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提出了一种柔性气囊环括式微型旋翼飞行体结构设计,利用气动外形的被动自适应变形吸收气体压力载荷对机体产生的扰动作用,改善飞行体的抗气流扰动能力。分析了各个结构参数、制造材料以及环境条件对于飞行体模型在阵风下产生的气动力参数的影响,完成了机体在水平方向和垂直方向受力的正交试验分析,讨论了影响飞行性能最显著的因素,找到在参数取值范围内的最佳响应结果,优化了设计参数之间的组合方式。分析结果表明,通过优化飞行体结构设计参数和材料特性,可以明显改善飞行体在阵风扰动下的飞行性能,产生有助于平稳飞行的气动力参数,提高飞行体的抗扰动能力。
A flexible airbag ring-type micro-rotor flying body structure design is proposed. The passive adaptive deformation of the aerodynamic profile absorbs the disturbance caused by the gas pressure load on the airframe and improves the anti-air-flow disturbance of the airframe. The influence of various structural parameters, manufacturing materials and environmental conditions on the aerodynamic parameters generated by gusts of the flying body model was analyzed. The orthogonal experimental analysis on the horizontal and vertical forces of the aircraft body was completed. The most significant influence on the aerodynamic performance was discussed Factor, find the best response within the parameter range, and optimize the way the design parameters are combined. The analysis results show that by optimizing the structural design parameters and material properties of the flying body, the flying performance of the flying body under the gust disturbance can be obviously improved, the aerodynamic parameters contributing to the smooth flight can be improved, and the anti-disturbance capability of the flying body can be improved.