Applicability of Low-Fidelity Tonal and Broadband Noise Models on Small-Scaled Rotors
Author:
Affiliation:
1. University of California Davis
2. University of California San Diego
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2023-1547
Reference37 articles.
1. Sound generation by turbulence and surfaces in arbitrary motion
2. Turbulent boundary layer trailing-edge noise: Theory, computation, experiment, and application
3. Farassat, F. "Derivation of Formulations 1 and 1A of Farassat," Tech. Rep. NASA/TM-2007-214853, NASA Langley Research Center, 2007.
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