首页> 美国政府科技报告 >Wind-tunnel investigation of the effects of geometric dihedral on the aerodynamic characteristics in pitch and sideslip of an unswept- and a 45 degree sweptback-wing-fuselage combination at high subsonic speeds
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Wind-tunnel investigation of the effects of geometric dihedral on the aerodynamic characteristics in pitch and sideslip of an unswept- and a 45 degree sweptback-wing-fuselage combination at high subsonic speeds

机译:风洞隧道研究几何二面角对高亚音速下未扫掠和45度后掠翼机翼组合的俯仰和侧滑的气动特性的影响

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