| 引用本文: | 刘君,郭正.超音速外流与塞式喷管形成的干扰流场数值模拟.[J].国防科技大学学报,2000,22(5):15-18.[点击复制] |
| LIU Jun,GUO Zheng.Numerical Simulation of Plug Nozzle in Supersonic Flow[J].Journal of National University of Defense Technology,2000,22(5):15-18[点击复制] |
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| 超音速外流与塞式喷管形成的干扰流场数值模拟 |
| 刘君, 郭正 |
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(国防科技大学 航天与材料工程学院, 湖南 长沙 410073)
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| 摘要: |
| 从考虑了k-ε湍流模型和双组分气体模型的三维薄层近似 NS 方程出发, 采用高效 ENO 差分格式, 数值模拟了超音速空气外流与塞式喷管燃气形成的内外流干扰流场。部分计算结果与国外文献相比一致。在此基础上论证了应用计算流体力学开展塞式喷管研究的可行性。 |
| 关键词: 塞式喷管 异质喷流 数值模拟 ENO 格式 |
| DOI： |
| 投稿日期：1999-12-05 |
| 基金项目: |
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| Numerical Simulation of Plug Nozzle in Supersonic Flow |
| LIU Jun, GUO Zheng |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| Interaction of plug nozzle jets with supersonic external flow was simulated numerically based on 3-D TLA NS equations with ENO scheme, then the structure of the flow field was analyzed. Calculations were performed under two-component model in which the external flow was air and the jet was fuel gas. Turbulence was taken into account with a k-ε turbulence model. The results agreed well with the reference. |
| Keywords: plug nozzle two-component model jet numerical simulation ENO scheme |
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