Crossflow and Unsteady Boundary-Layer Effects on Rotating Blades
- 1 August 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (8) , 1498-1505
- https://doi.org/10.2514/3.49952
Abstract
No abstract availableKeywords
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