通过有限元方法探究了机翼上气动力和惯性力对结构变形的影响.研究表明扑翼机翼产生的气动力和惯性力大小在同一量级.机翼惯性力对机翼结构变形具有不可忽视的影响.当机翼处于水平位置时机翼气动力对结构变形贡献最大,同时合力产生的最大变形也出现在机翼水平位置.仿生扑翼机翼结构变形研究为高升力、低能耗扑翼机翼的设计提供了理论指导. The influence of aerodynamic force and inertial force on the deformation of the wing was investigated by finite element method. The results show that the aerodynamic force and inertial force generated by the flapping wing are in the same order of magnitude. Ignoring the impact.When the wing is in the horizontal position, the aerodynamic force of the wing contributes the most to the deformation of the structure, and the maximum deformation caused by the resultant force also appears in the horizontal position of the wing.The research on the deformation of the biomimetic flapping-wing structure for the high-lift and low- The wing design provides theoretical guidance.