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Three-Dimensional Finite Element Ablative Thermal Response and Design of Thermal Protection Systems

机译:三维有限元烧蚀热响应及热保护系统设计

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摘要

A finite element ablation and thermal response program for the simulation of three-dimensional transient thermostructural analysis has been developed. The three-dimensional governing differential equations and finite element formulation are summarized. A novel probabilistic design methodology for thermal protection systems has been developed. The design methodology is an eight step process beginning with a parameter sensitivity study and is followed by a deterministic analysis whereby an optimum design can determined. The design process concludes with a Monte Carlo simulation where the probabilities of exceeding design specifications are estimated. The design methodology is demonstrated by applying the methodology to the carbon phenolic compression pads of the Crew Exploration Vehicle. The maximum allowed values of bondline temperature and tensile stress are used as the design specifications in this study. Using the design methodology, the probability of exceeding these design specifications was shown to be low and within an acceptable range.
机译:开发了用于三维瞬态热结构分析的有限元烧蚀和热响应程序。总结了三维控制微分方程和有限元公式。已经开发了用于热保护系统的新颖的概率设计方法。设计方法学是一个八步过程,首先进行参数敏感性研究,然后进行确定性分析,从而可以确定最佳设计。设计过程以蒙特卡洛模拟结束,其中将评估超出设计规格的概率。通过将该方法应用于乘员探索车的碳酚压缩垫进行了论证。粘结线温度和拉伸应力的最大允许值用作本研究的设计规格。使用设计方法论,证明超出这些设计规范的可能性很低,并且在可接受的范围内。

著录项

  • 来源
    《Journal of Spacecraft and Rockets》 |2013年第4期|725-734|共10页
  • 作者

    John A. Dec; Robert D. Braun;

  • 作者单位

    NASA Langley Research Center, Hampton, Virginia 23681;

    Georgia Institute of Technology, Atlanta, Georgia 30332-0150;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-18 02:34:23

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