NASA NACA-RM-L58C18-1958 当马赫数为1.41和2.01时,机翼和水平尾翼垂直位置对梯形机翼飞机模型静态横向及航向稳定性的影响
Effects of vertical location of the wing and horizontal tail on the static lateral and directional stability of a trapezoidal-wing airplane model at Mach numbers of 1.41 and 2.01