c ―airfoil chord Cl ―airfoil lift c

c ―airfoil chord
Cl ―airfoil lift coefficient
Cl,max ―maximum lift coefficient
Cd ―airfoil drag coefficient
Cm ―quarter-chord pitching moment as labeled in Chapter
Cm,c/4 ―airfoil pitching moment about the quarter-chord
L/D ―aircraft lift-to-drag ratio
Re ―Reynolds number based on airfoil chord
s ―distance along airfoil surface
V ―local velocity on airfoil surface
V∞― freestream velocity
x distance along airfoil chord
α―angle of attack
α0l ―angle of attack for zero lift
GPMM ―Great Planes Model Manufacturing
HAWTs ―horizontal axis wind turbines
LSATs ―Low-Speed Airfoil Tests
LTPT ―Low-Turbulence Pressure Tunnel
R/C ―radio controlled
UAV― unmanned aerial vehicle
UIUC ―University of Illinois at Urbana-Champaign

結果 (中文) 1:

c ―airfoil 和弦Cl ―airfoil 升力系数Cl，―maximum 最大升力系数Cd ―airfoil 阻力系数Cm ―quarter 弦俯仰力矩作为标记在章厘米，俯仰力矩关于四分之一弦 c/4 ―airfoilL/D ―aircraft 升阻比Re ―Reynolds 数基于翼型弦s ―distance 沿翼型表面V ―local 速度对翼型表面V∞― 射流速度x 沿翼型弦距离Α―angle 的攻击Α0l ―angle 攻击为零的电梯GPMM ―Great 飞机模型制造HAWTs ―horizontal 轴风力发电机Lsat ―Low 低速翼型测试LTPT ―Low 湍流压力隧道R/C ―radio 控制UAV― 无人驾驶的飞行器伊利诺伊州厄巴纳-尚佩恩分校 UIUC ―University

結果 (中文) 3:

C―翼型弦
CL―翼型的升力系数
CL，最大―最大升力系数
CD―翼型阻力系数
厘米―季度弦俯仰力矩作为标记的第
厘米，C / 4―翼型俯仰力矩对季度弦
L / D―飞机的升阻比
重新―雷诺兹数基于翼型弦
―翼型表面的距离
V―翼型表面的局部流速
V∞―流速度
X距离沿着机翼弦
α―攻角
α0L―攻角为零升
GPMM―杰出的飞机模型制造
HAWTs―水平轴风力机
法学院―低速翼型试验
低温钝化晶体管―低湍流风洞压力
R / C―无线电控制的
无人机―无人飞行器―
UIUC伊利诺伊大学厄本那-香槟分校