提出了一种基于临界粘度模型和粗糙度高度预测的涡轮叶栅颗粒沉积预测方法

IF 1.9 3区 工程技术 Q3 ENGINEERING, MECHANICAL Journal of Turbomachinery-Transactions of the Asme Pub Date : 2023-10-12 DOI:10.1115/1.4063752
Hong Wang, Peilin He, Jialong Li, Huawei Lu
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引用次数: 0

摘要

颗粒沉积是涡轮叶栅中常见的现象。它可以改变表面状况,从而影响流动和传热。准确预测颗粒沉积和表面状况变化具有重要意义。本文提出了一种基于临界粘度沉积模型和粗糙度高度预测的组合颗粒沉积算法。它耦合了表面粗糙度对颗粒沉积的影响。采用新建立的组合模型进行颗粒沉积。讨论了其对联合模型涡轮叶栅的影响。结果表明:沉积主要集中在叶栅前缘和压力侧;由于惯性作用,小粒径颗粒主要沉积在吸力侧,大粒径颗粒主要沉积在压力侧。沉积数随颗粒直径的增大而增大。随着时间的推移,更多的颗粒沉积在壁面上,形成粗糙度高度,并呈现扩散特征。表面粗糙度和流动特性(包括分离涡和泄漏涡)对换热有促进作用,其中流型对换热效果起主导作用。此外,分离涡和泄漏涡对沉积分布有显著影响,特别是对于直径较小的颗粒
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A method proposed to predict particle deposition based on critical viscosity model and roughness height prediction in a turbine cascade
Abstract Particle deposition is a common phenomenon in a turbine cascade. It can change the surface condition, which influences the flow and heat transfer. It is very important to accurately predict the particle deposition and surface condition changes. In this study, a combined particle deposition algorithm is proposed based on the critical viscosity deposition model and roughness height prediction. It couples the influence of surface roughness into the particle deposition. The combined model newly developed is employed for the particle deposition. Its effects in a turbine cascade with the combine model is discussed. The results show the deposition is mainly concentrated on the leading edge of the cascade and the pressure side. Small diameter particles are mainly deposited on the suction side and the large are mainly deposited on the pressure side due to inertial effect. The deposition number increases with the particle diameter. As time goes by, more particles deposit on the wall, which builds roughness height and shows a spreading characteristic. Heat transfer is enhanced by the surface roughness and flow characteristics including separation vortex and leakage vortex, in which flow pattern may dominate the effect. In addition, the separation vortex and leakage vortex have a significant effect on the deposition distribution, especially for smaller diameter particles
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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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