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高超声速飞行流场中的最大氧离解度分析

陈松 孙泉华

陈松, 孙泉华. 高超声速飞行流场中的最大氧离解度分析[J]. 力学学报, 2014, 46(1): 20-27. doi: 10.6052/0459-1879-13-146
引用本文: 陈松, 孙泉华. 高超声速飞行流场中的最大氧离解度分析[J]. 力学学报, 2014, 46(1): 20-27. doi: 10.6052/0459-1879-13-146
Chen Song, Sun Quanhua. ANALYSIS OF MAXIMUM DISSOCIATION DEGREE OF OXYGEN DURING HYPERSONIC FLIGHT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(1): 20-27. doi: 10.6052/0459-1879-13-146
Citation: Chen Song, Sun Quanhua. ANALYSIS OF MAXIMUM DISSOCIATION DEGREE OF OXYGEN DURING HYPERSONIC FLIGHT[J]. Chinese Journal of Theoretical and Applied Mechanics, 2014, 46(1): 20-27. doi: 10.6052/0459-1879-13-146

高超声速飞行流场中的最大氧离解度分析

doi: 10.6052/0459-1879-13-146
基金项目: 国家自然科学基金资助项目(90816012, 91116013, 11111120080).
详细信息
    作者简介:

    孙泉华,研究员,主要研究方向:稀薄气体及非平衡流动.E-mail:qsun@imech.ac.cn

  • 中图分类号: V211.22

ANALYSIS OF MAXIMUM DISSOCIATION DEGREE OF OXYGEN DURING HYPERSONIC FLIGHT

  • 摘要: 针对大气层内高超声速飞行时的化学非平衡现象,建立了沿驻点线流动的空气中氧离解度的计算模型. 模型假设氮气在氧气未充分离解时不发生离解,并且不涉及边界层内的复合反应. 理论计算发现,空气中氧的离解度随飞行高度的增加呈先增后减的非单调变化规律,其原因是由于化学反应平衡移动与非平衡效应相互作用的结果. 这一结论得到了数值模拟结果的验证,同时也解释了文献中当飞行高度较高时真实气体效应减弱的现象. 基于驻点线的近似理论模型,计算得到了轴对称钝头体绕流流场中的最大氧离解度及边界层外缘温度随飞行速度和高度变化的等值线图谱,相关结果可以为工程设计所用.

     

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  • 被引次数: 0
出版历程
  • 收稿日期:  2013-05-10
  • 修回日期:  2013-06-27
  • 刊出日期:  2014-01-18

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