首页> 外文会议>ASME (American Society of Mechanical Engineers) Turbo Expo 2002: Turbomachinery >EXPERIMENTAL INVESTIGATION OF TURBINE WAKE FLOW BY INTERFEROMETRICALLY TRIGGERED PIV AND LDV MEASUREMENTS
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EXPERIMENTAL INVESTIGATION OF TURBINE WAKE FLOW BY INTERFEROMETRICALLY TRIGGERED PIV AND LDV MEASUREMENTS

机译:干涉触发的PIV和LDV测量对涡轮尾流的实验研究。

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The process of vortex shedding had been investigated in a a linear turbine blade cascade by non- invasive optical measurement techniques. The experiments were carried out in the wake behind a linear arrangement of turbine profiles (VKI-1) with a chord length of 58mm at an isentropic exit Mach number of 0.7 and a Reynolds number of 9.75x10~5. Shedding frequency was approx. 18.2kHz. Density fluctuations in the vortex street were measured by guiding the beam of a Laser Vibrometer (LV) through the turbine blade cascade behind the trailing edge and a frequency analysis was performed. These interferometrically detected density fluctuations had then been used to trigger two-dimensional velocity measurements by Particle Image Velocimetry (PIV) and Laser Doppler Velocimetry (LDV) in the turbine wake flow, by means of an analog filter. This resulted in phase resolved measurements of the flow field during vortex shedding at this high frequency. Results of these velocity measurements within the wake flow are presented with a decomposition of the velocity into mean, periodic and turbulent components performed.
机译:已经通过非侵入式光学测量技术在线性涡轮叶片级联中研究了涡旋脱落的过程。实验是在涡轮机轮廓(VKI-1)的线性布置之后进行的,尾翼的弦长为58mm,等熵出口马赫数为0.7,雷诺数为9.75x10〜5。脱落频率为约。 18.2kHz。通过引导激光振动计(LV)的光束通过后缘后面的涡轮叶片级联,测量涡街的密度波动,并进行了频率分析。然后,这些干扰物检测到的密度波动已通过模拟滤波器通过涡轮机尾流中的粒子图像测速(PIV)和激光多普勒测速(LDV)触发了二维速度测量。这导致在此高频下涡旋脱落过程中流场的相位分辨测量。尾流中这些速度测量的结果将速度分解为平均,周期性和湍流分量。

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