top tail boom 顶桁架
ALU tail boom 铝合金尾管
bottom tail boom 下尾桁
tail-boom 尾撑
tail boom brace 尾撑杆
slender tail boom 细长尾撑
bi-tail-boom layout 双尾撑布局
high mounted tail boom 高置式尾梁
The aerodynamic forces on the tail boom have been calculated and their changes with the circulation control variables were drawn in curves.
根据测量数据计算出尾梁上气动力随环量控制参数的变化情况，并绘制成曲线。
The tail boom tapers from the main body to the swept-back, tapered fin with a rotor on the right. Two flats are mounted on the both side of the boom.
尾梁从机身渐细到后掠尾垂翼，尾螺旋桨在锥形尾垂翼右侧，二个尾平翼被装在尾梁两侧。
The design method of C/G composite tail boom of an unmanned air vehical is detailed in this paper. The result of strength test of the tail boom is also introduced.
本文较详细地介绍了小型无人机C／G复台材料尾撑杆的结构设计和工程计算方法，并给出了静力强度试验结果。
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