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气助式直接喷射喷油器动态喷雾场数值模拟及试验

程强 张振东 谢乃流

程强, 张振东, 谢乃流. 气助式直接喷射喷油器动态喷雾场数值模拟及试验[J]. 航空动力学报, 2013, 28(11): 2430-2439.
引用本文: 程强, 张振东, 谢乃流. 气助式直接喷射喷油器动态喷雾场数值模拟及试验[J]. 航空动力学报, 2013, 28(11): 2430-2439.
CHENG Qiang, ZHANG Zhen-dong, XIE Nai-liu. Numerical simulation and experiment on air-assisted direct injection injector dynamic spray field[J]. Journal of Aerospace Power, 2013, 28(11): 2430-2439.
Citation: CHENG Qiang, ZHANG Zhen-dong, XIE Nai-liu. Numerical simulation and experiment on air-assisted direct injection injector dynamic spray field[J]. Journal of Aerospace Power, 2013, 28(11): 2430-2439.

气助式直接喷射喷油器动态喷雾场数值模拟及试验

基金项目: 国家自然科学基金(51275309);上海市教委科研创新项目(13YZ110);上海市研究生创新基金(JWCXSL1201);上海工程技术大学校基金项目(2011xy28)

Numerical simulation and experiment on air-assisted direct injection injector dynamic spray field

  • 摘要: 为了研究小型飞机发动机气助式直接喷射(air-assisted direct injection,AADI)喷油器喷雾形态及发展规律,采用数值模拟和高速摄影技术对其动态喷雾场进行研究.以锥阀运动的物理学模型为数值计算的移动边界条件,结合动网格技术对AADI喷油器动态喷雾场的速度分布、静动压分布和不同时刻雾化颗粒的空间分布进行动态数值模拟分析.以0.2ms为步长,对3.0ms内不同锥阀开启时刻的喷雾形态、雾化颗粒和贯穿距离进行了试验和仿真对比分析.结果表明:采用CFD仿真模拟技术可对AADI喷油器动态喷雾场的速度分布、压力分布、喷雾形态等参数进行定性分析,有利于揭示喷雾的发展规律,同时通过对喷雾粒径和贯穿距离的定量对比分析,表明了仿真计算的精确性,数值模拟计算与试验结果误差小于5%,满足工程应用的要求.

     

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出版历程
  • 收稿日期:  2013-04-11
  • 刊出日期:  2013-11-28

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