Acoustic Energy Exchange Between Frequencies During Non-Linear Propagation of Shock Waves
Author:
Affiliation:
1. Office National d'Etudes et de Recherches Aerospatiales
2. Airbus Operations SAS
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2024-3424
Reference19 articles.
1. Impact of Turbofan Intake Distortion on Fan Noise Propagation and Generation
2. Tones from an Aero-Engine Fan: Comparison between Harmonic-Balance Simulation and Experiment
3. Milidonis,K.F.,Hynes,T.,Doherty,M.,and Namgoong,H."The EffectofSteady IntakeDistortiononFanMPTNoiseUnder SidelineFlightConditions,"24thAIAA/CEASAeroacousticsConference,2018. doi:https://doi.org/10.2514/6.2018-4188.
4. Winkler,J.,Reimann,C.A.,Reba,R.A.,andGilson,J."TurbofanInletDistortionNoisePredictionwithaHybridCFD-CAA Approach,"20thAIAA/CEASAeroacousticsConference,2014. doi:https://doi.org/10.2514/6.2014-3102.
5. Inlet and Aft Tonal Noise Predictions of a Full-Scale Turbofan Engine with Bifurcation and Inlet Distortion
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