Data-driven Empirical Wall pressure Spectrum Models for Fan Noise Prediction
Author:
Affiliation:
1. The University of Melbourne
2. Universite de Sherbrooke Faculte de Genie
3. Michigan State University
4. Indian Institute of Technology Kanpur
5. Ecole de technologie superieure
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-3508
Reference40 articles.
1. Turbulent boundary layer trailing-edge noise: Theory, computation, experiment, and application
2. Direct numerical simulation of turbulent flow past a trailing edge and the associated noise generation
3. Trailing-edge broadband noise prediction of an airfoil with boundary-layer tripping
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1. On the physical structure, modelling and computation-based prediction of two-dimensional, smooth-wall turbulent boundary layers subjected to streamwise pressure gradients;Journal of Turbulence;2024-08-19
2. Artificial Neural Networks Prediction of Wall-Pressure Spectrum;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
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