Numerical simulation of hypersonic viscous flow around space shuttle with method of diffusion analogy
Data(s) |
1993
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Resumo |
Hypersonic viscous flow around a space shuttle with M(infinity) = 7, Re = 148000 and angle of attack alpha = 5-degrees is simulated numerically with the special Jacobian matrix splitting technique and simplified diffusion analogy method. With the simplified diffusion analogy method the efficiency of computation and resolution of the shock can be improved. |
Identificador | |
Idioma(s) |
英语 |
Fonte |
Science In China Series A-Mathematics Physics Astronomy.1993,36(9):1084-1094 |
Palavras-Chave | #Spabe Shuttle #Numerical Simulation #Diffusion Analogy #Shock Capturing |
Tipo |
期刊论文 |