CHINESE JOURNAL OF ENERGETIC MATERIALS
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固体发动机不同角度跌落数值模拟及试验分析
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作者单位:

1.海军航空大学飞行器工程系;2.内蒙动力机械研究所

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预研重点基金(9140A28010215JB14073)


Numerical Simulation and Experimental Analysis of Drop at Different Angle of Solid Rocket Motor
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Affiliation:

1.Department of Aircraft Engineering Naval Aviation University, Yantai 264001, China;2.The Dynamical & Mechanical Institute of Inner Mongolia, Hohhot 010000, China

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    摘要:

    为了研究某型舰载固体发动机跌落的安全性问题,应用ANSYS/LS-DYNA有限元分析软件对固体发动机37.5 m高度的多角度跌落过程进行数值模拟分析,并开展真实发动机的跌落试验进行验证。结果表明,相同跌落高度下的危险角度为78°,通过推进剂点火增长模型计算得出发动机内部装药温升小于5 K,不会发生点火反应,发动机尾部与碰撞面接触的位置相对危险,壳体与内部装药的应力、应变值较大,可能产生断裂破坏。通过固体发动机跌落试验发现,发动机的尾部出现断裂破坏,但未发生点火或爆炸反应,试验采集的数据信息与有限元分析的结果一致。

    Abstract:

    To study the drop safety problem of a certain type of ship board solid rocket motor, the numerical simulation and analysis for the multi angle drop process at drop height of 37.5 m of solid motor were carried out by using ANSYS/LS-DYNA finite element analysis software. The verified test for drop test of real motor was performed. The results show that the dangerous angle at the same drop height is 78°, the temperature rise of charge in the motor calculated by ignition and growth model is less than 5 K, and the ignition reaction does not happen. The contact position of motor tail with collision surface is relatively dangerous. The stress and strain values of shell and internal charge are large, which may generate fracture failure. Through the drop test of solid rocket motor, it is found that the tail of motor has a fracture damage, but the ignition or explosion reaction do not occur. Data information collected from the test is consistent with the results of finite element analysis. The rationality of the calculation method is verified.

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引用本文

杨明,黄卫东,沈伟,等.固体发动机不同角度跌落数值模拟及试验分析[J].含能材料, 2018, 26(9):726-731. DOI:10.11943/CJEM2018036.
YANG Ming, HUANG Wei-dong, SHEN Wei, et al. Numerical Simulation and Experimental Analysis of Drop at Different Angle of Solid Rocket Motor[J]. Chinese Journal of Energetic Materials, 2018, 26(9):726-731. DOI:10.11943/CJEM2018036.

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历史
  • 收稿日期: 2018-02-02
  • 最后修改日期: 2018-07-14
  • 录用日期: 2018-05-16
  • 在线发布日期: 2018-06-29
  • 出版日期: 2018-09-20