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High-resolution measurement and analysis of the transient secondary flow field in a turbine cascade

机译:涡轮叶栅瞬态二次流场的高分辨率测量和分析

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Combining an improved particle image velocimetry technique with a far-field microscope, a high-resolution quantitative measurement of the transient secondary flow field in an annular turbine cascade is conducted through moving the laser light sheet to follow the primary flow. The measuring results revealed the transient behavior and strong unsteadiness of the secondary flow in a cascade for the first time. It is confirmed that the suction side leg of the horseshoe vortex rotates around the passage vortex along the rotating direction of passage vortex. In the secondary flow of cascade, the formation, development and decay of Hopf bifurcations caused by the competition between the tensile deformation and the dissipation, have become a major behavior of vortex evolution. Driven by the interaction between the passage vortex and the suction side leg of the horseshoe vortex as well as the transverse pressure gradient, the passage vortex was pushed to the suction surface and ultimately formed the wall vortex. Furthermore, the strength of secondary vortex was enhanced with the increase of aerodynamic parameters, though the scale of vortex was gradually shrinking and the limit cycle concentrated at the core of vortex. However, no change happened to the location of vortex core and the structure of vortex. The computational fluid dynamics results revealed that the results using the SST k-ω model was the closest to the experiment results in the topological structure, the evolution process of secondary flow and the magnitude estimation, followed by those with the RNG k-ε model. The results with standard k-e model were clearly inconsistent with the experimental results.
机译:将改进的粒子图像测速技术与远场显微镜相结合,可以通过移动激光片来跟踪一次流动来对环形涡轮机叶栅中的瞬态二次流场进行高分辨率的定量测量。测量结果首次揭示了级联中二次流的瞬态行为和强烈的不稳定性。可以确认,马蹄涡流的吸入侧支腿沿着流道涡流沿着流道涡流的旋转方向旋转。在叶栅的二次流中,由拉伸变形和耗散之间的竞争引起的霍夫夫分支的形成,发展和衰变已经成为涡旋演化的主要行为。在通道涡流和马蹄涡流的吸力侧支腿之间的相互作用以及横向压力梯度的驱动下,通道涡流被推向吸力表面,最终形成壁涡。此外,尽管涡流的规模逐渐缩小,极限循环集中在涡流的核心,但随着空气动力学参数的增加,次级涡流的强度也随之增强。但是,涡旋芯的位置和涡旋结构没有变化。计算流体动力学结果表明,使用SSTk-ω模型的结果在拓扑结构,二次流的演化过程和幅值估计方面最接近于实验结果,其次是使用RNGk-ε模型的结果。标准k-e模型的结果显然与实验结果不一致。

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