柔性翼挥拍运动惯性力及气动力实验测量与分析

Experimental measurement and analysis of inertia force and aerodynamic force in flapping motion of flexible wing

  • 摘要: 在蝙蝠扑翼运动过程中,惯性力和气动力往往同时存在。为研究蝙蝠柔性膜翼挥拍运动的气动特性,需从耦合的扑翼惯性力和气动力中分离出气动力。本文搭建了基于多目视觉的拍摄平台,以获取不同属性的柔性膜翼挥拍运动图像,使用多目视觉算法重构了柔性膜翼变形,从变形中计算惯性力。通过六维力传感器获得了柔性膜翼实时受力,从中消除惯性力后得到气动力,并分析了惯性力与气动力之间的关系。经短梁标准模型验证,采用该方法重构的最大变形误差约为2.36%。研究结果表明:大柔性膜翼在挥拍运动中显著变形,变形程度与惯性力和气动力相关;随着膜翼厚度增大,惯性力和气动力都有不同程度提高。

     

    Abstract: Inertia force and aerodynamic force are often coupled in flapping motion. In order to study the aerodynamic characteristics of a bat flexible membrane wing in flapping motion, it is necessary to separate the inertia force and the aerodynamic force to obtain the aerodynamic force. By setting up a photographic platform based on multi-vision, images of flexible membrane wings with different properties were captured, and a multi-vision algorithm was used to reconstruct the deformation of the flexible membrane wing, so the inertia force can be calculated from the deformation. A six-axis force sensor was used to obtain the real-time force of the flexible membrane wing, then the aerodynamic force can be obtained by eliminating the inertia force, and the law between the inertia force and the aerodynamic force was analyzed. A standard model verifies that the deformation error of this method is 2.36%. The results show that the highly flexible wing membrane has a significant deformation during the flapping process, which is related to both inertia force and aerodynamic force. And with the increase of the thickness of the wing membrane, the inertia force and the aerodynamic force are increased to different extents.

     

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