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Direct simulation of compressible turbulence in a shear flowCompressibility effects on the turbulence in homogeneous shear flow are investigated. The growth of the turbulent kinetic energy was found to decrease with increasing Mach number: a phenomenon which is similar to the reduction of turbulent velocity intensities observed in experiments on supersonic free shear layers. An examination of the turbulent energy budget shows that both the compressible dissipation and the pressure-dilatation contribute to the decrease in the growth of kinetic energy. The pressure-dilatation is predominantly negative in homogeneous shear flow, in contrast to its predominantly positive behavior in isotropic turbulence. The different signs of the pressure-dilatation are explained by theoretical consideration of the equations for the pressure variance and density variance. Previously, the following results were obtained for isotropic turbulence: (1) the normalized compressible dissipation is of O(M(sub t)(exp 2)); and (2) there is approximate equipartition between the kinetic and potential energies associated with the fluctuating compressible mode. Both of these results were substantiated in the case of homogeneous shear. The dilatation field is significantly more skewed and intermittent than the vorticity field. Strong compressions seem to be more likely than strong expansions.
Document ID
19910010748
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Sarkar, S.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Erlebacher, G.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Hussaini, M. Y.
(Institute for Computer Applications in Science and Engineering Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1991
Subject Category
Aerodynamics
Report/Patent Number
AD-A234673
NASA-CR-187537
ICASE-91-29
NAS 1.26:187537
Report Number: AD-A234673
Report Number: NASA-CR-187537
Report Number: ICASE-91-29
Report Number: NAS 1.26:187537
Accession Number
91N20061
Funding Number(s)
PROJECT: RTOP 505-90-52-01
CONTRACT_GRANT: NAS1-18605
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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