Interaction of rotor tip flow irregularities with stator vanes as a noise source
Author:
Affiliation:
1. NASA, Lewis Research Center, Cleveland, Ohio
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1977-1342
Reference31 articles.
1. Effects of forward velocity and acoustic treatment on inlet fan noise
2. Widnall, S. 'Helicopter Noise Due to Blade-Vortex Interaction,' Journal of the Acoustical Society America, Vol.50, July 1971, pp.354-365.
3. Rotating blades and aerodynamic sound
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