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TIME-SPACE EVOLUTION OF SECONDARY FLOW STRUCTURES IN A TWO-STAGE LOW-SPEED TURBINE

机译:两级低速涡轮机中二次流动结构的时空演变

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The aim of this work is to highlight the unsteady effects related to wake-blade and blade rows interactions, but also the time-space evolution of secondary flow structures in a two-stage low-speed turbine model designed and constructed to perform unsteady measurements with different techniques. In this case attention has been addressed to the analysis of the flow field in the first stage of the turbine model. Measurements are performed with aerodynamic probes downstream of the first stator and using a single slanted hot-wire anemometer downstream of the first rotor. Time-dependent relative flow field downstream of the first rotor (obtained from phase-locked averaging technique) have been reconstructed for different relative positions between stator and rotor blades. From these results the time- dependent secondary flow vectors have been obtained as well. The mean reference flow used to determine the secondary flow structure has been evaluated for each frame by mass-averaged technique. The evolution of the secondary flow structure due to the influence of the upstream and downstream stators on the first rotor has been investigated. The main unsteady effects put in evidence the variation of the intensity and spatial extension of the vortex flow structure.
机译:这项工作的目的是突出与唤醒叶片和叶片行相互作用相关的不稳定效果,也是在设计和构造的两级低速涡轮机模型中的二次流动结构的时空演变,以执行不稳定的测量不同的技术。在这种情况下,已经注意到涡轮机模型的第一阶段流场的分析。使用第一定子下游的空气动力学探针进行测量,并使用第一转子下游的单个倾斜的热线风速计。已经重建了第一转子下游(从锁相平均技术获得的时间)的相对流场,用于定子和转子叶片之间的不同相对位置。从这些结果中,也获得了时间依赖性的二次流量矢量。通过质量平均技术评估了用于确定次要流动结构的平均参考流程。研究了由第一转子上游和下游定子的影响引起的二次流动结构的演变。主要的不稳定效应掌握了涡流结构的强度和空间延伸的变化。

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