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Simulation and modeling of homogeneous, compressed turbulenceLow Reynolds number homogeneous turbulence undergoing low Mach number isotropic and one-dimensional compression was simulated by numerically solving the Navier-Stokes equations. The numerical simulations were performed on a CYBER 205 computer using a 64 x 64 x 64 mesh. A spectral method was used for spatial differencing and the second-order Runge-Kutta method for time advancement. A variety of statistical information was extracted from the computed flow fields. These include three-dimensional energy and dissipation spectra, two-point velocity correlations, one-dimensional energy spectra, turbulent kinetic energy and its dissipation rate, integral length scales, Taylor microscales, and Kolmogorov length scale. Results from the simulated flow fields were used to test one-point closure, two-equation models. A new one-point-closure, three-equation turbulence model which accounts for the effect of compression is proposed. The new model accurately calculates four types of flows (isotropic decay, isotropic compression, one-dimensional compression, and axisymmetric expansion flows) for a wide range of strain rates.
Document ID
19860021486
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Wu, C. T.
(Stanford Univ. CA, United States)
Ferziger, J. H.
(Stanford Univ. CA, United States)
Chapman, D. R.
(Stanford Univ. CA, United States)
Date Acquired
September 5, 2013
Publication Date
May 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NAS 1.26:176939
NASA-CR-176939
SU-TF-21
Accession Number
86N30958
Funding Number(s)
CONTRACT_GRANT: NCC2-15
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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