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高超声速三维化学非平衡流动的数值模拟
Numerical simulations of hypersonic three-dimensional chemical non-equilibrium flows
查看参考文献6篇
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文摘
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高温非平衡化学反应对高超声速再入飞行器绕流流场的气动热特性有较大影响．通过采用有限体积NND(Non-oscillatory，containing No free parameters and Dissipative scheme)格式求解三维N-S方程，分别计算了小攻角条件下球锥的完全气体粘性流场和化学反应非平衡气体流场．比较并分析了化学非平衡作用对三维高超声速钝头体绕流流场的影响．所得结果与国外文献结果符合的较好，证明了计算方法与程序的有效性和实用性． |
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其他语种文摘
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High temperature chemical non-equilibrium phenomena have a great effect on the flow field around a reentry vehicle. A three dimensional Navier-Stokes equations were solved by implicit finite volume NND scheme. Both ideal gas viscous flow and chemical non-equilibrium flow were calculated for a sphere-cone at a small attack angle. The results of the two flows were compared and the effect of chemical non-equilibrium was analyzed. The re sult is in good agreement with the reference paper. That proves that our method and programs are effective and prac tical. |
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来源
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北京航空航天大学学报
,2004,30(2):168-172 【核心库】
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关键词
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化学非平衡
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地址
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中国科学院力学研究所, 北京, 100080
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语种
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中文 |
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文献类型
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研究性论文 |
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ISSN
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1001-5965 |
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学科
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航空 |
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文献收藏号
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CSCD:1620103
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参考文献 共
6
共1页
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陈让福.
三维高超声速无粘定常绕流的数值模拟,1991
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An upwind-biased point-implicit relaxation algorithm for viscous compressible perfect-gas flows,NASA TP-2953,1990
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Three-dimensional unsteady euler equations solution using flux vector splitting, AIAA 84-1552,1984
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8
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6.
Kim S L.
Approximate jacobian methods for efficient calculation of reactive flows, AIAA 2000-3384,2000
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CSCD被引
1
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