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EXPERIMENTAL STUDY OF FLOW THROUGH A BLADE TRAILING EDGE WITH A WAVY PARTITION

机译:波浪形隔板沿滑道流动的实验研究

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摘要

Flow through a blade trailing edge passage has been experimentally investigated in this article. This rectangular passage is divided into two channels by either a straight or a 120° wavy partition. Fluid in the first channel was injected into the second channel via 14 openings (holes) distributed uniformly and in the crests and troughs for the wavy configuration. Particle image velocimetry and a charge coupled device camera were used in experiment, with Reynolds number varying from 1,800 to 6,700. Experimental results show that the wavy configuration produces an oscillation flow in the second channel. The cause for the oscillation may due to the 120° wavy partition causing shear-layer instabilities and the formation of spanwise eddies by the wavy board. Pictures from the charge coupled device camera revealed strong mixing in the trailing edge, and this mixing could enhance heat transfer, which was confirmed in previous research. The amplitude of oscillation depends on Reynolds number and hole positions. It was observed that the injection flow was not symmetric to the openings, and it was skewed to the direction of the first channel main flow. The ratio of flow rate through the outlet and the bleeding holes was from 1:1 to 1:3.
机译:本文已对通过叶片后缘通道的流动进行了实验研究。该矩形通道通过笔直的或120°的波浪形隔板分为两个通道。第一通道中的流体通过14个均匀分布的开口(孔)注入波状结构的波峰和波谷中,注入第二通道。实验中使用了粒子图像测速仪和电荷耦合器件照相机,雷诺数在1,800至6,700之间变化。实验结果表明,波浪形结构在第二个通道中产生振荡流。造成振荡的原因可能是由于120°的波浪形分隔引起剪切层不稳定性以及波浪形板形成翼展涡流。电荷耦合器件相机的图像显示出后缘强烈混合,这种混合可以增强热传递,这在先前的研究中得到了证实。振荡幅度取决于雷诺数和孔位置。观察到,注入流与开口不对称,并且偏向第一通道主流的方向。通过出口和放气孔的流量比为1:1至1:3。

著录项

  • 来源
    《Experimental Heat Transfer》 |2011年第3期|p.266-284|共19页
  • 作者

    S.-T. Ding; G. Li;

  • 作者单位

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beijing University of Aeronautics and Astronautics,Beijing, China;

    National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, Beijing University of Aeronautics and Astronautics,Beijing, China;

  • 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

    blade trailing edge; wavy partition; oscillation flow;

    机译:叶片后缘;波浪形隔板振荡流;
  • 入库时间 2022-08-18 00:20:51

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