The application of composites molding by vacuum-only cure technology in SUAV airframe is presented.
介绍袋压法成型复合材料在小型无人机机体结构中的应用情况。
The lateral-direct aerodynamic data of a SUAV without any aileron with different dihedrals and vertical-tail areas were obtained through an aerodynamic estimation method.
通过理论计算，定量地研究了小型无副翼电动无人机的横航向操稳特性，对不同机翼上反角和垂尾面积进行了横航向模态特性计算与分析。
应用推荐