On the generation and propagation of multiple pure tones inside turbofans at transonic regime
Author:
Affiliation:
1. ONERA
2. Snecma
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2014-3104
Reference12 articles.
1. Multiple tone generation by transonic compressors
2. Buzzsaw Noise Predictions for Modern Turbofans
3. ON THE PREDICTION OF “BUZZ-SAW” NOISE IN AERO-ENGINE INLET DUCTS
4. Prediction of the Spectral Content of Combination Tone Noise
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3. Nonlinear Propagation of Supersonic Fan Tones in Turbofan Intake Ducts;AIAA Journal;2018-01
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