Inlet and Aft Tonal Noise Predictions of a Full-Scale Turbofan Engine with Bifurcation and Inlet Distortion
Author:
Affiliation:
1. United Technologies Corporation
2. Pratt & Whitney
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3034
Reference25 articles.
1. Aeropropulsion for Commercial Aviation in the Twenty-First Century and Research Directions Needed
2. The Effect of Steady Flow Distortion on Noise Propagation in Turbofan Intakes
3. Effects of Bifurcations on Aft-Fan Engine Nacelle Noise
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