A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme - Part 3: Secondary Flow Effects

IF 1.9 3区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Turbomachinery-Transactions of the Asme Pub Date : 2023-11-13 DOI:10.1115/1.4063511
Christian Morsbach, Michael Bergmann, Adem Tosun, Bjoern F. Klose, Patrick Bechlars, Edmund Kuegeler
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Abstract

Abstract In this final paper of a three-part series, we apply the numerical test rig based on a high-order discontinuous Galerkin scheme to the MTU T161 low-pressure turbine with diverging end walls at off-design Reynolds number of 90,000, Mach number of 0.6, and inflow angle of 41 deg. The inflow end wall boundary layers are prescribed in accordance with the experiment. Validation of the setup is shown against recent numerical references and the corresponding experimental data. Additionally, we propose and conduct a purely numerical experiment with upstream bar wake generators at a Strouhal number of 1.25, which is well above what was possible in the experiment. We discuss the flow physics at midspan and in the end wall region and highlight the influence of the wakes from the upstream row on the complex secondary flow system using instantaneous flow visualization, phase averages, and modal decomposition techniques.
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基于高阶不连续伽辽金格式大涡模拟的涡轮机械流动数值试验台-第3部分:二次流效应
本文采用基于高阶不连续伽辽金格式的数值试验台,对非设计雷诺数为90000、马赫数为0.6、来流角为41°的MTU T161低压涡轮进行了试验,并根据实验规定了来流端壁边界层。根据最近的数值参考和相应的实验数据,验证了该设置。此外,我们提出并进行了上游条形尾流发生器的纯数值实验,斯特劳哈尔数为1.25,远高于实验中可能的结果。我们讨论了跨中和端壁区域的流动物理,并利用瞬时流动可视化、相平均和模态分解技术强调了上游排尾迹对复杂二次流系统的影响。
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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.
期刊最新文献
A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme - Part 3: Secondary Flow Effects UNDERSTANDING THERMAL UNSTEADINESS IN ENGINE REPRESENTATIVE FLOWS AND IMPROVED METHODOLOGIES FOR DERIVED HEAT TRANSFER CALCULATIONS USING THIN-FILM GAUGES A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme - Part 1: Sliding Interfaces and Unsteady Row Interactions Aerodynamics of a High-Speed Low-Pressure Turbine Cascade With Cavity Purge and Unsteady Wakes A Numerical Test Rig for Turbomachinery Flows Based on Large Eddy Simulations With a High-Order Discontinuous Galerkin Scheme - Part 2: Shock-Capturing and Transonic Flows
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