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。
Results of destructive test on hexagon section boom show that the test resu...
对六边形臂进行破坏试验，试验结果与计算值相当吻合。
Results of destructive test on hexagon section boom show that the test resu...
对六边形臂进行破坏试验，试验结果与计算值相当吻合。
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