NASA NACA-RM-L55J25-1956 在高亚音速下,机身横截面形状和机翼高度对有45°后掠翼的飞机模型静态纵向和横向稳定特性影响的风洞研究
Wind-tunnel investigation at high subsonic speeds of some effects of fuselage cross-section shape and wing height on the static longitudinal and lateral stability characteristics of a model having a 45 degrees swept wing