Tip vortex effects on oscillating rotor blades in hovering flight
- 1 January 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (1) , 106-113
- https://doi.org/10.2514/3.6130
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Compressibility effects on oscillating rotor blades in hovering flightAIAA Journal, 1970
- Rotor blade harmonic air loadingAIAA Journal, 1964
- The Influence of the Wake on the Flutter and Vibration of Rotor BladesAeronautical Quarterly, 1958