Part-Span Approximation of Tone Noise Propagation in an Aeroengine Intake. Part 2: Non-Linear Propagation
Author:
Affiliation:
1. University of Southampton Institute of Sound and Vibration Research
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3073
Reference35 articles.
1. Turbomachinery Noise Predictions: Present and Future
2. Binns, J. S. P., Wu, L., and Wilson, A. G. "Part-Span Approximation of Tone Noise Propagation in an Aeroengine Intake. Part I:LinearPropagation,"30thAIAA/CEASAeroacousticsConference,2024,2024.
3. Shock-Wave Radiation from a Supersonic Ducted Rotor
4. McAlpine, A., and Fisher, M. J. "On the prediction of "Buzz-saw" noise in aero-engine inlet ducts,"Journal of Sound and Vibration,Vol.248,No.1,2001,pp.123-149. https://doi.org/10.1006/jsvi.2001.3770.
5. A new look at the generation of buzz-saw noise
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