| 摘要: |
| 绕弹体的超声速气流与火箭发动机燃气喷流相互作用，在弹底部形成了复杂的干扰流场。应用四阶的ＭＵＳＣＬＴＶＤ格式，求解雷诺平均的Ｎ－Ｓ方程，对这一复杂流动进行了数值模拟，得到了流场结构随不同喷口压力比的变化规律。 |
| 关键词: 火箭发动机 超声速尾流 纳维尔－斯托克斯方程 数值模拟 尾流干扰 |
| DOI： |
| 分类号:V430 |
| 基金项目: |
|
| NUMERICAL STUDIES FOR INTERACTION FLOWFIELD BETWEEN SUPERSONIC FLOW AROUND BODY AND JET FLOW EXHAUSTING FROM ROCKET |
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Ju Yutao, Zheng Ya
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School of Machinery,Nanjing Univ.of Science and Technology,Nanjing,210094
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| Abstract: |
| The interaction between supersonic external flow and an exhaust jet forms a complex flowfield near the missile afterbody.The research about this interaction flows was completed with fourth order MUSCL TVD scheme to solve the Reynolds averaged N S equations.The flowfield structures observed and it’s relation with jet pressure ratio were obtained. |
| Key words: Rocket engine Supersonic wake Navier Stockes equations Numerical simulation Wake interaction |
