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CFD prediction of flutter of turbine blades and comparison with an experimental test case

机译:涡轮叶片颤振的CFD预测并与实验测试案例进行比较

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Last stage blades are a key element of steam turbines and in many ways determine the turbine configuration alongside with the overall turbine performance. The total efficiency of the low pressure turbine section can be increased by extending the last stage blades. The design process of such long blades involves a flutter analysis using CFD tools which have to be validated by measurements in test facilities under various operating conditions. Experimental data obtained from a subsonic wind tunnel with an oscillating turbine blade cascade, which is available at the Department of Power System Engineering at the University of West Bohemia, was compared with simulations in ANSYS CFX currently used in the Doosan ?koda Power. The paper provides a brief summary of experimental rig description, CFD tool setup and the results for the case of a travelling wave mode with the pure torsion motion of amplitude of 0.5°, Ma = 0.2, reduced frequency of 0.38 and angle of attack +5°.
机译:末级叶片是蒸汽涡轮机的关键要素,在许多方面决定着涡轮机的配置以及整个涡轮机的性能。低压涡轮机部分的总效率可以通过延长末级叶片来提高。这种长叶片的设计过程涉及使用CFD工具进行颤动分析,必须通过在各种操作条件下在测试设施中进行的测量来验证。西波西米亚大学电力系统工程系提供的具有振荡涡轮叶片级联的亚音速风洞获得的实验数据与目前在斗山?koda Power中使用的ANSYS CFX中的模拟进行了比较。本文简要介绍了实验装置的描述,CFD工具的设置以及行波模式下的结果,该行波模式的振幅为0.5°,Ma = 0.2,扭转频率为0.38,攻角为+5,纯扭转运动°。

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