| 绕HERMES外形高超声速无粘流动的数值模拟 |
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| 引用本文： | 叶友达,张涵信.绕HERMES外形高超声速无粘流动的数值模拟[J].空气动力学学报,1994,12(1):15-21. |
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| 作者姓名： | 叶友达 张涵信 |
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| 作者单位： | 中国空气动力研究与发展中心 |
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| 摘 要： | 本文采用时间相关法和隐式推进迭代方法求解了绕ＨＥＲＭＥＳ外形高超声速无粘流动。将抛物型方程和代数方程相结合生成计算网格，既节省了网格生成的时间，又能得到较合理的网格分布。在时间相关法计算中，采用了显式ＮＮＤ格式；在隐式推进迭代计算中，采用了推广的隐式ＮＮＤ格式。
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| 关 键 词： | 差分计算 航天飞机 网格生成 |
Numerical Simulation of Hypersonic Inviscid Flow Around the HERMES Configuration |
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| Ye Youda Zhang Hanxin Guo Zhiquan.Numerical Simulation of Hypersonic Inviscid Flow Around the HERMES Configuration[J].Acta Aerodynamica Sinica,1994,12(1):15-21. |
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| Authors: | Ye Youda Zhang Hanxin Guo Zhiquan |
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| Institution: | China Aerodynamics Research and Development Center |
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| Abstract: | The hypersonic inviscid flow around the HERMES config-uration has been simulated by the time-dependent algorithm and implicit spatial-marching itcration algorithm in this paper.The parabolic cquations are combined with the algebraic equations to generate the computational grids, and the reasonable grids distribution can be obtained with less computationaI time. The explicit NND schemes arc used in thc time-depcndent calculation and the implicit NND schemes are used in the im-plicit spatial-marching iteration calculation. |
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| Keywords: | difference calculation space shuttle orbiter Euler equa-tions NND schemes grid generation |
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