首页> 外文会议>ASME turbo expo: turbine technical conference and exposition >EXPERIMENTAL INVESTIGATIONS ON EFFECTS OF UNSTEADY WAKES ON THE SECONDARY FLOWS IN THE LINEAR T106 TURBINE CASCADE
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EXPERIMENTAL INVESTIGATIONS ON EFFECTS OF UNSTEADY WAKES ON THE SECONDARY FLOWS IN THE LINEAR T106 TURBINE CASCADE

机译:T106涡轮叶栅内非定常尾迹对二次流影响的实验研究。

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The present work extends previous investigations on the secondary flows around a steady base flow to detailed time-averaged and time-resolved flow field measurements up- and downstream of a low pressure turbine (LPT) cascade. Unsteady inflow was generated by a moving bar system. The inlet conditions were determined using single hot wire anemometry and a pitot probe. Further detailed measurements of the . three-dimensional flow field were carried out downstream of the cascade with triple hot wire anemometry, a conventional five hole pressure probe, and a dynamic pressure probe equipped with a single Kulite sensor. All measurements have been performed with and without moving bars. Cases with different Strouhal numbers and flow coefficients have been considered by varying the pitch of the moving bars between 40 mm and 80 mm and circumferential speed between 10m/s and 20m/s in order to investigate the influence of unsteady inflow in particular on the secondary flow field near the endwalls. It turned out that the effects of the incoming wakes are evident in the time-accurate data in terms of their interaction with secondary flow vortices. On a time-averaged basis, however, the influence of the incoming wakes on the secondary flow field turned out to be small for the small inlet boundary layer.
机译:本工作将先前对围绕稳定基流的二次流的研究扩展到了低压涡轮(LPT)级联上游和下游的详细的时间平均和时间分辨的流场测量。动杆系统产生不稳定的流入。使用单根热线风速仪和皮托管探头确定入口条件。进一步详细的测量。在三级热线风速仪,传统的五孔压力探头和配备单个Kulite传感器的动压探头的级联下游进行三维流场。所有测量都在有和没有移动棒的情况下进行。通过研究在40 mm和80 mm之间移动动杆的螺距以及在10m / s和20m / s之间改变圆周速度来考虑具有不同Strouhal数和流量系数的情况,以便研究不稳定流入的影响,特别是对二次流入的影响。端壁附近的流场。事实证明,在时间精确的数据中,传入尾流的影响与次级流涡流之间的相互作用十分明显。但是,按时间平均,对于较小的入口边界层,进入的尾流对次级流场的影响很小。

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