NASA NACA-RM-L56D05-1956 当马赫数为1.41, 1.61和2.01时,带有多种垂直尾翼的45°后掠翼战斗机模型的静态横向稳定性和控制特性
Static lateral stability and control characteristics of a model of a 45 degrees swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01