United States National Aeronautics and Space Administration
United States National Aeronautics and Space Administration: Publications
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Document Type
Article
Date of this Version
9-1982
Citation
AIAA JOURNAL, VOL. 20, NO.9, SEPTEMBER 1982, pp. 1203-1211
Abstract
The applicability to practical calculations of recent theoretical developments in the stability analysis of difference approximations is examined for initial boundary-value problems of the hyperbolic type. For the numerical experiments the one-dimensional inviscid gasdynamic equations in conservation law form are selected. A class of implicit schemes based on linear multistep methods for ordinary differential equations is chosen and the use of space or space-time extrapolations as implicit or explicit boundary schemes is emphasized. Some numerical examples with various inflow-outflow conditions highlight the commonly discussed issues: explicit vs implicit boundary schemes, and unconditionally stable schemes.
Comments
U.S. government work