Experimental Validation of Lifting Surface Theory for Rotor-Stator Interaction Noise Generation
Author:
Affiliation:
1. National Aerospace Laboratory NLR, 8300 AD Emmeloord, The Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/2.493
Reference12 articles.
1. 2Schulten, J. B. H. M. “Sound Generation by Ducted Fans and Propellers as a Lifting Surface Problem,” Ph.D. Thesis, Dept. of Applied Mathematics,Univ. of Twente, Enschede, The Netherlands,Feb. 1993.
2. Experimental validation of a lifting surface model for rotor wake-stator interaction
3. Stator vane response due to the impingement of the wake of an unloaded rotor
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