NASA NACA-RM-A52K14-1953 在马赫数为1.4和1.9时,采用十字形机翼和矩形飞机尾翼形式的空对空导弹空气动力特性的实验研究
Experimental investigation of the aerodynamic characteristics of an air-to-air missile employing cruciform wings and tail of rectangular plan form at Mach numbers of 1.4 and 1.9