首页> 外文期刊>Annals of the American Thoracic Society >Influence of Microstructures on Aerodynamic Characteristics for Dragonfly Wing in Gliding Flight
【24h】

Influence of Microstructures on Aerodynamic Characteristics for Dragonfly Wing in Gliding Flight

机译:微观结构对滑翔飞行蜻蜓翼的空气动力学特征的影响

获取原文
获取原文并翻译 | 示例
       

摘要

In this paper, the functionalities of microstructures for dragonfly wing during gliding flight are investigated. Three dragonfly-mimic airfoil-shaped wings with hybrid structures were designed and fabricated as: flat wing, zigzag-edged wing and zigzag-edged wing with pillar structure. Based on the wind tunnel experiments, the zigzag-edged wing structure significantly reduces the drag force in the gliding flight. Moreover, the drag reduction is more effective on the combination of the surface pillar and zigzag-edged structure. In addition, the zigzag-edged wing structure has less influence of Karman vortex street, and the surface pillars reduce the frictional drag and stabilized the streamline in the lower vortex region. Overall, the microstructure of the dragonfly wing is an important element in the aerodynamic study. These findings can enhance the knowledge of insect-mimic wing structure and facilitate the application of Micro Air Vehicle (MAV) in the gliding flight.
机译:本文研究了在滑动飞行期间蜻蜓翼微观结构的功能。 设计和制造具有混合动力车结构的三个蜻蜓 - 模拟翼型翅膀,如:扁平翼,锯齿翼翼和锯齿状边缘,带柱结构。 基于风洞实验,锯齿形边缘结构显着降低了滑动飞行中的阻力。 此外,减阻在表面柱和曲折边缘结构的组合上更有效。 此外,锯齿形边翼结构具有较小的Karman Vortex Street的影响,并且表面柱子会减少摩擦阻力并稳定下涡旋区域中的流线。 总的来说,蜻蜓翼的微观结构是空气动力学研究中的重要因素。 这些发现可以增强昆虫模拟机翼结构的知识,并促进微型空气车辆(MAV)在滑动飞行中的应用。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号