Optimal Movable Wing Tip Strake
Optimal Movable Wing Tip Strake
复制标题
最佳可动翼尖边条
DOI:
10.2514/1.c031014
复制
发表时间:
2011
影响因子:
2.2
通讯作者:
V. Nikolic
中科院分区:
文献类型:
--
作者:
V. Nikolic
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