雷诺数
翼
机械
航空航天工程
攻角
机翼外形
计算流体力学
雷诺平均Navier-Stokes方程
后掠翼
空气动力学
物理
数学
计算机科学
几何学
航空学
工程类
湍流
作者
Shigeru Sunada,T. Yasuda,Kunio Yasuda,Keiji Kawachi
出处
期刊:Journal of Aircraft
[American Institute of Aeronautics and Astronautics]
日期:2002-03-01
卷期号:39 (2): 331-338
被引量:125
摘要
The hydrodynamic characteristics of 20 wings of different airfoil shape were measured at Re = 4 X 103. Each wing had an aspect ratio At of 7.25. Comparison of the measured wing characteristics showed that hydrodynamic characteristics of a wing with a rectangular airfoil can be improved by either a camber of 5%, a sharp leading edge, or proper corrugation
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