Resolvent analysis-based pressure modeling for trailing edge noise prediction-Reference-Cited by-同舟云学术

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Resolvent analysis-based pressure modeling for trailing edge noise prediction

Published:2019-05-18 Issue: Volume: Page:
ISSN:
Container-title:25th AIAA/CEAS Aeroacoustics Conference
language:
Short-container-title:

Author:

Wagner Georges A.¹,Deuse Mathieu¹,Illingworth Simon J.¹,Sandberg Richard D.¹

Affiliation:

1. University of Melbourne

Publisher

American Institute of Aeronautics and Astronautics

Reference39 articles.

1. Semi-Empirical Modeling of Turbulent Anisotropy for Airfoil Self-Noise Predictions

2. The influence of solid boundaries upon aerodynamic sound

3. Aerodynamic sound generation by turbulent flow in the vicinity of a scattering half plane

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Resolvent model for aeroacoustics of trailing edge noise;Theoretical and Computational Fluid Dynamics;2024-04

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