阻力方向舵在无尾飞机上得到广泛的应用。
对直机翼无尾飞机，只有负弯度才满足飞行条件。
For straight - winged tailless airplanes, only the negative camber satisfies the conditions for flight.
考虑到无尾飞机在起飞离地前的纵向构型和参数与空中控制律有所不同，设计使用机轮承载开关进行控制律切换。
On the other hand, switch is used in control laws transformation, because longitudinal structure and parameters on land are different from those in air.
飞机设计师经常使用比例模型，并在案件的X - 36战斗机敏捷性研究无尾飞机，这是因为大的，因为它得到了。
Aircraft designers routinely use scale models, and in the case of the X-36 Tailless Fighter Agility Research Aircraft, that's as big as it got.
611所(成都飞机设计院)早在1960年代末就开始研究鸭式无尾三角翼布局飞行平台。
611 institute (Chengdu Aircraft Design institute) initiated studied on the "tailless delta-canard" wing planform as early as the late 1960s.
611所(成都飞机设计院)早在1960年代末就开始研究鸭式无尾三角翼布局飞行平台。
611 institute (Chengdu Aircraft Design institute) initiated studied on the "tailless delta-canard" wing planform as early as the late 1960s.
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