swept-wing transport 后掠翼运输机
swept-wing 后略翼
swept-wing layout 后掠翼布局
swept-wing aerodynamics [航] 后掠翼空气动力学
swept-wing-body combination 后掠机翼和机身组合体
variable-swept wing stage 变后掠翼级
forward-swept-wing configuration 前掠翼布局
a swept wing 机翼
ADJ (of an aircraft, winged missile, etc) having wings swept (usually) backwards (飞机、有翼导弹等)后掠机翼的
This article investigates the flow control technique of forward-swept wing blended body (FBB) tailless configuration by means of wind tunnel tests.
通过风洞试验研究了前掠翼融合体无尾气动布局(FBB布局)的流动控制技术。
For the aircraft with moderate swept wing, the main reasons of causing wing rock are the variations of roll damping moment with the Angle of attack and the sideslip Angle.
对具有中等后掠角机翼的飞机，产生机翼摇晃的主要原因是滚转阻尼力矩随迎角和侧滑角的变化。
The X-4's primary importance involved proving a negative, in that a swept-wing semi-tailless design was not suitable for speeds near Mach 1.
的X - 4的主要参与的重要性，证明1负，在这后掠翼半尾巴设计时并没有接近1马赫的速度合适。
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