2014
DOI: 10.1088/1755-1315/22/3/032046
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Comprehensive experimental and numerical analysis of instability phenomena in pump turbines

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Cited by 26 publications
(12 citation statements)
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“…Gentner et al 53 further found that this vortex structure is induced by the cross flow from the hub to the shroud at the leading edge. Figure 8 of Gentner et al 53 shows the amplitude of the secondary flow in the vaneless space based on particle image velocimetry (PIV) measurement, in which the averaged circumferential velocity has been subtracted. Near runway, the secondary flow is strong in two regions: one at the leading edges and another one at the center of blade channel.…”
Section: Vortex Formationmentioning
confidence: 95%
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“…Gentner et al 53 further found that this vortex structure is induced by the cross flow from the hub to the shroud at the leading edge. Figure 8 of Gentner et al 53 shows the amplitude of the secondary flow in the vaneless space based on particle image velocimetry (PIV) measurement, in which the averaged circumferential velocity has been subtracted. Near runway, the secondary flow is strong in two regions: one at the leading edges and another one at the center of blade channel.…”
Section: Vortex Formationmentioning
confidence: 95%
“…The elimination of the vortex structure at specific sites can be also employed as a design criteria of pump turbine. Gentner et al 53 proposed that the S-shaped characteristics at some guide vane openings can be eliminated by avoiding the formation of such kind of leading-edge vortex at runaway during the design stage. Gentner et al 53 further found that this vortex structure is induced by the cross flow from the hub to the shroud at the leading edge.…”
Section: Vortex Formationmentioning
confidence: 99%
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“…Staubli [11] pointed out that the instability of S characteristic area is related to the slope of the unit characteristic curve under no-load conditions. Gentner [12] found that the blocking effect of the vortex flow in the vaneless zone under no-load opening is an important source of the instability of the S area. The study of vortex flow in the vaneless zone has also been reported by many scholars [13][14][15].…”
Section: Introductionmentioning
confidence: 99%
“…Hasmatuchi 17 found in the experiment that the pressure fluctuation of a turbine in the guide vane region will increase, and the low frequency component in the pressure fluctuation will increase evidently when the turbine steps into the ''S'' region. Gentner et al 18,19 has evaluated several CFD procedures with different approaches for the calculation of the described instabilities in pump and turbine operation. Sun et al 20 Studied the S character of a pump turbine with discrete-event simulation (DES) model.…”
Section: Introductionmentioning
confidence: 99%