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轻质热防护系统多层材料组合结构的热应力分析

王琪 吉庭武 肖曼玉 谢公南

王琪, 吉庭武, 肖曼玉, 谢公南. 轻质热防护系统多层材料组合结构的热应力分析[J]. 应用数学和力学, 2013, 34(7): 742-749. doi: 10.3879/j.issn.1000-0887.2013.07.009
引用本文: 王琪, 吉庭武, 肖曼玉, 谢公南. 轻质热防护系统多层材料组合结构的热应力分析[J]. 应用数学和力学, 2013, 34(7): 742-749. doi: 10.3879/j.issn.1000-0887.2013.07.009
ZHANG Lang, LI Xue-wu, XIA Jian-zhong, . Numerical Analysis on Thermal Stress of Multilayer Materials Combined Structures for a Lightweight Thermal Protection System[J]. Applied Mathematics and Mechanics, 2013, 34(7): 742-749. doi: 10.3879/j.issn.1000-0887.2013.07.009
Citation: ZHANG Lang, LI Xue-wu, XIA Jian-zhong, . Numerical Analysis on Thermal Stress of Multilayer Materials Combined Structures for a Lightweight Thermal Protection System[J]. Applied Mathematics and Mechanics, 2013, 34(7): 742-749. doi: 10.3879/j.issn.1000-0887.2013.07.009

轻质热防护系统多层材料组合结构的热应力分析

doi: 10.3879/j.issn.1000-0887.2013.07.009
基金项目: 国家自然科学基金资助项目(11202164); 教育部高等学校博士学科点专项科研基金资助项目(20116102120021)
详细信息
    作者简介:

    王琪(1988—),男,湖南人,硕士生(E-mail: nwpuwq@mail.nwpu.edu.cn);谢公南(1980—),男,广东人,副教授,博士(通讯作者. E-mail: xgn@nwpu.edu.cn).

  • 中图分类号: V19;O343.6

Numerical Analysis on Thermal Stress of Multilayer Materials Combined Structures for a Lightweight Thermal Protection System

