2016
DOI: 10.1016/j.ijmultiphaseflow.2015.09.014
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Cavitating flow around a scaled-down model of guide vanes of a high-pressure turbine

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Cited by 35 publications
(21 citation statements)
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“…There is also a third mechanism, the side-entrant jet ( Foeth et al, 2008;Ji et al, 2013;Peng et al, 2016 ), which is associated with the part of the re-entrant flow that has a strong spanwise velocity component such as in hydrofoils. Decaix and Goncalves (2013) reported on the presence of an oblique mode of the cavity oscillations and Timoshevskiy et al (2016) concluded that the oblique mode of sheet cavity oscillations associated with the development of the spanwise instability exists for all test objects independent of their shape. Because of the similarity between the side-entrant jet to the re-entrant jet, the side-entrant jet is not discussed in further detail.…”
Section: Introductionmentioning
confidence: 99%
“…There is also a third mechanism, the side-entrant jet ( Foeth et al, 2008;Ji et al, 2013;Peng et al, 2016 ), which is associated with the part of the re-entrant flow that has a strong spanwise velocity component such as in hydrofoils. Decaix and Goncalves (2013) reported on the presence of an oblique mode of the cavity oscillations and Timoshevskiy et al (2016) concluded that the oblique mode of sheet cavity oscillations associated with the development of the spanwise instability exists for all test objects independent of their shape. Because of the similarity between the side-entrant jet to the re-entrant jet, the side-entrant jet is not discussed in further detail.…”
Section: Introductionmentioning
confidence: 99%
“…The experiments were carried out using the cavitation rig at the Institute of Thermophysics SB RAS, described in detail in [9]. The test object was a reduced model of the Francis turbine guide vane with a chord length 𝐶 = 100 mm and a maximum thickness 𝐻 max = 0.2149𝐶, described in detail in [10]. The hydrofoil was installed at an angle of attack 𝛼 = 9°.…”
Section: Methodsmentioning
confidence: 99%
“…Here, we consider a cavitating flow around the 2D symmetric hydrofoil section mimicking a guide vane of a Francis turbine (Timoshevskiy et al 2016) that was installed in the test channel of the cavitation tunnel in Kutateladze Institute of Thermophysics SB RAS (Kravtsova et al 2014). Its chord length C = 100 mm and aspect ratio is 0.8 (Fig.…”
Section: Piv Approachmentioning
confidence: 99%