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Computing aerodynamic sound using advanced statistical turbulence theoriesIt is noted that the calculation of turbulence-generated aerodynamic sound requires knowledge of the spatial and temporal variation of Q sub ij (xi sub k, tau), the two-point, two-time turbulent velocity correlations. A technique is presented to obtain an approximate form of these correlations based on closure of the Reynolds stress equations by modeling of higher order terms. The governing equations for Q sub ij are first developed for a general flow. The case of homogeneous, stationary turbulence in a unidirectional constant shear mean flow is then assumed. The required closure form for Q sub ij is selected which is capable of qualitatively reproducing experimentally observed behavior. This form contains separation time dependent scale factors as parameters and depends explicitly on spatial separation. The approximate forms of Q sub ij are used in the differential equations and integral moments are taken over the spatial domain. The velocity correlations are used in the Lighthill theory of aerodynamic sound by assuming normal joint probability.
Document ID
19810019347
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hecht, A. M.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Teske, M. E.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Bilanin, A. J.
(Continuum Dynamics, Inc. Princeton, NJ, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1981
Subject Category
Acoustics
Report/Patent Number
NASA-CR-165697
Report Number: NASA-CR-165697
Accession Number
81N27885
Funding Number(s)
CONTRACT_GRANT: NAS1-15937
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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