固含量调控下复合固体推进剂蠕变行为的跨尺度分析与本构建模OA
Multiscale analysis and constitutive modeling of the creep behavior of composite solid propellants under solid content control
复合固体推进剂的蠕变行为直接影响固体发动机的长期贮存可靠性,固含量(颗粒体积分数)是其关键调控参数.通过细观-宏观跨尺度仿真分析方法,揭示固含量对蠕变行为的调控机制,并建立与之耦合的本构模型.首先,引入颗粒增强型弹性与黏性元件,构建了弹性模量和黏性系数随固含量显式变化的参数化本构方程;其次,基于高分辨率微CT 重构的真实细观结构,采用 Monte Carlo 算法生成了固含量 10.48%~50.42%的颗粒增强细观模型,并开展了 0.02~0.1 MPa 恒定应力下的跨尺度蠕变仿真.结果表明,随着固含量增加,初始弹性模量与有效黏性系数呈显著非线性增长,并且界面应力集中进一步加剧该非线性;固含量提升可有效抑制减速蠕变阶段应变速率,证实颗粒填充通过增强基体黏弹性阻尼改善了抗蠕变性能;基于仿真数据辨识本构模型参数的预测误差低于 7.5%,实现了宽固含量范围内蠕变行为的精准预测.
The creep behavior of composite solid propellants directly affects the long-term storage reliability of solid rocket motors,with solid content(particle volume fraction)acting as a key controlling parameter.A meso-macro cross-scale simulation approach was employed to elucidate the regulation mechanism of solid content on creep behavior and to establish a coupled constitutive model.First,particle-reinforced elastic and viscous elements were introduced,and a parameterized constitutive equation was constructed in which the elastic modulus and viscosity coefficient vary explicitly with solid content.Second,based on the real mesostructure reconstructed via high-resolution micro-CT,particle-reinforced mesoscale models with solid contents ranging from 10.48%to 50.42%were generated using a Monte Carlo algorithm,and cross-scale creep simulations were carried out under constant stresses of 0.02~0.1 MPa.The results show that with increasing solid content,the initial elastic modulus and effective viscosity coefficient exhibit a pronounced nonlinear increase,which is further intensified by interfacial stress concentration.Moreover,the increase in solid content effectively suppresses the strain rate in the decelerating creep stage,confirming that particle filling improves creep resistance by enhancing the viscoelastic damping of the matrix.The constitutive parameters are identified from the simulation data,and the prediction error is below 7.5%,enabling accurate prediction of creep behavior over a wide range of solid contents.
冯帅星;王学仁;马巨;周伟勇;卫海波;潘进
内蒙动力机械研究所,呼和浩特 010010火箭军工程大学,固体推进全国重点实验室,西安 710025内蒙动力机械研究所,呼和浩特 010010内蒙动力机械研究所,呼和浩特 010010内蒙动力机械研究所,呼和浩特 010010内蒙动力机械研究所,呼和浩特 010010
航空航天
复合固体推进剂蠕变行为固含量本构模型跨尺度分析
composite solid propellantcreep behaviorsolid contentconstitutive modelmultiscale analysis
《固体火箭技术》 2026 (3)
418-426,9
国家级项目.
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