Airfoil section characteristics at a low Reynolds number

被引:104
作者
Sunada, S
Sakaguchi, A
Kawachi, K
机构
[1] FUJI HEAVY IND CO LTD,UTSUNOMIYA,TOCHIGI 320,JAPAN
[2] UNIV TOKYO,ADV SCI & TECHNOL RES CTR,MEGURO KU,TOKYO 153,JAPAN
来源
JOURNAL OF FLUIDS ENGINEERING-TRANSACTIONS OF THE ASME | 1997年 / 119卷 / 01期
关键词
D O I
10.1115/1.2819098
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
The aerodynamic characteristics of airfoils operating at Re = 4 x 10(3) were examined, varying the parameters related to the airfoil shape such as thickness, camber and roughness. Airfoils with good aerodynamic performance at this Re have the following shape characteristics: (1) they are thinner than airfoils for higher Re numbers, (2) they have a sharp lending edge, and (3) they have a camber of about five percent with its maximum camber at about mid-chord. The characteristics of airfoils are strongly affected by leading edge vortices. The measured two-dimensional airfoil characteristics indicate that the planform, which greatly affects the flight performance of the the three-dimensional wing at high Reynolds numbers, has little effect on the flight performance at this Reynolds number.
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页码:129 / 135
页数:7
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