| 跨音速叶栅流场的无粘-边界层迭代计算 |
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| 引用本文： | 罗曼芦,张柏年.跨音速叶栅流场的无粘-边界层迭代计算[J].空气动力学学报,1988(2). |
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| 作者姓名： | 罗曼芦 张柏年 |
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| 作者单位： | 上海交通大学
(罗曼芦)，上海交通大学(张柏年) |
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| 摘 要： | 二维跨音速叶栅流场的计算是在无粘时间相关法计算程序的基础上采用无粘-边界层迭代而得。马赫数从亚音速到超音速范围的几种数值试验均与测试结果吻合一致。在边界层无强烈脱流时可获得很好的结果。
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| 关 键 词： | 跨音速流 边界层 无粘流 激波 |
NUMERICAL CALCULATION FOR THE FLOW FIELD OF TRANSONIC CASCADE WITH INVISCID-VISCOUS INTERACTION METHOD |
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| Luo Manlu Zhang Bainian.NUMERICAL CALCULATION FOR THE FLOW FIELD OF TRANSONIC CASCADE WITH INVISCID-VISCOUS INTERACTION METHOD[J].Acta Aerodynamica Sinica,1988(2). |
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| Authors: | Luo Manlu Zhang Bainian |
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| Institution: | Shanghai Jiaotong University |
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| Abstract: | An inviscid-viscous interaction method based on the invis-cid time marching computer code has been employed to calculate the transonic flow field of two dimensional cascade.Good agreement with the experimental data has been achieved for several numerical test cases for which the Mach number ranged from subsonic up to supersonic.The computer code works exceedingly well with the transonic flow when there is no strong boundary seperation. |
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| Keywords: | transonic flow boundary layer inviscid flow shock |
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