NASA NACA-TN-3843-1956 被机翼垂直位置和与机身直径和机翼翼展比率的变化影响的60°三角形机翼飞机模型的实验性稳定状态偏航导数
Experimental steady-state yawing derivatives of a 60 degrees delta-wing model as affected by changes in vertical position of the wing and in ratio of fuselage diameter to wing span