首页> 外文会议>AIAA aerospace sciences meeting;AIAA SciTech forum >Flapping tandem-wing aerodynamics: dragonflies in steady forward flight
【24h】

Flapping tandem-wing aerodynamics: dragonflies in steady forward flight

机译:拍打串联翼的空气动力学特性:蜻蜓在稳定向前飞行中

获取原文

摘要

The study of tandem flapping wing aerodynamics of dragonflies in steady forward flight is presented here. CFD simulations of one forewing-hindwing pair are run using wing kinematics measured in experiments with free flying dragonflies. Wing kinematics were acquired from tests of dragonflies flying through a confined space using multiple high speed cameras, placed such that they could record the dragonfly's motion. The test results contain videos of dragonflies flying inverted as well as upright, and wing kinematics have been extracted for three inverted and two upright flights. In the inverted flights the upstroke is longer than the downstroke and the pitch angle of the forewing is lower during the downstroke than similar upright flights. Three simulations were run based on this kinematic information: one simulating upright flight, one simulating inverted flight, and one looking at the effect of changing relative downstroke duration. The simulation results indicate that the dragonflies are controlling the orientation of their wing such that they have a similar orientation relative to their velocity during the halfstroke when the wing is flapping down in the lab reference frame. In addition, decreasing relative downstroke duration increases peak and average lift, making it unclear why dragonflies use a longer downstroke than upstroke while flying upright.
机译:本文介绍了蜻蜓在稳定向前飞行中的串联拍打翼空气动力学的研究。使用在自由飞行的蜻蜓的实验中测得的机翼运动学来进行一对前-后翼对的CFD模拟。机翼运动学是通过使用多个高速摄像头对蜻蜓在密闭空间中飞行进行的测试而获得的,这些摄像头的位置可以记录蜻蜓的运动。测试结果包含蜻蜓倒立飞行和直立飞行的视频,并提取了三个倒立飞行和两次直立飞行的机翼运动学。在倒转的飞行中,向上行程比向下的行程长,并且在向下的行程中前爪的俯仰角比类似的垂直飞行时小。基于此运动学信息进行了三种模拟:一种模拟垂直飞行,一种模拟倒转飞行,另一种模拟改变相对下冲程持续时间的影响。仿真结果表明,蜻蜓正在控制其翅膀的方向,以使当翅膀在实验室参考系中向下扑打时,它们相对于它们的速度具有相似的方向。此外,减少相对的向下冲程持续时间会增加峰值和平均升力,这使得不清楚为什么蜻蜓在直立飞行时使用比向上冲程更长的向下冲程。

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