The Effect of Dynamic Stall on the Response and Airloading of Helicopter Rotor Blades
- 1 April 1969
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 14 (2) , 68-79
- https://doi.org/10.4050/jahs.14.68
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Aerodynamic loading on a two-dimensional airfoil during dynamic stall.AIAA Journal, 1968
- A PRESENTATION OF MEASURED AND CALCULATED FULL-SCALE ROTOR BLADE AERODYNAMIC AND STRUCTURAL LOADSPublished by Defense Technical Information Center (DTIC) ,1966
- TABULATED SIKORSKY CH-34 BLADE SURFACE PRESSURES MEASURED AT THE NASA/ AMES FULL SCALE WIND TUNNELPublished by Defense Technical Information Center (DTIC) ,1966
- Unsteady Air Loads on Helicopter Rotor BladesJournal of the Royal Aeronautical Society, 1964
- Future of Vertical Lift AircraftJournal of the American Helicopter Society, 1956