A Data-Driven Method for Stall Noise Predictions-Reference-Cited by-同舟云学术

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A Data-Driven Method for Stall Noise Predictions

Published:2024-05-30 Issue: Volume:2023 Page:
ISSN:
Container-title:30th AIAA/CEAS Aeroacoustics Conference (2024)
language:
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Author:

Ghiglino Aurelien¹,Zhou Beckett Y.²,Branch John²,Zang Bin²,Azarpeyvand Mahdi²,Rendon Jose³,Moreau Stephane³

Affiliation:

1. Stanford University

2. University of Bristol

3. Universite de Sherbrooke

Publisher

American Institute of Aeronautics and Astronautics

Link

https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3128

Reference47 articles.

1. Brooks, T. F., Pope, D. S., and Marcolini, M. A. "Airfoil self-noise and prediction," Tech. Rep. 19890016302, National AeronauticsandSpaceAdministration,1989.

2. Noise due to turbulent flow past a trailing edge

3. Mccullough,G.B.,andGault,D.E."Examplesofthreerepresentativetypesofairfoil-sectionstallatlowspeed,"Tech.rep., 1951.

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