  • 摘要: 提出了轻质热防护系统外面板使用多层结构的概念,设计了2种热防护材料组合构成的3种铺层方案.通过模拟飞行器再入大气层时受到的机械和热载荷条件,数值计算得到了层间剪切力、底部温度和y方向位移.计算结果发现,层间剪切力发生在边缘部位且呈反对称分布;选用高热导率和高热容材料能够减少材料内的温度梯度,进而有效地降低结构的热应力和热变形;在均匀温度场情况下,两种材料的热膨胀系数之差越小,则层间剪切力越小.该研究表明不同的材料组合和铺层次序的多层结构,可以满足不同设计要求,具有优化设计潜力.
  • [1] 陈战辉. RLV金属热防护系统传热分析与结构设计[D]. 硕士论文. 西安: 西北工业大学, 2008. (CHEN Zhan-hui. Thermal analysis and structure design of RLV metallic thermal protection systems[D]. Master thesis. Xi’an: Northwestern Polytechnical University, 2008. (in Chinese))
    [2] 郭朝邦, 李文杰. 高超声速飞行器结构材料与热防护系统[J]. 飞航导弹, 2010(4): 88-94. (GUO Chao-bang, LI Wen-jie. Hypersonic vehicle structure material and thermal protection system[J]. Winged Missiles Journal,2010(4): 88-94. (in Chinese))
    [3] 马忠辉. 可重复使用运载器热防护系统性能分析研究[D]. 博士论文. 西安: 西北工业大学, 2004. (MA Zhong-hui. Reusable launch vehicle thermal protection system performance study[D]. Ph D thesis. Xi’an: Northwestern Polytechnical University, 2004. (in Chinese))
    [4] Biamino S, Antonini A, EisenmengerSittner C, Fuso L, Pavese M, Fino P, Bauer E, Badini C. Multilayer SiC for thermal protection system of space vehicles with decreased thermal conductivity through the thickness[J]. Journal of European Ceramic Society,2010, 30(8): 1833-1840.
    [5] Daryabeigi K. Thermal analysis and design of multi-layer insulation for re-entry aerodynamic heating[C]//35th AIAA Thermophysics Conference.Anaheim, CA, Paper, No 2001-2834, USA, 2001.
    [6] 高效伟, 杨恺. 功能梯度材料结构的热应力边界元分析[J]. 力学学报, 2011,43(1): 136-143. (GAO Xiao-wei, YANG Kai. Thermal stress analysis of functionally graded material structures using boundary element method[J]. Chinese Journal of Theoretical and Applied Mechanics,2011, 43(1): 136-143. (in Chinese))
    [7] 孙陈诚, 胡子君, 陈海坤, 王晓婷, 周洁洁. 组合结构对多层反射纳米材料高温隔热性能的影响[J]. 宇航材料工艺, 2011, 41(6): 44-46.(SUN Chen-cheng, HU Zi-jun, CHEN Hai-kun, WANG Xiao-ting, ZHOU Jie-jie. Effects of structure on high temperature insulation performance of multi-layered nanoporous materials[J]. Journal of Aerospace Materials and Technology,2011, 41(6): 44-46. (in Chinese))
    [8] 包亦望, 左岩, 石新勇, 马眷荣. 有机无机层合玻璃的热应力分析[J]. 航空材料学报, 1999, 19(3): 51-56. (BAO Yi-wang, ZUO Yan, SHI Xin-yong, MA Juan-rong. Analysis on thermal stress of organic-inorganic glass laminate[J]. Journal of Aeronautical Materials,1999, 19(3): 51-56. (in Chinese))
    [9] 韩文梅, 陈敬芬, 薛春霞, 关学峰. 基于ANSYS航空层合玻璃的热应力分析[J]. 兵器材料科学与工程, 2010, 33(6): 1-3. (HAN Wen-mei, CHEN Jin-fen, XUE Chun-xia, GUAN Xue-feng. Thermal stress analysis of aerial laminated glass based on ANSYS[J]. Ordnance Material Science and Engineering,2010, 33(6):1-3. (in Chinese))
    [10] 李东辉, 夏新林, 艾青. 多层高温隔热结构的传热特性[J]. 宇航材料工艺, 2011, 41(1): 20-23. (LI Donghui, XIA Xin-lin, AI Qing. Heat transfer characteristics of high temperature multilayer thermal insulations[J]. Journal of Aerospace Materials and Technology,2011, 41(1): 20-23. (in Chinese))
    [11] 王琪, 吉庭武, 谢公南, 张卫红. 轻质热防护系统波纹夹芯结构热力耦合分析[J]. 应用数学和力学, 2013, 34(2): 172-182. (WANG Qi, JI Ting-wu, XIE Gong-nan, ZHANG Wei-hong. Structural analysis of corrugated-core sandwich panels for lightweight thermal protection system[J]. Applied Mathematics and Mechanics,2013, 34(2): 172-182. (in Chinese))
    [12] 马玉娥. 可重复使用运载器热防护系统热/力耦合数值计算研究[D]. 博士论文. 西安: 西北工业大学, 2005. (MA Yu-e. Study of thermo-mechanical coupled computation for thermal protection system of reusable launch vehicle[D]. Ph D thesis. Xi’an: Northwestern Polytechnical University, 2005. (in Chinese))
    [13] 韩秀峰. 碳改性C/SiC复合材料的结构与性能[D]. 硕士论文. 西安: 西北工业大学, 2006. (HAN Xiu-feng. Microstructure and properties of matrix modified C/SiC composites by pyrocarbon[D]. Master thesis. Xi’an: Northwestern Polytechnical University, 2006. (in Chinese))
    [14] 蔺晓轩, 武海棠, 魏玺, 沈志洵, 张伟刚. ZrB2-SiC前缘构件气动加热及热应力的数值模拟分析[J]. 过程工程学报, 2010, 10(3): 417423. (LIN Xiao-xuan, WU Hai-tang, WEI Xi, SHEN Zhi-xun, ZHANG Wei-gang. Numerical simulation on aerodynamic heating and thermal stress of ZrB2-SiC leading edge[J]. The Chinese Journal of Process Engineering,2010, 10(3): 417-423. (in Chinese))
    [15] Gogu C, Bapanapalli S K, Haftka R T, Sankar B V. Comparison of materials for an integrated thermal protection system for spacecraft reentry[J]. AIAA J Spacecraft and Rockets,2009, 46(3): 501-513. 
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出版历程
  • 收稿日期:  2013-05-14
  • 修回日期:  2013-05-16
  • 刊出日期:  2013-07-15

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