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 |
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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. |
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ISSN: | 1674-7283 1869-1862 |