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1)  twin-finned tail
双垂尾
1.
Self-balancing load calibration on aircraft twin-finned tail
飞机双垂尾载荷自平衡校准
2)  twin-vertical tail buffet
双垂尾抖振
1.
The numerical investigation of twin-vertical tail buffet of strake-wing configuration;
边条翼布局双垂尾抖振的数值模拟
3)  twin-finned aircraft
双垂尾式飞机
4)  twin-finned tail
双垂直尾翼(火)
5)  vertical tail
垂尾
1.
In the traditional assembly technology of aerofoils and vertical tails, the measurement of pose and print of the specified points are realized by the indicator of horizontal points and elastic striker respectively, which is not precise and difficult to be flexible.
在传统的机翼、垂尾装配中,姿态测量与测量点打制分别由特别设计的水平测量点指示器和弹簧打点器实现,不仅精度不高,而且难于实现柔性化。
2.
According to the phenomenon of vertical tail vibration divergence encountered during development test of an air- craft,a study on the flutter analysis and vibration data measured in flight test are performed.
针对某型机调整试飞中遇到的垂尾发散振动现象,对该机的颤振分析和试飞实测数据进行了研究。
6)  V-shape vertical tail
V型垂尾
补充资料:双[1-(4-二甲氨基)苯基2-苯基1,2-二硫代乙烯合镍]
分子式:
CAS号:

性质:紫黑色单斜晶体。熔点277~278℃。溶于苯、甲苯、三氯甲烷等大多数有机溶剂。红外频率υ(C=S)1190、1165、1140cm-1,红外频率υ(S-C-C-S)880cm-1。由对二甲氨基安息香、五硫化二磷在二噁烷(二氧六环)中反应后,加入镍(Ⅱ)盐溶液制得。用作光学非线性材料。

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