0001-0013, 2017-II-0006-0020, 2019-II-0003-0023)
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