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Radial fluid migration and endwall blockage in axial flow rotors

机译:轴流转子中的径向流体迁移和端壁堵塞

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摘要

The article presents an analytical model for systematic investigation of the effects stimulating or retarding radial outward migration of fluid in the suction side (SS) boundary layer of the blades of axial flow rotors, contributing to increased near-tip loss and promoting tip stalling. With application of the model to an experimental case study, coupled with evaluation of detailed flow measurement data, it has been pointed out that the outward migration and near-tip accumulation of high-loss fluid are intensified by the controlled vortex design (CVD) style. This phenomenon is related to the SS outward flow associated with the vortices shed from the blade of spanwise changing circulation. It has been found that the outward migration, and consequently, the endwall blockage at the casing, becomes more pronounced as the intensity of shed vortices due to CVD increases. Based on experimental data, it has been pointed out that the increase in axial displacement thickness is approximately proportional to the radial gradient of blade circulation. Based on the purposeful use of the analytical model, forward blade sweep was found to be especially beneficial for the rotors of CVD, as a means for moderating outward migration along the suction surface.
机译:本文提出了一种分析模型,用于系统研究轴向流动转子叶片的吸入侧(SS)边界层中流体的径向向外迁移的刺激或延迟,从而增加了近尖端损失并促进了尖端失速。将该模型应用于实验案例研究,并结合详细的流量测量数据进行评估,已指出,通过控制涡流设计(CVD)方式可增强高损耗流体的向外迁移和近端堆积。这种现象与SS向外流动有关,SS向外流动与从翼展方向变化的循环叶片上喷出的涡流有关。已经发现,随着由CVD引起的脱落涡流的强度增加,向外迁移以及因此在壳体处的端壁堵塞变得更加明显。根据实验数据,已经指出轴向位移厚度的增加大约与叶片循环的径向梯度成比例。基于对分析模型的有目的利用,发现向前叶片扫掠对CVD的转子特别有利,因为它可作为减缓沿吸力面向外迁移的手段。

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