Standard

Manipulating cavitation by a wall jet : Experiments on a 2D hydrofoil. / Timoshevskiy, Mikhail V.; Zapryagaev, Ivan I.; Pervunin, Konstantin S. и др.

в: International Journal of Multiphase Flow, Том 99, 01.02.2018, стр. 312-328.

Результаты исследований: Научные публикации в периодических изданияхстатьяРецензирование

Harvard

Timoshevskiy, MV, Zapryagaev, II, Pervunin, KS, Maltsev, LI, Markovich, DM & Hanjalić, K 2018, 'Manipulating cavitation by a wall jet: Experiments on a 2D hydrofoil', International Journal of Multiphase Flow, Том. 99, стр. 312-328. https://doi.org/10.1016/j.ijmultiphaseflow.2017.11.002

APA

Timoshevskiy, M. V., Zapryagaev, I. I., Pervunin, K. S., Maltsev, L. I., Markovich, D. M., & Hanjalić, K. (2018). Manipulating cavitation by a wall jet: Experiments on a 2D hydrofoil. International Journal of Multiphase Flow, 99, 312-328. https://doi.org/10.1016/j.ijmultiphaseflow.2017.11.002

Vancouver

Timoshevskiy MV, Zapryagaev II, Pervunin KS, Maltsev LI, Markovich DM, Hanjalić K. Manipulating cavitation by a wall jet: Experiments on a 2D hydrofoil. International Journal of Multiphase Flow. 2018 февр. 1;99:312-328. doi: 10.1016/j.ijmultiphaseflow.2017.11.002

Author

Timoshevskiy, Mikhail V. ; Zapryagaev, Ivan I. ; Pervunin, Konstantin S. и др. / Manipulating cavitation by a wall jet : Experiments on a 2D hydrofoil. в: International Journal of Multiphase Flow. 2018 ; Том 99. стр. 312-328.

BibTeX

@article{eec621df9b984ab0a8a1b7d678113ccb,
title = "Manipulating cavitation by a wall jet: Experiments on a 2D hydrofoil",
abstract = "We report on the experimental investigation of cavitating flow control over a 2D model of guide vanes of a Francis turbine by means of a continuous tangential injection of liquid along the foil surface. The generated wall jet, providing supplementary mass and momentum, issues from a nozzle chamber inside the hydrofoil through a spanwise slot channel on its upper surface. High-speed imaging was used to distinguish cavity flow regimes, study the spatial patterns and time dynamics of partial cavities, as well as to evaluate the characteristic integral parameters of cavitation. Time-resolved LIF visualization of the jet discharging from the nozzle was employed to check if the generated wall jet is stable and spanwise uniform. Hydroacoustic measurements were performed by a hydrophone to estimate how the amplitudes and frequencies of pressure pulsations associated with cavity oscillations change with the injection rate. A PIV technique was utilized to measure the mean velocity, its fluctuations and the dominant turbulent shear stress component, which were all compared for different flow conditions and with the results for the unmodified (standard) foil. The effect of injection rate on cavitation and flow dynamics was examined for three attack angles, 0, 3 and 9°, and a range of cavitation numbers corresponding to different regimes. The low-speed injection was shown to lead to an intensification of turbulent fluctuations in the boundary layer and shrinking of the attached cavity length by up to 25% compared to the case without injection. The injection with a high velocity, in turn, causes a rise of the local flow velocity and a reduction of turbulent fluctuations near the wall, which, consequently, increases the foil hydrodynamic quality at a relatively low energy consumption for generation of the wall jet. However, in this case the vapor cavity becomes longer. Thus, the low-speed injection turns out to be effective to mitigate cavitation but the injection at a high velocity is more preferable from the standpoint of the flow hydrodynamics. In the whole, the implemented control method showed to be quite an efficient tool to manipulate cavitation and hydrodynamic structure of the flow and, thereby, under certain conditions, to suppress the cavitation-caused instabilities.",
keywords = "Cavitation, Continuous tangential injection, Flow control, Frequency spectra analysis, Guide vane model, High-speed imaging, Instabilities, Partial/cloud cavities, PIV measurements, Pressure pulsations, Time-resolved LIF visualization, Wall jet, INSTABILITY, MECHANISM, CAVITY, Wall Jet, FLOW, High-speed Imaging, Time-resolved LiF visualization, HIGH-SPEED VISUALIZATION, CLOUD CAVITATION",
author = "Timoshevskiy, {Mikhail V.} and Zapryagaev, {Ivan I.} and Pervunin, {Konstantin S.} and Maltsev, {Leonid I.} and Markovich, {Dmitriy M.} and Kemal Hanjali{\'c}",
year = "2018",
month = feb,
day = "1",
doi = "10.1016/j.ijmultiphaseflow.2017.11.002",
language = "English",
volume = "99",
pages = "312--328",
journal = "International Journal of Multiphase Flow",
issn = "0301-9322",
publisher = "Elsevier",

}

RIS

TY - JOUR

T1 - Manipulating cavitation by a wall jet

T2 - Experiments on a 2D hydrofoil

AU - Timoshevskiy, Mikhail V.

