NASA NACA-RM-L57C20-1957 在高亚音速下,测定35°后掠翼上尾翼开缝扩散器结构横向控制和铰链力矩特性的研究结果
Results of an investigation at high subsonic speeds to determine lateral-control and hinge-moment characteristics of a spoiler-slot-deflector configuration on a 35 degrees sweptback wing