Li Hui, Su Xinrong, Yuan Xin
Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Department of Energy and Power Engineering, Tsinghua University, Beijing 100084, China.
Entropy (Basel). 2018 Dec 28;21(1):21. doi: 10.3390/e21010021.
In unshrouded turbine rotors, the tip leakage vortices develop and interact with the passage vortices. Such complex leakage flow causes the major loss in the turbine stage. Due to the complex turbulence characteristics of the tip leakage flow, the widely used Reynolds Averaged Navier-Stokes (RANS) approach may fail to accurately predict the multi-scale turbulent flow and the related loss. In order to effectively improve the turbine efficiency, more insights into the loss mechanism are required. In this work, a Delayed Detached Eddy Simulation (DDES) study is conducted to simulate the flow inside a high pressure turbine blade, with emphasis on the tip region. DDES results are in good agreement with the experiment, and the comparison with RANS results verifies the advantages of DDES in resolving detailed flow structures of leakage flow, and also in capturing the complex turbulence characteristics. The snapshot Proper Orthogonal Decomposition (POD) method is used to extract the dominant flow features. The flow structures and the distribution of turbulent kinetic energy reveal the development of leakage flow and its interaction with the secondary flow. Meanwhile, it is found that the separation bubble (SB) is formed in tip clearance. The strong interactions between tip leakage vortex (TLV) and the up passage vortex (UPV) are the main source of unsteady effects which significantly enhance the turbulence intensity. Based on the DDES results, loss analysis of tip leakage flow is conducted based on entropy generation rates. It is found that the viscous dissipation loss is much stronger than heat transfer loss. The largest local loss occurs in the tip clearance, and the interaction between the leakage vortex and up passage vortex promotes the loss generation. The tip leakage flow vortex weakens the strength of up passage vortex, and loss of up passage flow is reduced. Comparing steady and unsteady effects to flow field, we found that unsteady effects of tip leakage flow have a large influence on flow loss distribution which cannot be ignored. To sum up, the current DDES study about the tip leakage flow provides helpful information about the loss generation mechanism and may guide the design of low-loss blade tip.
在无罩涡轮转子中,叶尖泄漏涡会发展并与通道涡相互作用。这种复杂的泄漏流是涡轮级中主要的损失来源。由于叶尖泄漏流具有复杂的湍流特性,广泛使用的雷诺平均纳维 - 斯托克斯(RANS)方法可能无法准确预测多尺度湍流流动及相关损失。为了有效提高涡轮效率,需要更深入了解损失机制。在这项工作中,进行了延迟分离涡模拟(DDES)研究,以模拟高压涡轮叶片内部的流动,重点关注叶尖区域。DDES结果与实验结果吻合良好,与RANS结果的比较验证了DDES在解析泄漏流详细流动结构以及捕捉复杂湍流特性方面的优势。采用快照本征正交分解(POD)方法提取主导流动特征。流动结构和湍动能分布揭示了泄漏流的发展及其与二次流的相互作用。同时,发现叶尖间隙中形成了分离泡(SB)。叶尖泄漏涡(TLV)与上通道涡(UPV)之间的强烈相互作用是不稳定效应的主要来源,显著增强了湍流强度。基于DDES结果,基于熵产生率对叶尖泄漏流进行了损失分析。发现粘性耗散损失远大于传热损失。最大的局部损失发生在叶尖间隙,泄漏涡与上通道涡之间的相互作用促进了损失的产生。叶尖泄漏流涡减弱了上通道涡的强度,上通道流的损失减小。对比稳态和非稳态对流场的影响,发现叶尖泄漏流的非稳态效应对流场损失分布有很大影响,不容忽视。总之,当前关于叶尖泄漏流的DDES研究为损失产生机制提供了有用信息,并可能指导低损失叶片叶尖的设计。