Steady and Unsteady Numerical Characterization of the Secondary Flow Structures of a Highly Loaded Low-Pressure Compressor Stage

IF 1.3 Q2 ENGINEERING, AEROSPACE
Riccardo Toracchio, Fabrizio Fontaneto, Koen Hillewaert
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引用次数: 0

Abstract

This paper presents the numerical characterization of a highly loaded compressor by means of 3D unsteady RANS simulations. The focus is on critical flow structures and their evolution at different operating points of the machine. First, the numerical setup and mesh quality are presented to support the reliability of the provided results. The comparison against experiments is then described for this purpose. Later, a full description of the unsteady behavior of the machine is provided, giving special attention to the two regions where the most critical features are expected: the rotor hub wall and the casing. Rotor–stator interactions are then investigated and the role of the inlet guide vane (IGV) is finally discussed. Results are analyzed at design and near-stall conditions, with a focus on the behavior close to the stability limit at 100% speed.
高负荷低压压气机级二次流结构的定常与非定常数值表征
本文采用三维非定常RANS模拟方法对高负荷压气机进行了数值表征。重点是在机器的不同工作点的关键流动结构及其演变。首先,提出了数值设置和网格质量来支持所提供结果的可靠性。然后为此目的描述与实验的比较。后来,提供了机器的非定常行为的完整描述,特别注意两个区域,其中最关键的特征是预期:转子轮毂壁和机匣。然后研究了转子-定子相互作用,最后讨论了进口导叶的作用。在设计和接近失速条件下分析结果,重点关注在100%速度下接近稳定极限的行为。
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
2.30
自引率
21.40%
发文量
29
审稿时长
11 weeks
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