AU - Zapryagaev, Ivan I.

AU - Pervunin, Konstantin S.

AU - Maltsev, Leonid I.

AU - Markovich, Dmitriy M.

AU - Hanjalić, Kemal

PY - 2018/2/1

Y1 - 2018/2/1

N2 - We report on the experimental investigation of cavitating flow control over a 2D model of guide vanes of a Francis turbine by means of a continuous tangential injection of liquid along the foil surface. The generated wall jet, providing supplementary mass and momentum, issues from a nozzle chamber inside the hydrofoil through a spanwise slot channel on its upper surface. High-speed imaging was used to distinguish cavity flow regimes, study the spatial patterns and time dynamics of partial cavities, as well as to evaluate the characteristic integral parameters of cavitation. Time-resolved LIF visualization of the jet discharging from the nozzle was employed to check if the generated wall jet is stable and spanwise uniform. Hydroacoustic measurements were performed by a hydrophone to estimate how the amplitudes and frequencies of pressure pulsations associated with cavity oscillations change with the injection rate. A PIV technique was utilized to measure the mean velocity, its fluctuations and the dominant turbulent shear stress component, which were all compared for different flow conditions and with the results for the unmodified (standard) foil. The effect of injection rate on cavitation and flow dynamics was examined for three attack angles, 0, 3 and 9°, and a range of cavitation numbers corresponding to different regimes. The low-speed injection was shown to lead to an intensification of turbulent fluctuations in the boundary layer and shrinking of the attached cavity length by up to 25% compared to the case without injection. The injection with a high velocity, in turn, causes a rise of the local flow velocity and a reduction of turbulent fluctuations near the wall, which, consequently, increases the foil hydrodynamic quality at a relatively low energy consumption for generation of the wall jet. However, in this case the vapor cavity becomes longer. Thus, the low-speed injection turns out to be effective to mitigate cavitation but the injection at a high velocity is more preferable from the standpoint of the flow hydrodynamics. In the whole, the implemented control method showed to be quite an efficient tool to manipulate cavitation and hydrodynamic structure of the flow and, thereby, under certain conditions, to suppress the cavitation-caused instabilities.

AB - We report on the experimental investigation of cavitating flow control over a 2D model of guide vanes of a Francis turbine by means of a continuous tangential injection of liquid along the foil surface. The generated wall jet, providing supplementary mass and momentum, issues from a nozzle chamber inside the hydrofoil through a spanwise slot channel on its upper surface. High-speed imaging was used to distinguish cavity flow regimes, study the spatial patterns and time dynamics of partial cavities, as well as to evaluate the characteristic integral parameters of cavitation. Time-resolved LIF visualization of the jet discharging from the nozzle was employed to check if the generated wall jet is stable and spanwise uniform. Hydroacoustic measurements were performed by a hydrophone to estimate how the amplitudes and frequencies of pressure pulsations associated with cavity oscillations change with the injection rate. A PIV technique was utilized to measure the mean velocity, its fluctuations and the dominant turbulent shear stress component, which were all compared for different flow conditions and with the results for the unmodified (standard) foil. The effect of injection rate on cavitation and flow dynamics was examined for three attack angles, 0, 3 and 9°, and a range of cavitation numbers corresponding to different regimes. The low-speed injection was shown to lead to an intensification of turbulent fluctuations in the boundary layer and shrinking of the attached cavity length by up to 25% compared to the case without injection. The injection with a high velocity, in turn, causes a rise of the local flow velocity and a reduction of turbulent fluctuations near the wall, which, consequently, increases the foil hydrodynamic quality at a relatively low energy consumption for generation of the wall jet. However, in this case the vapor cavity becomes longer. Thus, the low-speed injection turns out to be effective to mitigate cavitation but the injection at a high velocity is more preferable from the standpoint of the flow hydrodynamics. In the whole, the implemented control method showed to be quite an efficient tool to manipulate cavitation and hydrodynamic structure of the flow and, thereby, under certain conditions, to suppress the cavitation-caused instabilities.

KW - Cavitation

KW - Continuous tangential injection

KW - Flow control

KW - Frequency spectra analysis

KW - Guide vane model

KW - High-speed imaging

KW - Instabilities

KW - Partial/cloud cavities

KW - PIV measurements

KW - Pressure pulsations

KW - Time-resolved LIF visualization

KW - Wall jet

KW - INSTABILITY

KW - MECHANISM

KW - CAVITY

KW - Wall Jet

KW - FLOW

KW - High-speed Imaging

KW - Time-resolved LiF visualization

KW - HIGH-SPEED VISUALIZATION

KW - CLOUD CAVITATION

UR - http://www.scopus.com/inward/record.url?scp=85035112062&partnerID=8YFLogxK

U2 - 10.1016/j.ijmultiphaseflow.2017.11.002

DO - 10.1016/j.ijmultiphaseflow.2017.11.002

M3 - Article

AN - SCOPUS:85035112062

VL - 99

SP - 312

EP - 328

JO - International Journal of Multiphase Flow

JF - International Journal of Multiphase Flow

SN - 0301-9322

ER -

ID: 9673411