Investigation of flow unsteadiness in a highly-loaded compressor cascade using a dynamic mode decomposition method
Open Access
- 20 October 2021
- journal article
- research article
- Published by Elsevier BV in Chinese Journal of Aeronautics
- Vol. 35 (5), 275-290
- https://doi.org/10.1016/j.cja.2021.09.003
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China
- National Major Science and Technology Projects of China
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