| 三维跨声速流粘性—无粘相互作用问题的分析和计算 |
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| 引用本文： | 温功碧,陈作斌.三维跨声速流粘性—无粘相互作用问题的分析和计算[J].空气动力学学报,1992,10(3):339-346. |
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| 作者姓名： | 温功碧 陈作斌 |
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| 作者单位： | 北京大学，北京大学，北京大学，中国空气动力研究与发展中心 北京 100871，北京 100871，北京 100871，四川绵阳 621000 |
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| 摘 要： | 本文对跨声速粘性-无粘相互作用问题进行了分析,论证了如何选择湍流边界层反模式的输入量。在FL027多重网格基础上作了局部加密。计算例子表明,本文建议的半逆方法适用于弱激波情形,可用于实际设计之中。
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| 关 键 词： | 跨音速流动 湍流边界层 |
The Analysis and Computation of Viscous-Inviscid Interactive Problem for Three Dimensional Transonic Flow |
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| Wen Gongbi He Xiaoyi Wu Wangyi.The Analysis and Computation of Viscous-Inviscid Interactive Problem for Three Dimensional Transonic Flow[J].Acta Aerodynamica Sinica,1992,10(3):339-346. |
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| Authors: | Wen Gongbi He Xiaoyi Wu Wangyi |
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| Institution: | Wen Gongbi He Xiaoyi Wu Wangyi (Beijing University)Chen Zuobin (China Aerodynamics Research and Development Center) |
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| Abstract: | In this paper we analyses the viscous-inviscid interactive problem for three dimensional transonic flow. A suitable choice of inputs for the boundary layer equations in the transonic regime was proved. Based on the multigrid of FL027, partial fine mesh was implemented. Numerical solutions about M6 and F1 wing are presented using full potential equation and an inverse integral three dimensional compressible turbulent boundary layer code and compared with experimental data. It shows that the semi-inverse code which is suggested in this paper can be applied to design for weak shock. |
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| Keywords: | viscous-inviscid interaction transonic flow inverse integral code turbulent boundary layer |
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