Airfoil pressure measurements during a blade-vortex interaction and a comparison with theory
- 11 January 1988
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
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- Helicopter Noise due to Blade-Vortex InteractionThe Journal of the Acoustical Society of America, 1971