| 对称翼型近场尾流及后缘边界层流动特性的试验研究 |
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| 引用本文： | 何克敏 屠兴. 对称翼型近场尾流及后缘边界层流动特性的试验研究[J]. 空气动力学学报, 1989, 7(4): 479-484 |
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| 作者姓名： | 何克敏 屠兴 |
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| 作者单位： | 西北工业大学(何克敏)，西北工业大学(屠兴) |
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| 摘 要： | 本文简述了用热线风速仪测量“NACA 63-012”对称翼型近场尾流及后缘边界层流动特性,讨论了流场的时均特性及雷诺应力等湍流量的分布特性,提出了无因次速度分布的半经验公式、相关参数及相关曲线解析式,并得出了几点重要结论。
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| 关 键 词： | 翼型 近场尾流 边界层 流动特性 |
EXPERIMENTAL INVESTIGATION OF TRAILING-EDGE AND NEAR WAKE FLOW OF A SYMMETRIC AIRFOIL |
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| He Kemin Tu Xing. EXPERIMENTAL INVESTIGATION OF TRAILING-EDGE AND NEAR WAKE FLOW OF A SYMMETRIC AIRFOIL[J]. Acta Aerodynamica Sinica, 1989, 7(4): 479-484 |
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| Authors: | He Kemin Tu Xing |
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| Affiliation: | Northwestern Polytechnical University |
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| Abstract: | This paper describes the trailing edge and near wake flow of a NACA 63-012 symmetric airfoil measured by a hot wire anemometer. The distribution of mean flow velocity and Reynolds stress is measured and discussed. The semiempirical relation of nondimentional velocity distribution is obtained. Some correlation parameters and ana-lytical correlation functions are also obtained. At last, some importantconclusions are given in this paper. |
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| Keywords: | airfoil trailing edge flow boundary layer near wake flow turbulence. |
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