发射过程中混合燃料介质内孔隙的绝热压缩

张奇 纪艳华 白春华 闫华 赵永涛 罗艾民 付智敏

张奇, 纪艳华, 白春华, 闫华, 赵永涛, 罗艾民, 付智敏. 发射过程中混合燃料介质内孔隙的绝热压缩[J]. 高压物理学报, 2004, 18(3): 237-244 . doi: 10.11858/gywlxb.2004.03.008
引用本文: 张奇, 纪艳华, 白春华, 闫华, 赵永涛, 罗艾民, 付智敏. 发射过程中混合燃料介质内孔隙的绝热压缩[J]. 高压物理学报, 2004, 18(3): 237-244 . doi: 10.11858/gywlxb.2004.03.008
ZHANG Qi, JI Yan-Hua, BAI Chun-Hua, YAN Hua, ZHAO Yong-Tao, LUO Ai-Min, FU Zhi-Min. Adiabatic Compression of Pores in Mixed Fuel Medium During Launching[J]. Chinese Journal of High Pressure Physics, 2004, 18(3): 237-244 . doi: 10.11858/gywlxb.2004.03.008
Citation: ZHANG Qi, JI Yan-Hua, BAI Chun-Hua, YAN Hua, ZHAO Yong-Tao, LUO Ai-Min, FU Zhi-Min. Adiabatic Compression of Pores in Mixed Fuel Medium During Launching[J]. Chinese Journal of High Pressure Physics, 2004, 18(3): 237-244 . doi: 10.11858/gywlxb.2004.03.008

发射过程中混合燃料介质内孔隙的绝热压缩

doi: 10.11858/gywlxb.2004.03.008
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    通讯作者:

    张奇

Adiabatic Compression of Pores in Mixed Fuel Medium During Launching

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    Corresponding author: ZHANG Qi
  • 摘要: 燃料空气炸药武器战斗部装填的云爆剂一般是固液混合态,固液混合药剂介质内部难免存在孔隙,孔隙尺度对发射安全性有重要影响。通过对孔隙压缩物理过程的理论分析,研究孔隙尺度对混合燃料发射安全性的影响,建立了相应的判别准则,给出发射过载加速度、混合燃料介质内孔隙尺度、孔隙绝热压缩温度之间的定量关系,并提出了发射模拟装置设计应考虑战斗部内装药缺陷的有关参数,给出相应的设计依据。固液混合燃料介质内孔隙的尺度越小,其压缩产生的温度越低,抗过载能力就越强。如果圆形孔隙的直径为70 m,在发射过载加速度为100 km/s2 的情况下,孔隙压缩产生的最高温度约573 K。将该值与固液混合药剂能够承受的临界温度进行比较,就可判断药剂在发射过载过程中的安全性。

     

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出版历程
  • 收稿日期:  2003-10-08
  • 修回日期:  2004-01-05
  • 发布日期:  2004-09-05

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