1) aircraft horizontal stabilizer
飞机平尾
1.
Test and analysis on load bearing capability of hinge lug of aircraft horizontal stabilizer elevator
飞机平尾升降舵接头耳片承载能力分析与试验
2) aircraft horizontal tail
飞机水平尾翼
1.
A new health state recognition and diagnosis approach for the primordial acoustic emission signals from an aircraft horizontal tail is proposed,which uses wavelet packet transform and support vector machine to monitor effec- tively the aircraft key structure component fatigue damages,discover hidden trouble in early time and avoid fearful ac- cident from occurring.
对于采用先进声发射技术所监测到的某飞机水平尾翼的原始声发射信息,提出采用小波包分析与支持向量机相结合的方法对飞机水平尾翼的健康状况进行识别与诊断。
2.
The advanced AE technology is used to monitor the aircraft horizontal tail health state.
实验研究表明,该方法能很好地预测飞机水平尾翼的健康状态,具有较好的实用性,适用于强噪声环境中飞机结构部件的健康预测。
3) 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。
4) aircraft spin
飞机尾旋
补充资料：水平尾翼
见尾翼。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条