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A second-order accurate kinetic-theory-based method for inviscid compressible flowsAn upwind method for the numerical solution of the Euler equations is presented. This method, called the kinetic numerical method (KNM), is based on the fact that the Euler equations are moments of the Boltzmann equation of the kinetic theory of gases when the distribution function is Maxwellian. The KNM consists of two phases, the convection phase and the collision phase. The method is unconditionally stable and explicit. It is highly vectorizable and can be easily made total variation diminishing for the distribution function by a suitable choice of the interpolation strategy. The method is applied to a one-dimensional shock-propagation problem and to a two-dimensional shock-reflection problem.
Document ID
19870009350
Acquisition Source
Legacy CDMS
Document Type
Technical Publication (TP)
Authors
Deshpande, Suresh M.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
December 1, 1986
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
L-16050
NASA-TP-2613
NAS 1.60:2613
Accession Number
87N18783
Funding Number(s)
PROJECT: RTOP 505-31-03-02
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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