Numerical simulation of burning gas flow during vertical launch of a rocket

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作者：
Nanjing Univ of Science and, Technology, Nanjing, China [1 ]
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来源：
Tuijin Jishu | / 1卷 / 61-65期
关键词：
Combustion - Computer simulation - Launching - Nozzles - Shock waves;
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摘要：
The second order accurate MUSCL scheme was employed. The scheme is suitable for the calculation in Eulerian coordinates on monotonicity condition, and some dissipation mechanisms were introduced. The computed results showed that the shock wave structure in interaction flowfield is very clear and agrees well with the observation in experiments.
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