Geometrical and numerical considerations in computing advanced-propeller noise
Author:
Affiliation:
1. Arizona State University, Tempe, Arizona 85287
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.46343
Reference15 articles.
1. Advanced turboprop noise prediction based on recent theoretical results
2. Near-field frequency - Domain theory for propeller noise
3. Thickness noise of a propeller and its relation to blade sweep
4. Shocks and singularities in the pressure field of a supersonically rotating propeller
5. Integrating the acoustic analogy for supersonic rotating surfaces
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1. New perspectives in the use of the Ffowcs Williams–Hawkings equation for aeroacoustic analysis of rotating blades;Journal of Fluid Mechanics;2007-01-03
2. ON SOME FUNDAMENTAL FLAWS IN PRESENT AEROACOUSTIC THEORY;Journal of Sound and Vibration;2000-05
3. Algorithm to Integrate the Ffowcs Williams-Hawkings Equation on Supersonic Rotating Domain;AIAA Journal;1999-09
4. COMPUTING AERODYNAMICALLY GENERATED NOISE;Annual Review of Fluid Mechanics;1997-01
5. Effects of asymmetric inflow on near-field propeller noise;AIAA Journal;1996-02
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