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首页> 外文期刊>Journal of Spacecraft and Rockets >Simulating Stardust Earth Reentry with Radiation Heat Transfer
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Simulating Stardust Earth Reentry with Radiation Heat Transfer

机译:利用辐射传热模拟星尘进入地球

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摘要

A multigroup spectral method is integrated into an interdisciplinary formulation for nonequilibrium radiativenhypersonic flows. The developed simulation capability has been successfully applied to study the Stardust capsulenEarth reentry via an axisymmetric approximation. The predicted total heat transfer rates at different stages ofnreentry achieve a reasonable agreement with results in literature. The computational results reveal a closencorrelation between the relaxation of vibrational excitations and diffusive heat transfer in the wake, as well as andiminished radiative intensity and a shifted emission spectrum in the shock layer toward the lower-frequencyndomain from the earlier to the later stages of the reentry.
机译:多组谱方法已集成到非平衡辐射非人身流的跨学科公式中。通过轴对称近似,已开发的模拟功能已成功地用于研究星尘胶囊n地球折返。预测的不同阶段的总传热速率与文献结果达到合理的一致。计算结果表明,振动激励的弛豫与尾流中的扩散热传递之间有着紧密的相关性,并且从后入阶段的较早阶段到后期阶段,减弱的辐射强度和激波层中的辐射谱向低频域偏移。 。

著录项

  • 来源
    《Journal of Spacecraft and Rockets 》 |2011年第3期| p.385-396| 共12页
  • 作者

    J S. Shang; S T. Surzhikov;

  • 作者单位

    J. S. Shang∗Wright State University, Dayton, Ohio 45435andS. T. Surzhikov†Russian Academy of Sciences, 119526, Moscow, Russia;

  • 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
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