Cavitation Control on a 2D Hydrofoil through a Continuous Tangential Injection of Liquid: Experimental Study

被引:16
作者
Timoshevskiy, M. V. [1 ,2 ]
Zapryagaev, I. I. [1 ,2 ]
Pervunin, K. S. [1 ,2 ]
Markovich, D. M. [1 ,2 ,3 ]
机构
[1] Russian Acad Sci IT SB RAS, Kutateladze Inst Thermophys, Siberian Branch, 1 Lavrentyev Ave, Novosibirsk 630090, Russia
[2] Novosibirsk State Univ, Dept Phys, 2 Pirogov Str, Novosibirsk 630090, Russia
[3] Tomsk Polytech Univ, Inst Power Engn, 30 Lenin Ave, Tomsk 634050, Russia
来源
INTERNATIONAL CONFERENCE ON THE METHODS OF AEROPHYSICAL RESEARCH (ICMAR 2016) | 2016年 / 1770卷
基金
俄罗斯科学基金会;
关键词
CLOUD CAVITATION; UNSTEADY;
D O I
10.1063/1.4963968
中图分类号
O59 [应用物理学];
学科分类号
摘要
In the paper, the possibility of active control of a cavitating flow over a 2D hydrofoil that replicates a scaled down model of high-pressure hydroturbine guide vane (GV) was tested. The flow manipulation was implemented by a continuous tangential liquid injection at different flow rates through a spanwise slot in the foil surface. In experiments, the hydrofoil was placed in the test channel at the attack angle of 9. Different cavitation conditions were reached by varying the cavitation number and injection velocity. In order to study time dynamics and spatial patterns of partial cavities, high-speed imaging was employed. A PIV method was used to measure the mean and fluctuating velocity fields over the hydrofoil. Hydroacoustic measurements were carried out by means of a pressure transducer to identify spectral characteristics of the cavitating flow. It was found that the present control technique is able to modify the partial cavity pattern (or even totally suppress cavitation) in case of stable sheet cavitation and change the amplitude of pressure pulsations at unsteady regimes. The injection technique makes it also possible to significantly influence the spatial distributions of the mean velocity and its turbulent fluctuations over the GV section for non-cavitating flow and sheet cavitation.
引用
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页数:8
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