Optimal Movable Wing Tip Strake

Optimal Movable Wing Tip Strake
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最佳可动翼尖边条

DOI:
10.2514/1.c031014
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发表时间:
2011
影响因子:
2.2
通讯作者:
V. Nikolic
V. Nikolic
中科院分区:
工程技术3区
文献类型:
--
作者:
V. Nikolic

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术语AR=展弦比,b=S b=跨度,mm CD=外形阻力系数CL=外形升力系数c=弦,mm ds=翼缘相对于翼弦面的角度(正,翼缘前缘向上),q=自由流动压,1 2 1V 2 1,kpa Re=基于机翼模型弦的雷诺数,1V1c=1 S=参考面积,m V1=自由流速度,m=S x,y,z=气动轴=攻角,deg=绝对粘度,N S=空气密度,kg=m
Nomenclature AR = aspect ratio, b=S b = span, mm CD = configuration drag coefficient CL = configuration lift coefficient c = chord, mm ds = angle of strake setting relative to wing chord plane (positive, strake leading edge up), q = freestream dynamic pressure, 1 2 1V 2 1, kPa Re = Reynolds number based on wing model chord, 1V1c= 1 S = reference area, m V1 = freestream velocity, m=s x, y, z = aerodynamic axes = angle of attack, deg = absolute viscosity, N s=m = air density, kg=m