飞机尾坞,the tail dock of plane
1)the tail dock of plane飞机尾坞
2)tailless aircraft无尾飞机
1.Fault-tolerant reconfigurable control of tailless aircraft based on self-adaptive PID technology;基于自适应PID技术的无尾飞机容错重构控制
2.A drag rudder is mostly used by tailless aircraft.阻力方向舵在无尾飞机上得到广泛的应用。
3.The W-shaped tailless aircraft has not stabilizer and vertical tail,and it is based on the design of forward-swept wing and the integrated design of blended wing-fuselage.W型无尾飞机基于前掠翼及翼身融合的一体化设计,取消了平尾和垂尾,可大幅降低雷达反射截面积,减轻结构重量;同时具有亚声速气动效率高、横航向操纵面效率高的优势。
英文短句/例句

1.For straight-winged tailless airplanes, only the negative camber satisfies the conditions for flight.对直机翼无尾飞机,只有负弯度才满足飞行条件。
2.Research on Flight Dynamic Analysis and Flight Simulation Research for Unmanned Aerial Vehicle Without Empennage;无尾式无人机飞行动力学分析及飞行仿真研究
3.the tail assembly of an aircraft飞机的机尾装配组件.
4.aircraft wake turbulence avoidance防止飞机进入前机尾流
5.The alternate lift and descent of the nose and tail of an airplane.(飞机)摇晃飞机机头机尾交替下沉
6.A spar that connects the tail surfaces and the main structure of an airplane.尾桁连接飞机的尾部表面和机身的桁
7.The wings and tails help the aircraft take off,机翼和机尾帮助飞机起飞,
8.(aeronautical) pertaining to the tail section of a plane.(航空)与飞机的尾部相关。
9.vapour trails,eg those left in the sky by high-flying aircraft蒸汽尾迹(如飞机在高空飞行留下的)
10.vapour trail( trail of condensed water left in the sky by a high-flying aircraft)雾化尾迹(飞机在高空飞行时留下的).
11.Flight Test Technique for Certain Model Airplane's Stall/Spin Motion某型飞机模型失速/尾旋飞行试验技术
12.unprotected aircraft无飞行安全设备的飞机
13.The tail is fixed on the model plane with nails模型飞机的尾部被钉在机身上。
14.the vertical airfoil in the tail assembly of an aircraft.飞机尾部组成部分的垂直机翼。
15.a roBot airplane无线电操纵飞机,无人飞机
16.To swing the tail of an airplane from side to side in order to reduce speed.摆尾航行,曲折航行使飞机尾翼左右摆动以减慢飞行速度
17.a tail - heavy cargo plane.一架尾部太重的货运飞机
18.the horizontal stabilizer and elevator in the tail assembly of an aircraft.飞机尾部的水平稳定器和升降舵。
相关短句/例句

tailless aircraft无尾飞机
1.Fault-tolerant reconfigurable control of tailless aircraft based on self-adaptive PID technology;基于自适应PID技术的无尾飞机容错重构控制
2.A drag rudder is mostly used by tailless aircraft.阻力方向舵在无尾飞机上得到广泛的应用。
3.The W-shaped tailless aircraft has not stabilizer and vertical tail,and it is based on the design of forward-swept wing and the integrated design of blended wing-fuselage.W型无尾飞机基于前掠翼及翼身融合的一体化设计,取消了平尾和垂尾,可大幅降低雷达反射截面积,减轻结构重量;同时具有亚声速气动效率高、横航向操纵面效率高的优势。
3)aircraft spin飞机尾旋
4)Jet flow fields飞机尾焰
5)aircraft tail assembly飞机尾部
6)aircraft trail飞机尾迹
延伸阅读

无尾飞机无尾飞机taillessairplane没有水平尾翼和鸭翼的飞机。它的俯仰平衡和操纵靠机翼后缘升降副翼来完成(见鸭式飞机)。由于取消平尾和机身载荷减小,结构重量轻。但是,为保持飞机平衡须付出一定的阻力代价;并且起飞着陆性能差。为了改善起飞着陆性能,无尾飞机通常采取较大的机翼面积。将飞机重心移到气动中心之后,可克服配平阻力大的缺点,再配以前缘增升装置,进一步改进机动性和起飞着陆性能。