HTPB推进剂单向拉伸过程的分子动力学模拟OA
Molecular Dynamics Simulation of Uniaxial Tensile Process of HTPB Propellant
为研究拉伸载荷下端羟基聚丁二烯(hydroxyl-terminated polybutadiene,HTPB)推进剂的微观损伤,建立高氯酸铵(ammonium perchlorate,AP)/HTPB 和 AP/HTPB/AP界面模型.基于经典分子动力学方法计算单向拉伸时界面模型的变形和失效行为,分析温度对界面模型力学性能的影响,得到界面模型的应力应变曲线和能量变化曲线.计算结果表明:在轴向载荷的作用下 HTPB 层内部会出现微空穴,随着应变的增加微空穴合并,界面模型的最终失效位置在界面附近.界面模型的名义应力应变曲线可分为近似线弹性、屈服、应力强化和界面失效 4 阶段.随着温度的升高,界面模型的失效应力减小,延伸率无明显变化.
In order to investigate the micro-damage of hydroxyl-terminated polybutadiene(HTPB)propellant under tensile loading,interface models of ammonium perchlorate(AP)/HTPB and AP/HTPB/AP were established.Based on classical molecular dynamics,the deformation and failure behavior of the interface models under uniaxial tension were calculated.The influence of temperature on the mechanical properties of the interface models was analyzed,and the stress-strain curves and energy change curves of the interface models were obtained.The calculation results showed that micro cavities would appear inside the HTPB layer under axial loading.As the strain increased,the micro cavities merged,and the final failure location of the interface model was near the interface.The nominal stress-strain curve of the interface model could be divided into four stages:approximately linear elastic,yield,stress strengthening,and interface failure.As the temperature increased,the failure stress of the interface model decreased,and the elongation rate showed no significant change.
李金飞;曲凯;孟超;庄振民
海军航空大学,山东 烟台 264001海军航空大学,山东 烟台 264001海军航空大学,山东 烟台 264001海军航空大学,山东 烟台 264001
军事科技
HTPB推进剂分子动力学单向拉伸界面失效应力应变
HTPB propellantmolecular dynamicsuniaxial tensioninterfacial failurestress-strain
《兵工自动化》 2026 (1)
5-10,6
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