Rate-dependent cohesive zone model of the interface between HTPB propellant and insulation
-
摘要: 采用实验与反演相结合的方法构建了端羟基聚丁二烯(HTPB)推进剂/衬层界面的率相关的内聚力模型.采用改进的单搭接试件完成了HTPB推进剂/衬层界面的断裂实验研究,采用内聚力单元方法对单搭接试件进行了数值研究,结合基于Hook-Jeeves优化算法的反演识别程序,获取了不同加载率下的界面断裂参数.由于界面断裂参数具有明显的率相关性,通过构建率相关的损伤函数,构建了基于双线性内聚力模型的率相关HTPB推进剂/衬层界面Ⅱ型内聚力模型.模型预测结果和实验结果的对比相关系数大于99%,说明本文所建立的 率相关内聚力模型具有较高的准确性,能够准确描述加载率为5~200mm/min时推进剂/衬层界面的断裂性质.Abstract: In order to build up a rate-dependent cohesive zone model (CZM) of the interface between hydroxyl-terminated polybutadiene(HTPB) propellant and insulation, experimental method and inverse analysis were adopted. Improved single lap joints (SLJ) specimens were used to conduct the HTPB propellant and insulation interface debonding experiment, then a numerical analysis was conducted with cohesive elements method, and with an inverse program developed based on Hook-Jeeves optimizing algorithm, the inverse analysis was conducted for the SLJ specimens to calibrate the interface parameters in different loading rates. Considering the significant rate-dependency shown in the parameters, a rate-dependent damage function was built and then the rate-dependent interfacial type Ⅱ CZM of HTPB propellant and insulation was built based on the bilinear CZM. The correlation coefficient between the predicted result and the experimental result is bigger than 99%, illustrating the rate-dependent CZM referred herein can accurately describe the fracture properties of propellant and insulation interface for the loading rate of 5mm/min to 200mm/min.
-
[1] 许进升.复合推进剂热粘弹性本构模型实验及数值仿真研究[D].南京:南京理工大学,2013. XU Jinsheng.Experimental and numerical research on thermo-viscoelastic constitutive model of composite propellant[D].Nanjing:Nanjing University of Science and Technology,2013.(in Chinese) [2] 郑晓亚,柳青,王卫祥.固体装药结构界面应力分析[J].航空动力学报,2012,27(8):1861-1866. ZHENG Xiaoya,LIU Qing,WANG Weixiang.Interface stress analysis of solid motor grain structure[J].Journal of Aerospace Power,2012,27(8):1861-1866.(in Chinese) [3] 姜爱民,李高春,郭宇,等.黏接界面试件拉伸变形破坏过程的数字散斑相关方法分析[J].航空动力学报,2014,29(5):255-261. JIANG Aimin,LI Gaochun,GUO Yu,et al.Adhesive interface deformation and failure digital speckle correlation method[J].Journal of Aerospace Power,2014,29(5):255-261.(in Chinese) [4] Bazant Z P,Planas J.Fracture and size effect in concrete and other quasibrittle materials[M].Boca Raton:CRC Press,1998. [5] Barenblatt G I.The formation of equilibrium cracks during brittle fracture:general ideas and hypotheses,axially-symmetric cracks[J].Journal of Applied Mathematics and Mechanics,1959,23(3):622-636. [6] Dugdale D S.Yielding of steel sheets containing slits[J].Journal of the Mechanics and Physics of Solids,1960,8(2):100-104. [7] Xu C,Siegmund T,Ramani K.Rate-dependent crack growth in adhesives:I modeling approach[J].International Journal of Adhesion and Adhesives,2003,23(1):9-13. [8] Musto M,Alfano G.A novel rate-dependent cohesive-zone model combining damage and visco-elasticity[J].Computers and Structures,2013,118:126-133. [9] Wang J,Qin Q H,Kang Y L,et al.Viscoelastic adhesive interfacial model and experimental characterization for interfacial parameters[J].Mechanics of Materials,2010,42(5):537-547. [10] Campilho R,De Moura M,Domingues J.Using a cohesive damage model to predict the tensile behaviour of CFRP single-strap repairs[J].International Journal of Solids and Structures,2008,45(5):1497-1512. [11] NIU Ranming,ZHOU Qingchun,CHEN Xiong,et al.Experimental and numerical analysis of mode II fracture between propellant and insulation[J].International Journal of Adhesion and Adhesives,2014,52:1-10. [12] Chandra N,Li H,Shet C,et al.Some issues in the application of cohesive zone models for metal-ceramic interfaces[J].International Journal of Solids and Structures,2002,39(10):2827-2855. [13] Davila C G,Camando P P,Moura,M F.Mixed-mode decohesion ele-590ments for analyses with progressive delamination[R].Seattle:42nd AIAA/ASME/ASCE/AHS/ASC Structures,Structural Dynamics and Materials Conferences,2001. [14] Geubelle P H,Baylor J S.Impact-induced delamination of composites:a 2D simulation[J].Composites:Part B Engineering,1998,29(5):589-602. [15] Van den Boshi M J,Schreurs P J G,Geers M G D.An improved description of the exponential Xu and Needleman cohesive zone law for mixed-mode decohesion[J].Engineering Fracture Mechanics,2006,73(9):1220-1234. [16] Park K.Potential-based fracture mechanics using cohesive zone and virtual internal bond modeling[D].Illinois:University of Illinois at Urbana-Chanmpaign,2009. [17] ZHOU Qingchun,JU Yutao,WEI Zhen,et al.Cohesive zone modeling of propellant and insulation interface debonding[J].The Journal of Adhesion,2014,90(3):1-22. [18] Watkins J.Fracture toughness test for soll-cement samples in mode Ⅱ[J].International Journal of Fracture,1983,23(4):135-138.
点击查看大图
计量
- 文章访问数: 819
- HTML浏览量: 2
- PDF量: 562
- 被引次数: 0