Torsional oscillation of helicopter blades due to stall.
- 1 May 1966
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 3 (3), 218-224
- https://doi.org/10.2514/3.43728
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- An Experimental Investigation of Stall FlutterJournal of the American Helicopter Society, 1962
- Single Degree of Freedom Flutter of Compressor Blades in Separated FlowJournal of the Aeronautical Sciences, 1954