Technical Notes: Reduction of Blade‐Vortex Interaction Noise Through Higher Harmonic Pitch Control
- 1 January 1990
- journal article
- Published by AHS International dba Vertical Flight Society in Journal of the American Helicopter Society
- Vol. 35 (1) , 86-91
- https://doi.org/10.4050/jahs.35.86
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- Rotor blade-vortex interaction impulsive noise source identificationand correlation with rotor wake predictionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Concepts for reduction of blade/vortex interaction noiseJournal of Aircraft, 1987