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Physics-Informed Broadband Noise Source Identification and Prediction of an Ideally Twisted RotorThis work aims to provide a physics-based approach for the prediction and isolation of broadband noise emanating from different regions of an ideally twisted rotor. A preliminary prediction was conducted using a lattice-Boltzmann method–very-large-eddy simulation (LBM-VLES) implemented within the software suite, PowerFLOW. Regions of particular interest to broadband noise were investigated by calculating one-third octave sound pressure levels of the unsteady pressure fluctuations acting on the rotor. These regions were then treated as individual Ffowcs Williams and Hawkings (FW-H) surfaces and simulated for three run conditions at a finer spatial resolution to identify the broadband noise from these separate regions and isolate it from the total acoustic spectra. These predictions were then compared to experimentally acquired data and to semiempirical prediction methods to highlight the acoustic contributions of various broadband noise generation mechanisms as well as to exemplify and explain shortcomings in the semiempirical methodology.
Document ID
20205010085
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Christopher S Thurman
(Langley Research Center Hampton, Virginia, United States)
Nikolas S Zawodny
(Langley Research Center Hampton, Virginia, United States)
Nicole A Pettingill
(Langley Research Center Hampton, Virginia, United States)
Leonard V Lopes
(Langley Research Center Hampton, Virginia, United States)
James D Baeder
(University of Maryland, College Park College Park, Maryland, United States)
Date Acquired
November 13, 2020
Subject Category
Acoustics
Meeting Information
Meeting: AIAA SciTech Forum and Exposition
Location: Virtual
Country: US
Start Date: January 11, 2021
End Date: January 21, 2021
Sponsors: American Institute of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNL09AA00A
WBS: 664817.02.07.03.02.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
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