CHINESE JOURNAL OF ENERGETIC MATERIALS
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固体火箭发动机粘接界面蠕变损伤研究进展
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火箭军工程大学导弹工程学院, 陕西 西安 710025

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国家自然科学基金资助(11772352)


Research Progress on Bonding Interface Creep Damage in Solid Rocket Motors
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School of Missile Engineering, Rocket Force University of Engineering, Xi''an 710025, China

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    摘要:

    固体火箭发动机粘接界面在长期立式贮存下因蠕变效应产生损伤。本文从蠕变条件下界面损伤影响因素、界面损伤测试试验和界面损伤数值模拟3个方面综述了相关研究进展,指出了蠕变条件下粘接界面累积损伤不容忽视,总结了试验和数值模拟研究中的不足,并进行了展望。分析认为,试验研究的难点是设计合理的试验和选取有效表征损伤时效性的变量,数值模拟研究的重点是构建含损伤的蠕变型界面内聚力本构模型,以期为开展贮存条件下粘接界面的性能评估研究提供一定参考。

    Abstract:

    The bonding interface of solid rocket motor will be damaged due to the creep effect from long-term vertical storage. This paper reviews the relevant research progress from three perspectives as the influencing factors of interface damage under creep condition, interface damage test, and numerical simulation of interface damage. It emphasizes that the cumulative damage of bonding interface under creep condition cannot be ignored, summarizes the shortcomings of test and numerical simulation research, and makes a prospect. According to the findings, the most difficult aspect of experimental research is devising reasonable tests and selecting variables that effectively characterize the timeliness of damage. The focus of numerical simulation research is to build a creep interface cohesion model with damage, in order to provide some reference for the performance evaluation of bonding interface under storage conditions.

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李康佳,强洪夫,王哲君,等.固体火箭发动机粘接界面蠕变损伤研究进展[J].含能材料, 2022, 30(8):861-871. DOI:10.11943/CJEM2022125.
LI Kang-jia, QIANG Hong-fu, WANG Zhe-jun, et al. Research Progress on Bonding Interface Creep Damage in Solid Rocket Motors[J]. Chinese Journal of Energetic Materials, 2022, 30(8):861-871. DOI:10.11943/CJEM2022125.

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历史
  • 收稿日期: 2022-05-11
  • 最后修改日期: 2022-07-22
  • 录用日期: 2022-07-18
  • 在线发布日期: 2022-07-18
  • 出版日期: 2022-08-25