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用于固体火箭发动机的氢氧化铝增强三元乙丙橡胶涂层的速率依赖性拉伸性能

Rate-Dependent Tensile Properties of Aluminum-Hydroxide-Enhanced Ethylene Propylene Diene Monomer Coatings for Solid Rocket Motors.

作者信息

Wang Ran, Zhang Yiming, Wang Ningfei, Wu Yi

机构信息

School of Aerospace Engineering, Beijing Institute of Technology, Beijing 100081, China.

Chongqing Innovation Center, Beijing Institute of Technology, Chongqing 401120, China.

出版信息

Materials (Basel). 2024 Aug 1;17(15):3790. doi: 10.3390/ma17153790.

Abstract

Quasi-static and dynamic tensile tests on aluminum-hydroxide-enhanced ethylene propylene diene monomer (EPDM) coatings were conducted using a universal testing machine and a Split Hopkinson Tension Bar (SHTB) over a strain rate range of 10 to 10 s. This comprehensive study explored the tensile performance of enhanced EPDM coatings in solid rocket motors. The results demonstrated a significant impact of strain rate on the mechanical properties of EPDM coatings. To capture the hyperelastic and viscoelastic characteristics of EPDM coatings at large strains, the Ogden hyperelastic model was used to replace the standard elastic component to develop an enhanced Zhu-Wang-Tang (ZWT) nonlinear viscoelastic constitutive model. The model parameters were fitted using a particle swarm optimization (PSO) algorithm. The improved constitutive model's predictions closely matched the experimental data, accurately capturing stress-strain responses and inflection points. It effectively predicts the tensile behavior of aluminum-hydroxide-enhanced EPDM coatings within a 20% strain range and a wide strain rate range.

摘要

使用万能试验机和分离式霍普金森拉杆(SHTB),在10⁻⁵至10² s⁻¹的应变率范围内,对氢氧化铝增强的三元乙丙橡胶(EPDM)涂层进行了准静态和动态拉伸试验。这项全面的研究探讨了固体火箭发动机中增强EPDM涂层的拉伸性能。结果表明应变率对EPDM涂层的力学性能有显著影响。为了捕捉EPDM涂层在大应变下的超弹性和粘弹性特性,使用奥格登超弹性模型取代标准弹性分量,开发了一种增强的朱-王-唐(ZWT)非线性粘弹性本构模型。模型参数采用粒子群优化(PSO)算法进行拟合。改进后的本构模型预测结果与实验数据紧密匹配,准确捕捉了应力-应变响应和拐点。它有效地预测了氢氧化铝增强EPDM涂层在20%应变范围内和宽应变率范围内的拉伸行为。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/7c45/11312910/8b2e6f41d14e/materials-17-03790-g001.jpg

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