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Computation of turbulent high speed mixing layers using a two-equation turbulence modelA two-equation turbulence model was extended to be applicable for compressible flows. A compressibility correction based on modelling the dilational terms in the Reynolds stress equations were included in the model. The model is used in conjunction with the SPARK code for the computation of high speed mixing layers. The observed trend of decreasing growth rate with increasing convective Mach number in compressible mixing layers is well predicted by the model. The predictions agree well with the experimental data and the results from a compressible Reynolds stress model. The present model appears to be well suited for the study of compressible free shear flows. Preliminary results obtained for the reacting mixing layers are included.
Document ID
19910011771
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Narayan, J. R.
(Analytical Services and Materials, Inc., Hampton VA., United States)
Sekar, B.
(Vigyan Research Associates, Inc., Hampton VA., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1991
Publication Information
Publication: NASA, Lewis Research Center, Computational Fluid Dynamics Symposium on Aeropropulsion
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
91N21084
Funding Number(s)
CONTRACT_GRANT: NAS1-18599
CONTRACT_GRANT: NAS1-18585
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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