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A compressible Navier-Stokes code for turbulent flow modelingAn implicit, finite volume code for solving two dimensional, compressible turbulent flows is described. Second order upwind differencing of the inviscid terms of the equations is used to enhance stability and accuracy. A diagonal form of the implicit algorithm is used to improve efficiency. Several zero and two equation turbulence models are incorporated to study their impact on overall flow modeling accuracy. Applications to external and internal flows are discussed.
Document ID
19840013765
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Coakley, T. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 4, 2013
Publication Date
February 1, 1984
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
A-9669
NASA-TM-85899
NAS 1.15:85899
Accession Number
84N21833
Funding Number(s)
PROJECT: RTOP 505-51-11
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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