NUMERICAL SIMULATION OF COMBUSTION PROCESS IN LRE TEST COMBUSTION CHAMBER

Wang Zhenguo; Zhou Jin; Yan Xiaoqing; Zhuang Fengchen

Volume 11 Issue 3

Jul. 1996

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Article Navigation > Journal of Aerospace Power > 1996 > 11(3): 277-280,331

Wang Zhenguo, Zhou Jin, Yan Xiaoqing, Zhuang Fengchen. NUMERICAL SIMULATION OF COMBUSTION PROCESS IN LRE TEST COMBUSTION CHAMBER[J]. Journal of Aerospace Power, 1996, 11(3): 277-280,331.

Citation:

Wang Zhenguo, Zhou Jin, Yan Xiaoqing, Zhuang Fengchen. NUMERICAL SIMULATION OF COMBUSTION PROCESS IN LRE TEST COMBUSTION CHAMBER[J]. Journal of Aerospace Power, 1996, 11(3): 277-280,331.

Wang Zhenguo, Zhou Jin, Yan Xiaoqing, Zhuang Fengchen. NUMERICAL SIMULATION OF COMBUSTION PROCESS IN LRE TEST COMBUSTION CHAMBER[J]. Journal of Aerospace Power, 1996, 11(3): 277-280,331.

Citation:

Wang Zhenguo, Zhou Jin, Yan Xiaoqing, Zhuang Fengchen. NUMERICAL SIMULATION OF COMBUSTION PROCESS IN LRE TEST COMBUSTION CHAMBER[J]. Journal of Aerospace Power, 1996, 11(3): 277-280,331.

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NUMERICAL SIMULATION OF COMBUSTION PROCESS IN LRE TEST COMBUSTION CHAMBER

1st Dept.National University of Defense Technology, Changsha 410073

Received Date: 1995-06-01
Rev Recd Date: 1996-01-01
Publish Date: 1996-07-28

Abstract

Abstract

Two-phase turbulent reacting flow model of the internal operating processes in Liquid Rocket Engine (LRE) is set up in non-orthogonal curvilinear coordinates.By means of this model,numerical simulation of the combustion flow process in LO x/GH 2 test rocket engine has been accomplished.From the simulation,velocity patterns,contour maps of gas species concentration,temperature,pressure,Mach number,combustion efficiency,and plots of wall temperature and average radiateion temperature,and plot of spray vaporization are obtained.
- Liquid propallant,
- Rocket engines,
- Combustion processes