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飞行器滚转尾翼设计

Xiao-min ZHANG,Shan LU,Xiao-ni WANG

兵器装备工程学报（2017）

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Abstract
采用自由滚转尾翼技术是解决鸭式布局导弹横滚控制的有效途径,针对某试飞器助推飞行段需求,设计了一型滚转尾翼.试验结果表明,滚转尾翼设计合理,性能良好,成功用于飞行试验.更多还原
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