NASA NACA-RM-L50E26-1950 在根据装有火箭发动机的飞机模型决定的跨音速和亚音速时,有不同展弦比和NACA 65A系列的不同厚弦比翼剖面的矩形机翼滚转阻尼
Damping in roll of rectangular wings of several aspect ratios and NACA 65A-series airfoil sections of several thickness ratios at transonic and supersonic speeds as determined with rocket-powered models