Airfoil dynamic stall at constant pitch rate and high Reynolds number
- 1 June 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (6) , 548-556
- https://doi.org/10.2514/3.45621
Abstract
No abstract availableKeywords
This publication has 8 references indexed in Scilit:
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- Dynamic Stall of Airfoil Sections for High‐Speed RotorsJournal of the American Helicopter Society, 1969
- Dynamic Stall Considerations in Helicopter RotorsJournal of the American Helicopter Society, 1968