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A class of high resolution explicit and implicit shock-capturing methodsAn attempt is made to give a unified and generalized formulation of a class of high resolution, explicit and implicit shock capturing methods, and to illustrate their versatility in various steady and unsteady complex shock wave computations. Included is a systematic review of the basic design principle of the various related numerical methods. Special emphasis is on the construction of the basis nonlinear, spatially second and third order schemes for nonlinear scalar hyperbolic conservation laws and the methods of extending these nonlinear scalar schemes to nonlinear systems via the approximate Riemann solvers and the flux vector splitting approaches. Generalization of these methods to efficiently include equilibrium real gases and large systems of nonequilibrium flows are discussed. Some issues concerning the applicability of these methods that were designed for homogeneous hyperbolic conservation laws to problems containing stiff source terms and shock waves are also included. The performance of some of these schemes is illustrated by numerical examples for 1-, 2- and 3-dimensional gas dynamics problems.
Document ID
19890016281
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Yee, H. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1989
Subject Category
Numerical Analysis
Report/Patent Number
A-89091
NASA-TM-101088
NAS 1.15:101088
Report Number: A-89091
Report Number: NASA-TM-101088
Report Number: NAS 1.15:101088
Accession Number
89N25652
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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