NASA NACA-RM-L8D30-1948
在雷诺数为2.9x10(指数6)至8.4x10(指数6)时,前缘高升力装置和分裂式襟翼对带有圆弧翼剖面且展弦比为3.4的矩形机翼最大升力及横向特性的影响
Effect of leading-edge high-lift devices and split flaps on the maximum-lift and lateral characteristics of a rectangular wing of aspect ratio 3.4 with circular-arc airfoil sections at Reynolds numbers from 2.9 x 10(exp 6) to 8.4 x 10(exp 6)