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CAG12 - A CSCM based procedure for flow of an equilibrium chemically reacting gasThe Conservative Supra Characteristic Method (CSCM), an implicit upwind Navier-Stokes algorithm, is extended to the numerical simulation of flows in chemical equilibrium. The resulting computer code known as Chemistry and Gasdynamics Implicit - Version 2 (CAG12) is described. First-order accurate results are presented for inviscid and viscous Mach 20 flows of air past a hemisphere-cylinder. The solution procedure captures the bow shock in a chemically reacting gas, a technique that is needed for simulating high altitude, rarefied flows. In an initial effort to validate the code, the inviscid results are compared with published gasdynamic and chemistry solutions and satisfactorily agreement is obtained.
Document ID
19850056794
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Green, M. J.
(NASA Ames Research Center Moffett Field, CA, United States)
Davy, W. C.
(NASA Ames Research Center Computational Chemistry and Aerothermodynamics Branch, Moffett Field, CA, United States)
Lombard, C. K.
(PEDA Corp. Palo Alto, CA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 85-0927
Accession Number
85A38945
Distribution Limits
Public
Copyright
Other

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