Suppr超能文献

复合固体推进剂单轴拉伸力学行为的实验与数值研究

Experimental and Numerical Investigation into the Mechanical Behavior of Composite Solid Propellants Subject to Uniaxial Tension.

作者信息

Wu Chengfeng, Jiang Ming, Lu Yingying, Qu Hongjian, Li Hongyan, Hu Shaoqing

机构信息

Xi'an Modern Chemistry Research Institute, Xi'an 710065, China.

出版信息

Materials (Basel). 2023 Oct 15;16(20):6695. doi: 10.3390/ma16206695.

Abstract

To further explore the quasi-static mechanical characteristics of composite solid propellants at low strain rates, an investigation was conducted on the mechanical behavior and damage mechanisms of a four-component hydroxy-terminated polybutadiene (HTPB) propellant by means of experiments and numerical simulation. A uniaxial tensile test and scanning electron microscope (SEM) characterization experiment were carried out. A microstructural model, which accurately represents the mesoscopic structure, was developed via the integration of micro-CT scanning and image-processing techniques. The constructed microstructural model was utilized to conduct a numerical simulation of the mechanical behavior. The experimental results demonstrated that the maximum tensile strength increases with increasing strain rate, and the primary cause of propellant failure at low strain rates is the dewetting phenomenon occurring at the interface between the larger particles and the matrix. The maximum tensile strength is 0.48 MPa when the strain rate is 0.00119 s, and the maximum tensile strength is 0.37 MPa when the strain rate is 0.000119 s. The simulation results indicated a consistent trend in variation when comparing the simulation and experimental curves. This suggested that the established model exhibits a high level of reliability, and provides a promising approach for carrying out microstructural simulations of heterogeneous propellants in future. The mechanical behavior of the propellant can be effectively described by utilizing a mesoscopic finite element model that incorporates the superelastic constitutive model of the matrix and the bilinear cohesive model. This framework facilitates the representation of mesoscopic damage evolution, which consequently provides insights into the damage mechanism. Additionally, the utilization of such models assists in compensating for the limitations of damage evolution characterization experiments.

摘要

为了进一步探究复合固体推进剂在低应变速率下的准静态力学特性,通过实验和数值模拟对一种四组分端羟基聚丁二烯(HTPB)推进剂的力学行为和损伤机制进行了研究。开展了单轴拉伸试验和扫描电子显微镜(SEM)表征实验。通过整合显微CT扫描和图像处理技术,建立了一个能够准确表征细观结构的微观结构模型。利用所构建的微观结构模型对力学行为进行了数值模拟。实验结果表明,最大拉伸强度随应变速率的增加而增大,低应变速率下推进剂失效的主要原因是较大颗粒与基体界面处发生的脱湿现象。应变速率为0.00119 s时,最大拉伸强度为0.48 MPa;应变速率为0.000119 s时,最大拉伸强度为0.37 MPa。模拟结果表明,模拟曲线与实验曲线的变化趋势一致。这表明所建立的模型具有较高的可靠性,并为今后开展非均质推进剂的微观结构模拟提供了一种有前景的方法。利用包含基体超弹性本构模型和双线性粘结模型的细观有限元模型,可以有效地描述推进剂的力学行为。该框架有助于表征细观损伤演化,从而深入了解损伤机制。此外,此类模型的应用有助于弥补损伤演化表征实验的局限性。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/dcc8/10608625/666a4a2d382f/materials-16-06695-g001.jpg

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验