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Broadband Noise Prediction When Turbulence Simulation Is Available - Derivation of Formulation 2B and Its Statistical AnalysisWe show that a simple modification of Formulation 1 of Farassat results in a new analytic expression that is highly suitable for broadband noise prediction when extensive turbulence simulation is available. This result satisfies all the stringent requirements, such as permitting the use of the exact geometry and kinematics of the moving body, that we have set as our goal in the derivation of useful acoustic formulas for the prediction of rotating blade and airframe noise. We also derive a simple analytic expression for the autocorrelation of the acoustic pressure that is valid in the near and far fields. Our analysis is based on the time integral of the acoustic pressure that can easily be obtained at any resolution for any observer time interval and digitally analyzed for broadband noise prediction. We have named this result as Formulation 2B of Farassat. One significant consequence of Formulation 2B is the derivation of the acoustic velocity potential for the thickness and loading terms of the Ffowcs Williams-Hawkings (FW-H) equation. This will greatly enhance the usefulness of the Fast Scattering Code (FSC) by providing a high fidelity boundary condition input for scattering predictions.
Document ID
20120008645
Acquisition Source
Langley Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Farassat, Fereidoun
(NASA Langley Research Center Hampton, VA, United States)
Casper, Jay H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 25, 2013
Publication Date
January 1, 2012
Subject Category
Acoustics
Report/Patent Number
NF1676L-12184
Funding Number(s)
WBS: WBS 877868.02.07.07.04.03.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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