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复合固体推进剂损伤行为的多尺度研究进展OA北大核心CSTPCD

Multiscale Research Progress on Damage Behaviors of Composite Solid Propellants

中文摘要英文摘要

从微观、细观、宏观尺度和跨尺度4个方面,对复合固体推进剂损伤行为的研究进展进行了梳理,重点综述了不同尺度下损伤的观测和表征方法、损伤阈值的确定方法、损伤演化模型的构建方法、损伤数值模拟方法及宏细观跨尺度分析方法,并在此基础上针对当前研究中存在的若干不足,展望了需进一步重点开展研究的方向:拓宽微观尺度上开展复合固体推进剂损伤行为数值模拟时考虑的影响因素的范围,并从多个方面加强与试验研究结论的验证;提高细观尺度上损伤观测试验的能力、损伤演化模型的表征水平和损伤数值模拟的计算精度;提高宏观尺度上损伤识别测试试验的检测精度、损伤阈值确定方法的精确性和损伤演化模型的预测能力;在形成微细宏观单一尺度上复合固体推进剂损伤行为研究的标准规范的基础上,进一步建立推进剂损伤行为跨尺度研究的理论方法体系.

The damage behaviors of composite solid propellants were reviewed from four aspects:micro scale,meso scale,mac-ro scale and cross scale.During this process,the observation and characterization methods of damage at different scales,deter-mination methods for damage thresholds,construction methods for damage evolution models,numerical simulation methods for damage,and macro-mesoscopic cross-scale analysis methods were summarized.Based on this,to several shortcomings in cur-rent research,the future research directions that need to be further focused on are as follows:expanding the range of influencing factors to be considered in numerical simulation of damage behaviors for composite solid propellants at the microscale,and strengthening the verification of simulation results with experimental research conclusions from multiple aspects;improve the ob-servation ability of damage experiments at the meso scale,the characterization level of damage evolution models,and the com-putational accuracy of damage numerical simulations;improve the detection accuracy of damage identification testing at the macro scale,the accuracy of determination methods for damage thresholds,and the predictive ability of damage evolution mod-els;further establishing a theoretical method system for cross-scale study of the propellant damage behaviors based on the devel-oped standard specification for the study of damage behaviors for composite solid propellants in single-scale.

王哲君;强洪夫;王稼祥;裴书帝;李世奇;耿挺京;韩永恒

火箭军工程大学,陕西 西安 710025海军装备部驻北京地区军事代表局,北京 100071

武器工业

复合固体推进剂损伤观测损伤表征损伤模型数值模拟多尺度

composite solid propellantdamage observationdamage characterizationdamage modelnumerical simulationmultiscale

《含能材料》 2024 (004)

435-464 / 30

国家自然科学基金(22205259),陕西省高校科协青年人才托举项目(20190504) National Natural Science Foundation of China(No.22205259);The Youth Talent Promotion Plan of Shaanxi University Science and Technology Association(No.20190504)

10.11943/CJEM2024014

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