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The Determination of the Geometries of Multiple-Element Airfoils Optimized for Maximum Lift Coefficient

机译：确定最大提升系数的多元翼型几何形状的确定

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作者
Chen, A. W.;
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年度 1971
页码 1-9
总页数 9
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerodynamic coefficients ; Airfoils ; Lift ; Pressure distribution ; Optimization ; Reynolds number ; Skin friction ; Velocity distribution;

机译：气动系数;翼型;升力;压力分布;优化;雷诺数;表面摩擦;速度分布;
入库时间 2022-08-29 11:13:14

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1. EXPERIMENTAL DETERMINATION OF THE INFLUENCE OF TURBULENT SCALE ON THE LIFT AND DRAG COEFFICIENTS OF LOW REYNOLDS NUMBER AIRFOILS [J] . J.S.DELNERO, J.MARANON DI LEO, F.A.BACCHI, Latin American Applied Research . 2005,第3期

机译：实验确定湍流尺度对低雷诺数机翼的起升系数和阻力系数的影响
2. Experimental determination of the influence of turbulent scale on the lift and drag coefficients of low Reynolds number airfoils [J] . Delnero J. S., Mara?on di Leo J., Bacchi F. A., Latin American Applied Research . 2005,第3期

机译：湍流尺度对低雷诺数机翼升力和阻力系数影响的实验确定
3. OPTIMIZATION OF THE SLOT SUCTION OF AIR FROM A CIRCULAR VORTEX CELL ON A THICK NACA0022 AIRFOIL WITH A MAXIMUM LIFT-DRAG RATIO [J] . S. A. Isaev, E. I. Kalinin, A. G. Sudakov, Journal of engineering physics and thermophysics . 2015,第6期

机译：优化具有最大升降比的厚NACA0022机翼上圆形涡流细胞的吸入空气
4. A Surface Parameterization Method for Airfoil Optimization and High Lift 2D Geometries Utilizing the CST Methodology [C] . K. Lane, D. Marshall AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition . 2009

机译：利用CST方法进行机翼优化和高升程2D几何的表面参数化方法
5. OPTIMIZATION OF AIRFOILS FOR MAXIMUM LIFT. [D] . LIEBECK, ROBERT HAUSCHILD. 1968

机译：优化机翼以实现最大提升。
6. Optimized depth-resolved estimation to measure optical attenuation coefficients from optical coherence tomography and its application in cerebral damage determination [O] . Jian Liu, Ning Ding, Yao Yu, 2019

机译：用于测量光学相干断层扫描仪光学衰减系数的深度解析优化估计及其在脑损伤确定中的应用
7. Effects of Airfoil Thickness and Maximum Lift Coefficient on Roughness Sensitivity: 1997--1998 [O] . D M Somers 2005

机译：翼型厚度和最大升力系数对粗糙度灵敏度的影响：1997--1998

The Determination of the Geometries of Multiple-Element Airfoils Optimized for Maximum Lift Coefficient

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