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An approximate Riemann solver for thermal and chemical nonequilibrium flowsAmong the many methods available for the determination of inviscid fluxes across a surface of discontinuity, the flux-difference-splitting technique that employs Roe-averaged variables has been used extensively by the CFD community because of its simplicity and its ability to capture shocks exactly. This method, originally developed for perfect gas flows, has since been extended to equilibrium as well as nonequilibrium flows. Determination of the Roe-averaged variables for the case of a perfect gas flow is a simple task; however, for thermal and chemical nonequilibrium flows, some of the variables are not uniquely defined. Methods available in the literature to determine these variables seem to lack sound bases. The present paper describes a simple, yet accurate, method to determine all the variables for nonequilibrium flows in the Roe-average state. The basis for this method is the requirement that the Roe-averaged variables form a consistent set of thermodynamic variables. The present method satisfies the requirement that the square of the speed of sound be positive.
Document ID
19950008498
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Prabhu, Ramadas K.
(Lockheed Engineering and Sciences Co. Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1994
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-CR-195003
NAS 1.26:195003
Report Number: NASA-CR-195003
Report Number: NAS 1.26:195003
Accession Number
95N14912
Funding Number(s)
CONTRACT_GRANT: NAS1-19000
PROJECT: RTOP 232-01-04-06
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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