Some problems of design and operation of a 250- knot compound helicopter rotor
- 1 September 1964
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 1 (5) , 252-259
- https://doi.org/10.2514/3.43591
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- HIGH PERFORMANCE SINGLE ROTOR HELICOPTER STUDYPublished by Defense Technical Information Center (DTIC) ,1961
- Analysis of the Stability of a Flexible Rotor Blade at High Advance RatioJournal of the American Helicopter Society, 1959
- Stability of a Flexible Helicopter Rotor Blade in Forward FlightJournal of the Aeronautical Sciences, 1956
- Rotor blade flapping motionQuarterly of Applied Mathematics, 1947