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Self-ignition characteristics of the high-speed ramjet kinetic energy projectile in the launch process 被引量:1
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作者 Changfei ZHUO Haotian CHEN +1 位作者 Wenjin YAO Xiaoming WANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2019年第4期851-860,共10页
To research the self-ignition characteristics of high-speed ramjet kinetic energy projectile in the launch process, the self-ignition process based on the solid fuel of polyethylene was numerically simulated by using ... To research the self-ignition characteristics of high-speed ramjet kinetic energy projectile in the launch process, the self-ignition process based on the solid fuel of polyethylene was numerically simulated by using the dynamic grid technology. The effect of different muzzle velocity on the self-ignition performance, and the effect of opening the blockage at different times on the flow field stability of the combustion chamber and the flow field characteristics after the solid fuel ramjet stabilized were analyzed. The results show that the occurrence of self-ignition is not only related to the pressure, temperature in the combustion chamber, and the muzzle velocity, but also to the content of C_2H_4 and its degree of mixing with air in the combustion chamber. After the kinetic energy projectile gets out of the muzzle and before the blockage opens, there is oscillation occurring in the combustion chamber. The higher the muzzle velocity of the kinetic energy projectile, the more prone to the occurrence of the self-ignition and the negative effects can be avoided due to the pressure oscillation in the combustion chamber. The effect of opening the blockage at different times on the flow field stability after the self-ignition occurs in a period of time is weak. After the blockage opens, the solid fuel ramjet can reach a stable working condition quickly. 展开更多
关键词 Dynamic grid kinetic energy projectile Muzzle velocity SELF-IGNITION Solid fuel ramjet
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聚乙烯在高速冲压推进动能弹中的燃烧特性数值模拟
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作者 卓长飞 邹延兵 王晓鸣 《含能材料》 EI CAS CSCD 北大核心 2016年第11期1057-1062,共6页
为了研究聚乙烯在高速冲压推进动能弹中的燃烧特性,进行了高速冲压推进动能弹全弹一体化流场的数值模拟研究,分析了冲压发动机工作和非工作时流动特性差异,以及冲压发动机工作时聚乙烯的燃烧和推进特性。结果表明,冲压发动机工作时,燃... 为了研究聚乙烯在高速冲压推进动能弹中的燃烧特性,进行了高速冲压推进动能弹全弹一体化流场的数值模拟研究,分析了冲压发动机工作和非工作时流动特性差异,以及冲压发动机工作时聚乙烯的燃烧和推进特性。结果表明,冲压发动机工作时,燃烧室内压力均匀,中心轴线平均压力约为2.1MPa。随着轴向距离x的增大,火焰锋面先靠近固体燃料表面后逐渐远离。在再附着点之前,随着轴向距离x的增大,固体燃料的表面温度与燃面退移速率均持续增大,在再附着点附近达到最大值,然后不断减小。在本研究设计的气动构型下,高速冲压推进动能弹产生的额定推力、净推力分别为250N和76N,基于燃料的比冲为10593m·s^(-1)。 展开更多
关键词 固体燃料冲压发动机 动能弹 聚乙烯 燃烧特性
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高速冲压推进动能弹自点火工作过程数值模拟研究 被引量:1
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作者 邹延兵 卓长飞 封锋 《含能材料》 EI CAS CSCD 北大核心 2017年第1期12-19,共8页
为了研究高速冲压推进动能弹在自点火过程中的工作特性,数值模拟了基于聚乙烯为固体燃料的高速冲压推进动能弹自点火过程,分析了自点火过程中的点火延迟时间,喷管出口堵盖打开前燃烧室的流场变化规律,以及堵盖打开火焰稳定后燃烧室流场... 为了研究高速冲压推进动能弹在自点火过程中的工作特性,数值模拟了基于聚乙烯为固体燃料的高速冲压推进动能弹自点火过程,分析了自点火过程中的点火延迟时间,喷管出口堵盖打开前燃烧室的流场变化规律,以及堵盖打开火焰稳定后燃烧室流场变化规律和全弹性能。结果表明:高速冲压推进动能弹由于其初始的独特结构(喷管出口堵塞),点火延迟时间短,自点火能够成功进行;堵盖打开前,燃烧室压力发生了剧烈的振荡,并且燃烧室内化学反应增强了振荡效应;堵盖打开并且燃烧室火焰稳定后,高速冲压推进动能弹的额定推力为283 N,净推力为83 N,基于聚乙烯燃料的比冲为9129 m·s-1。 展开更多
关键词 固体燃料冲压发动机 高速冲压推进动能弹 聚乙烯 自点火 点火延迟
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