Experimental investigation of the perpendicular rotor blade-vortex interaction at transonic speeds
- 1 March 1992
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 30 (3) , 747-755
- https://doi.org/10.2514/3.10980
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Rotor-vortex interaction noisePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Full-Scale Measurements of Blade-Vortex Interaction NoiseJournal of the American Helicopter Society, 1982
- Research on Model Helicopter Rotor Blade Slap at Moderate Tip SpeedsJournal of the American Helicopter Society, 1982
- Helicopter Noise: State-of-the-ArtJournal of Aircraft, 1978
- Some Conclusions from an Investigation of Blade‐Vortex InteractionJournal of the American Helicopter Society, 1975
- Some experimental results of the effect of a streamwise vortex on a two-dimensional wingThe Aeronautical Journal, 1974
- Helicopter Noise due to Blade-Vortex InteractionThe Journal of the Acoustical Society of America, 1971