Efficient aerodynamic optimization of turbine blade profiles: an integrated approach with novel HDSPSO algorithm

IF 1.7 4区 材料科学 Q3 MATERIALS SCIENCE, MULTIDISCIPLINARY Multidiscipline Modeling in Materials and Structures Pub Date : 2024-06-11 DOI:10.1108/mmms-02-2024-0051
Cheng Yan, Enzi Kang, Haonan Liu, Han Li, Nianyin Zeng, Yancheng You
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Abstract

PurposeThis paper delves into the aerodynamic optimization of a single-stage axial turbine employed in aero-engines.Design/methodology/approachAn efficient integrated design optimization approach tailored for turbine blade profiles is proposed. The approach combines a novel hierarchical dynamic switching PSO (HDSPSO) algorithm with a parametric modeling technique of turbine blades and high-fidelity Computational Fluid Dynamics (CFD) simulation analysis. The proposed HDSPSO algorithm introduces significant enhancements to the original PSO in three pivotal aspects: adaptive acceleration coefficients, distance-based dynamic neighborhood, and a switchable learning mechanism. The core idea behind these improvements is to incorporate the evolutionary state, strengthen interactions within the swarm, enrich update strategies for particles, and effectively prevent premature convergence while enhancing global search capability.FindingsMathematical experiments are conducted to compare the performance of HDSPSO with three other representative PSO variants. The results demonstrate that HDSPSO is a competitive intelligent algorithm with significant global search capabilities and rapid convergence speed. Subsequently, the HDSPSO-based integrated design optimization approach is applied to optimize the turbine blade profiles. The optimized turbine blades have a more uniform thickness distribution, an enhanced loading distribution, and a better flow condition. Importantly, these optimizations lead to a remarkable improvement in aerodynamic performance under both design and non-design working conditions.Originality/valueThese findings highlight the effectiveness and advancement of the HDSPSO-based integrated design optimization approach for turbine blade profiles in enhancing the overall aerodynamic performance. Furthermore, it confirms the great prospects of the innovative HDSPSO algorithm in tackling challenging tasks in practical engineering applications.
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涡轮叶片轮廓的高效气动优化:采用新型 HDSPSO 算法的综合方法
目的 本文探讨了航空发动机中使用的单级轴流式涡轮的气动优化问题。设计/方法/途径 本文提出了一种针对涡轮叶片轮廓的高效综合设计优化方法。该方法将新颖的分层动态切换 PSO(HDSPSO)算法与涡轮叶片参数建模技术和高保真计算流体动力学(CFD)仿真分析相结合。所提出的 HDSPSO 算法在三个关键方面对原始 PSO 进行了重大改进:自适应加速系数、基于距离的动态邻域和可切换学习机制。这些改进的核心思想是结合进化状态,加强蜂群内部的相互作用,丰富粒子的更新策略,在增强全局搜索能力的同时有效防止过早收敛。研究结果通过数学实验比较了 HDSPSO 和其他三种具有代表性的 PSO 变体的性能。结果表明,HDSPSO 是一种有竞争力的智能算法,具有显著的全局搜索能力和快速收敛速度。随后,基于 HDSPSO 的集成设计优化方法被应用于优化涡轮叶片轮廓。优化后的涡轮叶片厚度分布更均匀,载荷分布更合理,流动条件更好。重要的是,无论在设计工况还是非设计工况下,这些优化都显著提高了气动性能。 原创性/价值这些研究结果凸显了基于 HDSPSO 的涡轮叶片轮廓综合设计优化方法在提高整体气动性能方面的有效性和先进性。此外,它还证实了创新 HDSPSO 算法在解决实际工程应用中的挑战性任务方面的巨大前景。
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来源期刊
CiteScore
3.70
自引率
5.00%
发文量
60
期刊介绍: Multidiscipline Modeling in Materials and Structures is published by Emerald Group Publishing Limited from 2010
期刊最新文献
Reliability analysis of various modeling techniques for the prediction of axial strain of FRP-confined concrete High-temperature oxidation and gas thermal shock studies of IC10 simulated specimens with thermal barrier coatings Research on torque measurement in flight test for all-moving horizontal tail based on spiral driver Viscous fluid flow and heat transfer past a permeable wall jet with convective boundary conditions Efficient aerodynamic optimization of turbine blade profiles: an integrated approach with novel HDSPSO algorithm
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