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Title: Flow Analysis of Tandem Blades as the Outlet Vane of a Highly Loaded Compressor
题目：串列叶片作为高负荷压气机出口导叶的流动分析
Authors: LUO Qiao, LUO Lei, DU Wei,YAN Han, WANG Songtao, ZHOU Xun
作者：罗樵，罗磊，杜巍，闫晗，王松涛，周逊
单位：哈尔滨工业大学能源科学与工程学院
Journal of Thermal Science, 2024, 33(6): 2005-2018.
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Flow Analysis of Tandem Blades as the Outlet Vane of a Highly Loaded Compressor.pdf
摘要
Abstract: A tandem blade configuration is a significant flow control method that delays the onset of flow separation. This study numerically investigates the effects of diffusion factor and percentage pitch on the flow structure of tandem blades. Diffusion factors vary from 0.328 to 0.484. Percentage pitches change from 0.80 to 0.92. Results show that the loss coefficient increases with diffusion factor and decreases with percentage pitch. There is a hub-corner stall of the forward blade in all cases. Gap flow determines the rear blade corner separation. Varying the percentage pitch and diffusion factor changes the momentum distribution of the gap flow. Corner separation of the rear blade is inhibited as low-momentum gap fluids are involved in the passage vortex along with the hub-corner stall of the forward blade. Increasing diffusion factor causes a change in incidence at the leading edge of the rear blade, resulting in a variation at the corner separation of the rear blade. A tandem blade is compared with the reference outlet vane. The performance of the tandem blade is superior to that of the reference outlet vane in all incidences, with a 26.35% reduction in the loss coefficient and a 7.89% enhancement in the pressurization at the designed incidence. Tandem blades stall at positive incidence because of the hub-corner stall of the forward blade. The intensity of the gap flow increases with incidence, preventing corner separation of the rear blade at positive incidences.
摘要：串列叶片是一种可以延迟分离的流动控制方法。本研究利用数值方法探究了扩压因子和节距比对串列叶片流动结构的影响。单个叶片扩压因子从0.328变化到0.484。节距比从0.80变化到0.92。结果表明，损失系数随扩压因子的增加而增加，随节距比的增加而减小。前叶片叶根角区失速出现在所有研究的情况。间隙流决定了后叶片的角区分离情况。改变节距比和扩压因子会改变间隙流的动量分布。后叶片的角区分离会由于通道涡卷吸低动量间隙流和前叶片的叶根角区失速流体而受到抑制。增加扩压因子会导致后叶片的攻角发生变化，从而导致后叶片角区分离的变化。将串列叶片与参考的出口单列叶片进行对比。所有攻角下，串列叶片的性能都优于参考叶片。在设计攻角下，损失系数降低了26.35%，增压能力提高了7.89%。串列叶片在正攻角下的流动失稳是由前叶片的叶根角区失速造成的。间隙流的强度会随着攻角的增加而提高，从而防止后叶片在正攻角时发生角区分离。
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引用格式
LUO Qiao, LUO Lei, DU Wei,YAN Han, WANG Songtao, ZHOU Xun, Flow Analysis of Tandem Blades as the Outlet Vane of a Highly Loaded Compressor, Journal of Thermal Science, 2024, 33(6): 2005-2018.
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