| 细长机翼非线性升力和压心的近似解析计算法 |
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| 引用本文： | 尹协远.细长机翼非线性升力和压心的近似解析计算法[J].航空学报,1980,1(1):1-6. |
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| 作者姓名： | 尹协远 |
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| 作者单位： | 中国科技大学 |
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| 摘 要： | 本文给出了计算前、侧缘涡升力及其压心的一种近似简化分析方法,同时给出两个经验修正公式,与其它方法和实验数据比较表明,本方法精度良好,可以满足工程设计的需要。
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| 收稿时间： | 1979-10-01; |
AN APPROXIMATE ANALYTICAL METHOD FOR VORTEX-LIFT AND CENTRE OE PRESSURE ON THE SLENDER WING |
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| Yin Xieyuan.AN APPROXIMATE ANALYTICAL METHOD FOR VORTEX-LIFT AND CENTRE OE PRESSURE ON THE SLENDER WING[J].Acta Aeronautica et Astronautica Sinica,1980,1(1):1-6. |
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| Authors: | Yin Xieyuan |
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| Institution: | The Science and Technology University of China |
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| Abstract: | This paper presents a, simplified approximate analytical method for predicting vortex-lift and centre of pressure; on the slender wing at high angle of attack, and proposes two empirical correlations as well. In comparison with other methods and experimental data, this method provides good accuracy and suits for preliminary aerodynamic design. |
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