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A Deep Insight to Secondary Flows

机译:对次级流动深入了解

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摘要

Flow through turbine stages is three-dimensional and highly complex due to secondary flows, axial and tip clearances, 3D blades, rotational effects, varying fluid properties, turbulence effects, boundary layer development, etc. Secondary flows presence in turbines is identified as one of the main reason for losses and less efficiency performance. Hence in turbines, the need for understanding of secondary flows mechanisms and application of methods for their reduction is significant. This study is targeted to the discussion of secondary flows, аs follows: analysis of reasons for their development in turbine stages; influence on flow parameters distribution, efficiency of energy conversion and the overall aerodynamic performance of the turbo aggregate and ways to reduce their presence in the flow structure. As a result of the fulfilled intensive research works, a methodology for numerical modeling and mechanisms identification of secondary flows, through turbine channels, is attained also. Flow structures, specifics in aerodynamics, flow parameters distribution; interaction effects among vortices, core flow, endwalls and tip leaks, and many other flow features are discussed. An innovative approach to overcome reasons for secondary flows to appear and how to increase efficiency, have been studied and discussed.
机译:通过涡轮级的流动是次级流动,轴向和尖端间隙,3D叶片,旋转效应,不同的流体性质,湍流效应,边界层开发等引起的三维和高度复合。次级流量在涡轮机中被识别为一个损失和效率效率较少的主要原因。因此,在涡轮机中,需要了解二次流动机制和减少方法的应用是显着的。本研究旨在讨论二次流动,Аs遵循:分析其在涡轮机阶段发展的原因;对流动参数分布,能量转换效率的影响,涡轮增长的总空气动力学和降低流动结构存在的方法。由于集成的密集研究作品,通过涡轮机通道实现了用于数值建模和机制识别二次流动的方法。流动结构,空气动力学的细节,流量参数分布;换气,芯流,端壁和尖端泄漏的相互作用效果以及许多其他流特征。研究并讨论了克服次要流量的原因的创新方法以及如何提高效率。

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