CHINESE JOURNAL OF ENERGETIC MATERIALS
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HTPB推进剂三点弯曲过程试验与数值模拟
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1.海军航空大学 研究生大队, 山东 烟台 264001;2.海军航空大学 导弹总体与发动机教研室, 山东 烟台 264001

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装备预研基金(9140A28010215JB14073)


Experimental and Numerical Simulation on the Damage Process of HTPB Propellant at the Crack Tip
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1.Graduate Students′ Brigade, Naval Aviation University, Yantai 264001, China;2.Teaching and Research Section of Missile Body and Engine, Naval Aviation University, Yantai 264001, China

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    摘要:

    为了研究端羟基聚丁二烯(HTPB)推进剂三点弯曲过程裂纹尖端细观损伤特点,采用扫描电镜对裂纹尖端动态损伤过程进行了观察。建立了基于子模型的推进剂三点弯曲多尺度模型,实现了三点弯曲试件宏观变形和裂纹尖端细观损伤的有效计算,并从试验和数值模拟两个角度分析了裂纹尖端损伤过程。结果表明:推进剂三点弯曲裂纹尖端损伤过程先是裂尖颗粒与基体脱湿,在裂纹尖端附近形成损伤区,随压缩位移的增加,不同颗粒脱湿引起的微裂纹与裂尖汇聚,使裂纹向前扩展;压缩过程中,由于裂纹尖端两端的拉伸作用使裂尖发生钝化。压缩位移从0增加至1.2 mm,裂纹张开位移从0增加至84.1 μm,并且随压缩位移的增加,其增加的速率也增大;数值模拟结果与试验结果吻合良好。建立的基于子模型的多尺度数值模型可以有效模拟推进剂三点弯曲试验宏观变形以及裂纹尖端细观损伤过程,为开展推进剂宏细观损伤过程分析提供了一种新方法。

    Abstract:

    To study the microscopic damage characteristics of crack tip in the three-point bending process of hydroxyl-terminated polybutadiene(HTPB) propellant, the dynamic damage process of crack tip was observed by scanning electron microscopy. Based on submodel of propellant, a multi-scale model of three-point bending process was established. The macroscopic deformation and meso-damage of crack tip during three-point bending process were calculated. The damage process of crack tip was analyzed by experiment and numerical simulation, respectively. The results show that the damage process of the three-point bending test is firstly the dewetting of the particles at crack tip, and then from the damage zone. With the increase of the compression displacement, the microcrack caused by the dewetting of different particles converges with crack tip to make the crack develop. Due to the tensile action at both sides of the crack, the crack tip becomes blunt. As the compression displacement increases from 0 to 1.2 mm, the crack opening displacement increases from 0 to 84.1 μm, and the increase rate is also increased. The numerical simulation results agree well with the experimental results. The multi-scale numerical model based on submodel can effectively simulate the macroscopic deformation of propellant on three-point bending process and the microscopic damage process of crack tip, which provides a new method for the analysis of macroscopic and microscopic damage process of propellant.

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引用本文

伍鹏,李高春,王鑫. HTPB推进剂三点弯曲过程试验与数值模拟[J].含能材料, 2020, 28(6):514-521. DOI:10.11943/CJEM2019187.
WU Peng, LI Gao-chun, WANG Xin. Experimental and Numerical Simulation on the Damage Process of HTPB Propellant at the Crack Tip[J]. Chinese Journal of Energetic Materials, 2020, 28(6):514-521. DOI:10.11943/CJEM2019187.

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历史
  • 收稿日期: 2019-07-01
  • 最后修改日期: 2019-11-11
  • 录用日期: 2019-09-20
  • 在线发布日期: 2019-11-05
  • 出版日期: 2020-06-25