Predicting High-Lift Low-Pressure Turbine Cascades Flow Using Transition-Sensitive Turbulence Closures

IF 1.9 3区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Turbomachinery-Transactions of the Asme Pub Date : 2014-05-01 DOI:10.1115/1.4025224
R. Pacciani, M. Marconcini, A. Arnone, F. Bertini
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引用次数: 20

Abstract

This paper discusses the application of different transition-sensitive turbulence closures to the prediction of low-Reynolds-number flows in high-lift cascades operating in low-pressure turbine (LPT) conditions. Different formulations of the well known γ-R˜eθt model are considered and compared to a recently developed transition model based on the laminar kinetic energy (LKE) concept. All those approaches have been coupled to the Wilcox k-ω turbulence model. The performance of the transition-sensitive closures has been assessed by analyzing three different high-lift cascades, recently tested experimentally in two European research projects (Unsteady Transition in Axial Turbomachines (UTAT) and Turbulence and Transition Modeling for Special Turbomachinery Applications (TATMo)). Such cascades (T106A, T106C, and T108) feature different loading distributions, different suction side diffusion factors, and they are characterized by suction side boundary layer separation when operated in steady inflow. Both steady and unsteady inflow conditions (induced by upstream passing wakes) have been studied. Particular attention has been devoted to the treatment of crucial boundary conditions like the freestream turbulence intensity and the turbulent length scale. A detailed comparison between measurements and computations, in terms of blade surface isentropic Mach number distributions and cascade lapse rates will be presented and discussed. Specific features of the computed wake-induced transition patterns will be discussed for selected Reynolds numbers. Finally, some guidelines concerning the computations of high-lift cascades for LPT applications using Reynolds-averaged Navier–Stokes (RANS)/unsteady RANS (URANS) approaches and transition-sensitive closures will be reported.
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利用过渡敏感湍流闭包预测高升程低压涡轮叶栅流动
本文讨论了不同过渡敏感湍流闭包在低压涡轮(LPT)条件下高升程叶栅低雷诺数流动预测中的应用。考虑了众所周知的γ-R ~ eθt模型的不同公式,并将其与最近基于层流动能(LKE)概念开发的过渡模型进行了比较。所有这些方法都与Wilcox k-ω湍流模型相结合。通过分析三种不同的高升力叶栅,对过渡敏感闭包的性能进行了评估,最近在两个欧洲研究项目(轴向涡轮的非定常转捩(UTAT)和特殊涡轮机械应用的湍流和转捩建模(TATMo))中进行了实验测试。这三种叶栅(T106A、T106C和T108)载荷分布不同,吸力侧扩散系数不同,在稳定进流工况下,其特点是吸力侧边界层分离。研究了稳定和非稳定两种流入条件(由上游通过尾迹引起)。特别注意的是处理关键的边界条件,如自由流湍流强度和湍流长度尺度。在叶片表面等熵马赫数分布和叶栅递减率方面,测量和计算之间的详细比较将被提出和讨论。对于选定的雷诺数,将讨论计算的尾迹诱导过渡模式的具体特征。最后,本文将介绍一些关于LPT应用中使用reynolds -average Navier-Stokes (RANS)/非定常RANS (URANS)方法和过渡敏感闭包计算高升力叶栅的指导原则。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
CiteScore
4.70
自引率
11.80%
发文量
168
审稿时长
9 months
期刊介绍: The Journal of Turbomachinery publishes archival-quality, peer-reviewed technical papers that advance the state-of-the-art of turbomachinery technology related to gas turbine engines. The broad scope of the subject matter includes the fluid dynamics, heat transfer, and aeromechanics technology associated with the design, analysis, modeling, testing, and performance of turbomachinery. Emphasis is placed on gas-path technologies associated with axial compressors, centrifugal compressors, and turbines. Topics: Aerodynamic design, analysis, and test of compressor and turbine blading; Compressor stall, surge, and operability issues; Heat transfer phenomena and film cooling design, analysis, and testing in turbines; Aeromechanical instabilities; Computational fluid dynamics (CFD) applied to turbomachinery, boundary layer development, measurement techniques, and cavity and leaking flows.
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