NASA NACA-RM-L9K11-1950 通过NACA机翼流量方法对带有1/4弦倾斜后缘襟翼和配平片的35°后掠角的NACA 65-009机翼模型空气动力特性的测量 NASA NACA-TR-661-1939 带有普通和分裂式襟翼的NACA 23012机翼可变密度风洞试验 NASA NACA-MR-L5L11-1946 对装配有XF6U-1飞机开缝襟翼和普通NACA低阻力翼剖面的两个NACA低...
These airfoils are designated by a 4-digit number followed by a dash and a 2-digit number (that is, NACA 0012-63). The first two digits are zero for a symmetrical airfoil and the second two digits indicate the thickness-chord ratio. The first digit after the dash is a _eading-edge ...