Aeroacoustic design of the Prop Fan
Author:
Affiliation:
1. United Technologies Corp., Hamilton Standard Div., Windsor Locks, Conn.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1979-610
Reference5 articles.
1. Near field noise of high tip speed propellers in forward flight
2. London Series A;Ffowcs-Williams J. E.,1969
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2. The effect of blade sweep on the reduction and enhancement of supersonic propeller noise;Journal of Fluid Mechanics;1995-06-25
3. Theoretical prediction of single rotation propeller noise;10th Aeroacoustics Conference;1986-07-09
4. Weakly nonlinear acoustic and shock-wave theory of the noise of advanced high-speed turbopropellers;Journal of Fluid Mechanics;1986-03
5. Aeroacoustics of an advanced propeller design under takekoff and landing conditions;Journal of Aircraft;1986-02
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