一种无人直升机旋翼桨叶设计与动力学试验_无人机 螺旋桨 ...
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综上所述，本文基于某型号无人直升机平台的旋翼系统，对直升机旋翼桨叶进行了气动仿真计算并结合发动机分析其悬停效率，通过动特性试验，验证了仿真计算的正确性，为桨叶动力学计算提供了正确的依据，通过动力学计算，验证了该旋翼桨叶的设计合理性。
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