| 引用本文: | 赵文涛,庄逢辰,聂万胜.液体火箭发动机非线性燃烧不稳定过程的并行仿真.[J].国防科技大学学报,2002,24(4):5-8.[点击复制] |
| ZHAO Wentao,ZHUANG Fengchen,NIE Wansheng.Parallel Simulation Studies of Nonlinear Combustion Instabilities in Liquid Rocket Engine[J].Journal of National University of Defense Technology,2002,24(4):5-8[点击复制] |
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| 液体火箭发动机非线性燃烧不稳定过程的并行仿真 |
| 赵文涛1, 庄逢辰2, 聂万胜2 |
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(1.国防科技大学 计算机学院，湖南 长沙 410073;2.总装备部装备指挥技术学院，北京 101400)
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| 摘要: |
| 采用计算燃烧学方法对火箭发动机非线性燃烧不稳定工作过程进行了并行数值模拟。气相控制方程组用欧拉坐标系下的Navier-Stokes方程组描述，液相控制方程组在Lagrangian坐标系下进行描述。气、液两相作用通过方程组的源项互相耦合。编制了串行和并行程序，并在并行计算环境下进行了测试。从计算结果可以看出并行计算的效率较高。 |
| 关键词: 并行计算 非线性燃烧过程 液体火箭发动机 |
| DOI： |
| 投稿日期：2002-03-21 |
| 基金项目:国家自然科学基金资助项目(50176054) |
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| Parallel Simulation Studies of Nonlinear Combustion Instabilities in Liquid Rocket Engine |
| ZHAO Wentao1, ZHUANG Fengchen2, NIE Wansheng2 |
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(1.College of Computer, National Univ. of Defense Technology, Changsha 410073, China;2.Institute of Command and Technology of Equipment,Beijing 101400,China)
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| Abstract: |
| The nonlinear combustion instability process in liquid rocket engine is simulated. The gas controlling Navier-Stokes equations are described under the Euler coordinate.The liquid phase controlling equations are described under the Lagrangian coordinate.The two phase influences of gas and liquid are through the sources of equations.The sequential and parallel codes are written,and the codes are tested in parallel virtual machine environment.The results show that the parallel computation efficiency is reeasonably high. |
| Keywords: parallel computation nonlinear combustion process liquid rocket engine |
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