Prediction of Control Loads Due to Blade Stall
- 1 April 1972
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 17 (2) , 33-46
- https://doi.org/10.4050/jahs.17.33
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- Rotor High Speed Performance, Theory vs. TestJournal of the American Helicopter Society, 1970
- Blade Stall—Half Fact, Half FictionJournal of the American Helicopter Society, 1968
- An Analysis of the Stall Flutter Instability of Helicopter Rotor BladesJournal of the American Helicopter Society, 1967
- Preliminary Study of Radial Flow Effects on Rotor BladesJournal of the American Helicopter Society, 1966
- Torsional oscillation of helicopter blades due to stall.Journal of Aircraft, 1966