| 分离流中多段翼型的优化计算 |
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| 引用本文： | 曹建发,陈晏清. 分离流中多段翼型的优化计算[J]. 航空学报, 1990, 11(8): 313-319 |
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| 作者姓名： | 曹建发 陈晏清 |
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| 作者单位： | 北京航空航天大学(曹建发)，北京航空航天大学(陈晏清) |
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| 摘 要： | 本文给出带有分离流动的多段冀型的优化计算方法。以最大升力系数为目标函数,对前缘缝翼或襟翼的位置和偏角进行优化。文中对带有后缘富勒式襟翼的NLR 7301翼型和GA(W)-1翼型进行最大升力计算和优化计算,所得结果和实验值相比符合得较好。
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| 关 键 词： | 多段翼型 分离流 最大升力系数 优化 |
OPTIMIZATION OF MULTI-ELEMENT AIRFOILS FOR MAXIMUM LIFTS IN SEPARATED FLOWS |
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| Beijing University of Aeronautics and Astronautics Cao Jianfa and Chen Yanqing. OPTIMIZATION OF MULTI-ELEMENT AIRFOILS FOR MAXIMUM LIFTS IN SEPARATED FLOWS[J]. Acta Aeronautica et Astronautica Sinica, 1990, 11(8): 313-319 |
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| Authors: | Beijing University of Aeronautics and Astronautics Cao Jianfa and Chen Yanqing |
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| Affiliation: | Beijing University of Aeronautics and Astronautics Cao Jianfa and Chen Yanqing |
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| Abstract: | A theoretical method for optimizing multi-element airfoils in separated flow is presented to determine the optimum location and deflection angle of flap or slat relative to the main component corresponding to the optimum CLmax. We take the maximum lift coefficient as the objective function. This approach is used to calculate the maximum lifts of NLR 7301 airfoil and GA(w)-l airfoil. The optimum computations are carried out for GA (w)-l airfoil. The results of the calculations are in good agreement with the wind-tunnel testing results. |
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| Keywords: | multi-element airfoils separated flow maximum lift coefficient optimization. |
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