Unsteady Wake-Blade Interaction: A Correlation Between Surface Pressure Fluctuations and Loss Generation

Author:

Biester Marc H.-O.1,Henke Michael1,Seume Jörg R.1,Gündogdu Yavuz2,Engel Karl2

Affiliation:

1. Leibniz Universität Hannover, Hannover, Germany

2. MTU Aero Engines GmbH, München, Germany

Abstract

This paper presents loss mechanisms associated with unsteady flows in axial turbines due to the interaction of wakes with downstream blade-rows. To evaluate the effect of wake induced loss mechanisms, extensive 3D-URANS computations of an 1.5-stage low pressure turbine rig have been performed. The investigation of the flow field shows how the wake influences well-known effects like the negative-jet effect and resulting flow structures. A detailed view on the impact of these time-dependent flow structures on the fluctuating pressure distribution on the blade is presented by evaluation in both, the time and frequency domains. The effects causing the fluctuations are identified in detail and attributed to their corresponding sources. Unsteady pressure induced by potential effects is distinguished from unsteadiness induced by wake passage. Regarding the latter, it is shown that the amplitude of the pressure fluctuations correlates with the instantaneous state of the wake. In order to describe this behavior, an analytical model is proposed and referred to as the conservation of wake circulation. The evaluation of the entropy generation caused by wake deformation allows the distinction of different loss mechanisms. Finally, an empirical correlation between the amplitude of pressure fluctuation and loss generation is shown.

Publisher

American Society of Mechanical Engineers

Cited by 5 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. On the Aeroacoustic Scaling of Axial Flow Turbines;International Journal of Gas Turbine, Propulsion and Power Systems;2024

2. Loss Assessment of the Axial-Gap Size Effect in a Low-Pressure Turbine;Journal of the Global Power and Propulsion Society;2021-01-26

3. Blade–Row Interactions in a Low Pressure Turbine at Design and Strong Off-Design Operation;Journal of Turbomachinery;2014-08-26

4. Unsteady Work Transfer Within a Turbine Blade Row Passage;Journal of Turbomachinery;2014-02-27

5. Modeling Vortex Generating Jet-Induced Transition in Low-Pressure Turbines;Journal of Turbomachinery;2014-01-02

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