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Lagrangian Coherent Structures in Tandem Flapping Wing Hovering

机译:串联拍打翼悬停中的拉格朗日相干结构。

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摘要

Lagrangian Coherent Structures (LCS) of tandem wings hovering in an inclined stroke plane is studied using ImmersedBoundary Method (IBM) by solving two dimensional (2D) incompressible Navier-Stokes equations.Coherent structures responsible for the force variation are visualized by calculating Finite Time Lyapunov Exponents (FTLE),and vorticity contours.LCS is effective in determining the vortex boundaries,flow separation,and the wing-vortex interactions accurately.The effects of inter-wing distance and phase difference on the force generation are studied.Results show that in-phase stroking generates maximum vertical force and counter-stroking generates the least vertical force.In-phase stroking generates a wake with swirl,and counter stroking generates a wake with predominant vertical velocity.Counter stroking aids the stability of the body in hovering.As the hindwing operates in the wake of the forewing,due to the reduction in the effective Angle of Attack (AoA),the hindwing generates lesser force than that of a single flapping wing.
机译:利用ImmersedBoundary方法(IBM)研究了二维(2D)不可压缩的Navier-Stokes方程,研究了在倾斜的行程平面内盘旋的双翼机翼的拉格朗日相干结构(LCS),并通过计算有限时间Lyapunov可视化了引起力变化的相干结构指数(FTLE)和涡度等值线.LCS有效地准确确定涡旋边界,流分离和机翼-涡流相互作用。研究了机翼间距离和相差对力产生的影响。相向行程产生最大的垂直力,逆向行程产生最小的垂直力。相向行程产生带有漩涡的尾流,逆向行程产生具有主要垂直速度的尾流。反向行程有助于身体在悬停时的稳定性。后翼在前翼后运行,由于有效攻角(AoA)减小,后翼产生比单个襟翼的力量小。

著录项

  • 来源
    《仿生工程学报(英文版)》 |2017年第2期|307-316|共10页
  • 作者单位

    Department of Applied Mechanics,Indian Institute of Technology Madras,Chennai,Tamil Nadu,India;

    Department of Applied Mechanics,Indian Institute of Technology Madras,Chennai,Tamil Nadu,India;

  • 收录信息 中国科学引文数据库(CSCD);中国科技论文与引文数据库(CSTPCD);
  • 原文格式 PDF
  • 正文语种 eng
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