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Characteristics of the Tip Leakage Vortex in a Low-Speed Axial Compressor

机译:低速轴流式压缩机尖端泄漏涡的特性

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摘要

The flowfields in the tip region of the rotor passage are investigated from a large-scale low-speed axial compressor test at both the design and near-stall conditions by using stereoscopic particle image velocimetry. The characteristics of the tip leakage vortex (TLV) are analyzed based on the variations of its trajectory, concentration, size, streamwise velocity, and the blockage effect, which are extracted from both the ensemble- and conditional-averaged results. According to the ensemble-averaged performance of the TLV, its evolution procedures can be divided into several distinct flow phases. As the flow phase of the TLV changes, its mean flow characteristics also change accordingly. The TLV is inherently unsteady and features unsteady behaviors of vortex wandering, splitting, and breakdown, which have profound effects to its mean flow characteristics.
机译:通过使用立体粒子图像测速技术,在设计和接近失速条件下,通过大规模低速轴流压气机试验研究了转子通道尖端区域中的流场。根据其轨迹,浓度,大小,流向速度和阻塞效应的变化来分析尖端泄漏涡(TLV)的特性,这些变化是从集合平均和条件平均结果中提取的。根据TLV的整体平均性能,其演变过程可以分为几个不同的流动阶段。随着TLV的流动相变化,其平均流动特性也随之变化。 TLV本质上是不稳定的,并且具有涡流徘徊,分裂和破裂的不稳定行为,这对其平均流量特性产生了深远的影响。

著录项

  • 来源
    《AIAA Journal》 |2007年第4期|p.870-878|共9页
  • 作者单位

    Beijing University of Aeronautics and Astronautics, 100083 Beijing, People's Republic of 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 航空、航天;航空;
  • 关键词

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