Numerical Simulation of Hypersonic Viscous Flow Around Space Shuttle With Method of Diffusion Analogy

Hypersonic viscous flow around a space shuttle with M_∞=7,Re=148000and angle of attack a=5°is simulated numerically with the special Jacobian matrix split-ting technique and simplified diffusion analogy method.With the simplified diffusion anal-ogy method the efficiency of computation and resolution...

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Veröffentlicht in:中国科学:数学英文版 1993 (9), p.1084-1094
1. Verfasser: 傅德薰 马延文
Format: Artikel
Sprache:eng
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Zusammenfassung:Hypersonic viscous flow around a space shuttle with M_∞=7,Re=148000and angle of attack a=5°is simulated numerically with the special Jacobian matrix split-ting technique and simplified diffusion analogy method.With the simplified diffusion anal-ogy method the efficiency of computation and resolution of the shock can be improved.
ISSN:1674-7283
1869-1862