Shock Wave Generation and Radiation from a Turbofan Engine Under Flow Distortion
Author:
Affiliation:
1. ONERA–Paris Saclay University, F-92322 Châtillon, France
Funder
Cleansky
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Reference27 articles.
1. Turbofan Inlet Distortion Noise Prediction with a Hybrid CFD-CAA Approach
2. Impact of Turbofan Intake Distortion on Fan Noise Propagation and Generation
3. Inlet and Aft Tonal Noise Predictions of a Full-Scale Turbofan Engine with Bifurcation and Inlet Distortion
4. Effect of Distortion on Turbofan Tonal Noise at Cutback with Hybrid Methods
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1. CFD/CAA coupling for the prediction of fan tone noise propagation and radiation through a drooped intake;28th AIAA/CEAS Aeroacoustics 2022 Conference;2022-06-13
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3. Numerical assessment of fan noise confinement effects in a closed wind-tunnel;AIAA AVIATION 2021 FORUM;2021-07-28
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