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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