NASA NACA-RM-L9A07-1949 当雷诺数大约为6.0x10(指数6)时,带有42°后掠角有前缘和圆弧翼剖面的机翼副翼和尾翼特性的低速研究
Low-speed investigation of aileron and spoiler characteristics of a wing having 42 degrees sweepback of the leading edge and circular-arc airfoil sections at Reynolds numbers of approximately 6.0 x 10(exp 6)