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Effect of unequal flapping frequencies on flow structures

机译:拍打频率不相等对流动结构的影响

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摘要

The effects of unequal pitching and plunging frequency on the flow structures around a flapping airfoil is investigated using the Digital Particle Image Velocimetry (DPIV) technique in the reduced frequency range of 0.31≤k≤6.26 corresponding to Strouhal number range of 0.1≤St≤1.0. The SD7003 airfoil model undergoes a combined flapping motion where the pitch leads the plunge with a phase angle of 90° in a steady current. The investigated cases are classified into five flow structure categories based on instantaneous and averaged vorticity patterns and velocity fields around and in the near-wake of the airfoil while the frequency of plunging motion was kept the same as the frequency of pitching motion. Example cases for each category were then investigated for unequal pitching and plunging frequencies and it is observed that employing unequal pitching and plunging frequencies for an oscillating airfoil may result in a change of flow structure category.
机译:使用数字粒子图像测速(DPIV)技术在降低的频率范围0.31≤k≤6.26(对应于Strouhal数范围0.1≤St≤1.0)中研究了不等的俯仰和俯冲频率对扑翼周围流动结构的影响。 。 SD7003机翼模型经历了组合的拍打运动,在恒定电流下,俯仰以90°的相位角引导切入点。根据瞬时和平均涡度模式以及翼型附近和接近尾流时的速度场,将被调查的情况分为五类流动结构类别,同时使俯冲运动的频率与俯仰运动的频率保持一致。然后研究每个类别的示例情况的俯仰和下降频率不相等,并且观察到,对于振荡翼型采用不相等的俯仰和下降频率可能会导致流结构类别的变化。

著录项

  • 来源
    《Aerospace science and technology》 |2014年第5期|39-53|共15页
  • 作者单位

    Department of Astronautical Engineering, Istanbul Technical University, Maslak-Ayazaga, Istanbul 34469, Turkey;

    Department of Astronautical Engineering, Istanbul Technical University, Maslak-Ayazaga, Istanbul 34469, Turkey;

  • 收录信息 美国《科学引文索引》(SCI);美国《工程索引》(EI);
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Pitching; plunging airfoil; P1V; Unequal oscillating frequency;

    机译:投球;翼型下降;P1V;振荡频率不相等;
  • 入库时间 2022-08-18 02:32:21

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