Frequency-domain method for the computation of propeller acoustics
Author:
Affiliation:
1. National Aerospace Laboratory NLR, Amsterdam, the Netherlands
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.10008
Reference18 articles.
1. Benefits of blade sweep for advanced turboprops
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5. On sound generated aerodynamically I. General theory
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