Surrogate Model-Based Acoustic Optimisation of Jet Nozzle Exit Geometry
Author:
Affiliation:
1. University of Bristol
2. Queen Mary University of London
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0683
Reference29 articles.
1. Directional Suppression of Noise from a High-Speed Jet
2. Parametric Testing of Chevrons on Single Flow Hot Jets
3. New Method for Jet Noise Reduction in Turbofan Engines
4. Installed jet-flap impingement tonal noise
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1. A Dynamical System Method for Finding Flow Structures from Jet LES Data;30th AIAA/CEAS Aeroacoustics Conference (2024);2024-05-30
2. Influence of Nozzle Geometry on Jet mixing and Jet Installation Noise;AIAA SCITECH 2023 Forum;2023-01-19
3. Robustness of Reduced-Order Jet Noise Models;AIAA Journal;2023-01
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