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Uncertainty and Sensitivity Analysis of Afterbody Radiative Heating Predictions for Earth Entry

机译:进入地球后车身辐射加热预测的不确定度和灵敏度分析

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摘要

The objective of this work was to perform sensitivity analysis and uncertainty quantification for afterbody radiative heating predictions of the Stardust capsule during Earth entry at peak afterbody radiation conditions. The radiation environment in the afterbody region poses significant challenges for accurate uncertainty quantification and sensitivity analysis due to the complexity of the flow physics, computational cost, and large number of uncertain variables. In this study, first a sparse collocation nonintrusive polynomial chaos approach along with global nonlinear sensitivity analysis was used to identify the most significant uncertain variables and reduce the dimensions of the stochastic problem. Then, a total-order stochastic expansion was constructed over only the important parameters for an efficient and accurate estimate of the uncertainty in radiation. Based on previous work, 388 uncertain parameters were considered in the radiation model, which came from the thermodynamics, flowfield chemistry, and radiation modeling. The sensitivity analysis showed that only four of these variables contributed significantly to afterbody radiation uncertainty, accounting for almost 95% of the uncertainty. These included the electronic-impact excitation rate for N between level 2 and level 5 and rates of three chemical reactions influencing N, N+, O, and O+ number densities in the flowfield.
机译:这项工作的目的是对在进入后体辐射峰值时的星尘舱后体辐射加热预测进行灵敏度分析和不确定性量化。由于流动物理的复杂性,计算成本和大量不确定变量,后车身区域的辐射环境对准确的不确定性定量和灵敏度分析提出了重大挑战。在这项研究中,首先使用稀疏搭配非侵入式多项式混沌方法以及全局非线性灵敏度分析来识别最重要的不确定变量,并减小随机问题的规模。然后,仅在重要参数上构建总阶随机扩展,以有效,准确地估计辐射的不确定性。根据以前的工作,在辐射模型中考虑了388个不确定参数,这些参数来自热力学,流场化学和辐射建模。敏感性分析表明,这些变量中只有四个对后体辐射不确定性有显着影响,几乎占不确定性的95%。其中包括N在2级和5级之间的电子碰撞激发速率,以及影响流场中N,N +,O和O +数密度的三种化学反应的速率。

著录项

  • 来源
    《Journal of Thermophysics and Heat Transfer》 |2017年第2期|294-306|共13页
  • 作者单位

    NASA, Langley Res Ctr, Vehicle Anal Branch, Syst Anal & Concepts Directorate, Hampton, VA 23681 USA;

    NASA, Langley Res Ctr, Aerothermodynam Branch, Res Directorate, Hampton, VA 23681 USA;

    Missouri Univ Sci & Technol, Dept Aerosp & Mech Engn, Aerosp Engn, Rolla, MO 65409 USA;

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

  • 入库时间 2022-08-18 03:01:18

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