| 压缩拐角区的压力,热流工程计算方法 |
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| 引用本文： | 杨茂昭.压缩拐角区的压力,热流工程计算方法[J].航空学报,1988,9(2):77-81. |
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| 作者姓名： | 杨茂昭 |
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| 作者单位： | 中国气动力研究与发展中心 |
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| 摘 要： | <正> 引言 从压缩拐角分离流动的试验及数值计算出发,建立起一个实用范围较广精度较高的工程估算程序,方便快速地估算出压缩拐角分离区和再附区的峰值压力、峰值热流;分离区和再附点位置;分离区长度等。这是气动设计部门关注的课题。这些工作是在文献(3,4)中的经验公式的基础上,按照分离流动流谱,分区进行迭代修正计算,对二维情况给出了完整
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| 收稿时间： | 1988-01-14; |
ENGINEERING METHOD FOR PREDICTING PRESSURE AND HEAT RATE OF THE COMPRESSIBLE CORNER REGION |
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| Yang Maozhao.ENGINEERING METHOD FOR PREDICTING PRESSURE AND HEAT RATE OF THE COMPRESSIBLE CORNER REGION[J].Acta Aeronautica et Astronautica Sinica,1988,9(2):77-81. |
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| Authors: | Yang Maozhao |
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| Institution: | China Aerodynamic Research and Development Centre |
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| Abstract: | An iterative correction method is presented in this paper for predicting the pressure and the heat rate in the separated and reattached regions in a compressible corner. The metho'd is constructed based on the basic separated flow patterns, in conjunction with empirical formulas. For the two-dimensional compressible corner, good agreement is obtained for the pressure and heat rate with the experimental data. |
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| Keywords: | separated flow corner flow shock wave and boundary layer interaction thermal boundary layer |
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