Effect of Unsteady Pressure Gradient Reduction on Dynamic Stall Delay
- 1 October 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (10), 839-841
- https://doi.org/10.2514/3.59179
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Aerodynamic loading on a two-dimensional airfoil during dynamic stall.AIAA Journal, 1968
- Theoretical Pressure Distributions for a Thin Airfoil Oscillating in Incompressible FlowJournal of the Aeronautical Sciences, 1948