Yan WANG, Jie FANG, Jinhui YANG, et al. Simulation study on combustion flow in low⁃pressure condition of hydrogen⁃oxygen torch ignitor[J]. Journal of Aerospace Power, 2021, 36(11): 2344-2352.
DOI:
Yan WANG, Jie FANG, Jinhui YANG, et al. Simulation study on combustion flow in low⁃pressure condition of hydrogen⁃oxygen torch ignitor[J]. Journal of Aerospace Power, 2021, 36(11): 2344-2352.DOI: 10.13224/j.cnki.jasp.20200552.
Simulation study on combustion flow in low⁃pressure condition of hydrogen⁃oxygen torch ignitor
The effects of hydrogen⁃oxygen injection interval and droplet mean diameter on the combustion flow of the low⁃temperature liquid hydrogen and liquid oxygen torch electric ignitor in low⁃pressure condition were investigated by numerical simulation.Discrete phase model(DPM) and 16⁃step,6 species hydrogen⁃oxygen chemical reaction mechanism were applied for the analysis.Considering the turbulent combustion effect,the eddy dissipation concept combustion model was utilized for simulation calculation.The temperature results obtained by simulation were in good agreement with those obtained by experiment,and the deviations of pressure were within 5%,thereby verifying the accuracy of the numerical models.As the results shown,under low⁃pressure condition,when the hydrogen⁃oxygen injection interval increased,the ignitor head inner wall temperature increased,the chamber pressure decreased,and the combustion length decreased.The larger liquid hydrogen droplets diameter resulted in the longer combustion length and higher head inner wall temperature,besides,the pressure in the ignitor chamber was slightly reduced.The diameter of liquid oxygen droplets had little effect on combustion flow of the ignitor.
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references
REPAS G A . Hydrogen‑oxygen torch ignitor [R]. NASA TM‑106493 , 1994 .
LIANG P Y . Modeling of SSME fuel preburner ASI [R].NASA N92 ‑32259 , 1992 .
OECHSLEIN W . Status of the Vinci combustion chamber vacuum ignition tests [R]. AIAA⁃2004⁃3531 , 2004 .
HENSEL C , WIEDMANN D , OECHSLEIN W , et al . Ignition aspects of the Vinci thrust chamber [R]. AIAA⁃2002⁃4008 , 2002 .
HENDERSON J , FOUST R . RL10⁃Three decades of H 2 /O 2 space engine evolution,capabilities for the future [R]. AIAA 91⁃3622 , 1991 .
WU Hongbin . Pyrotechnic igniters and electrical spark igniters for LOx/LH 2 rocket engines [J]. Missiles and Space Vehicles , 1994 ( 5 ): 32 ⁃ 42,76 . (in Chinese)
朱森元 . 氢氧火箭发动机及其低温技术 [M]. 北京 : 国防工业出版社 , 1995 .
ANOOP A , ASSIZ M P , MANU M J . Optimization of length of mixing zone in GH 2 ⁃GO 2 based torch igniter,applying numerical techniques [J]. Applied Mechanics and Materials , 2014 ,592/ 593 / 594 : 1692 ⁃ 1696 .
SUN Jiguo , WANG Jue . Experimental study on high mixture ratio torch ignitor [J]. Journal of Propulsion Tecnology , 2000 , 21 ( 1 ): 34 ⁃ 36 . (in Chinese)
GUO Tianli , SUN Huijuan . Orthogonal testing study on ignition energy of a torch ignition system [J]. Missiles and Space Vehicles , 2016 ( 2 ): 90 ⁃ 93,96 . (in Chinese)
YANG Jinhui , WANG Zhaohui , ZUO Anjun , et al . Combustion flow analysis of the hydrogen⁃oxygen torch igniter [J]. Missiles and Space Vehicles , 2019 , 368 ( 3 ): 45 ⁃ 48 . (in Chinese)
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