A lifting-surface solution for vortex-induced airloads
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 9 (4) , 689-695
- https://doi.org/10.2514/3.6249
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Helicopter Noise due to Blade-Vortex InteractionThe Journal of the Acoustical Society of America, 1971
- New directions in lifting surface theoryAIAA Journal, 1965
- Some Aspects of Non-Stationary Airfoil Theory and Its Practical ApplicationJournal of the Aeronautical Sciences, 1941