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Laser–doppler–velocimetry measurements in a one and a half stage transonic test turbine with different angular stator–stator positions

机译:在具有不同定子角定子位置的半跨音速测试涡轮中进行激光多普勒测速测量

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摘要

A one and a half stage transonic turbine was tested using a two component laser–doppler–velocimetry system. The measurements were carried out in order to record rotor phase resolved velocity, flow angle and turbulence distributions upstream and downstream of the second stator row at several different angular stator–stator positions (“clocking” positions). Altogether, the measurements downstream of the second stator were performed for ten different clocking positions and upstream of the second stator for two different clocking positions. These different clocking positions have a significant influence on the flow field upstream and downstream of the second stator. Furthermore error estimation and a discussion of the tracer particle response are discussed.
机译:使用两分量激光多普勒测速系统测试了一个半级跨音速涡轮机。为了记录转子相分辨速度,第二定子行上游和下游在几个不同的定子定子位置(“计时”位置)上游和下游的湍流分布,进行了测量。总之,针对十个不同的时钟位置进行第二定子下游的测量,针对两个不同的时钟位置进行第二定子上游的测量。这些不同的计时位置对第二定子上游和下游的流场具有重大影响。此外,还讨论了误差估计和对示踪剂颗粒响应的讨论。

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  • 来源
    《Experiments in Fluids》 |2007年第3期|385-393|共9页
  • 作者单位

    Institute for Thermal Turbomachinery and Machine Dynamics Graz University of Technology Inffeldgasse 25 8010 Graz Austria;

    Institute for Thermal Turbomachinery and Machine Dynamics Graz University of Technology Inffeldgasse 25 8010 Graz Austria;

    Institute for Thermal Turbomachinery and Machine Dynamics Graz University of Technology Inffeldgasse 25 8010 Graz Austria;

    Institute for Thermal Turbomachinery and Machine Dynamics Graz University of Technology Inffeldgasse 25 8010 Graz Austria;

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