Particle image velocimetry (2D-PIV) has been used for the investigation of the time averaged flow field inside the vaned diffuser of a centrifugal pump operating at best efficiency point. Pump performances and the diffuser flow field were analysed for three different vane setting angles. It was evidenced that the best efficiency point flow coefficient decreases with the diffuser setting angle reduction. A boundary layer thickness growth on the pressure side, which increases as the flow coefficient decreases, was also shown. No evident separation was ever seen on the diffuser vane suction side even with a sharp diffuser vane LE, used in a previous investigation. The total pressure loss coefficient, obtained from the classical expression proposed by Lieblein for linear cascades, was found to decrease as the setting angle increases. It was evidenced an influence of the diffuser vane setting angle on the impeller slip and an over-turning of the diffuser flow field, at mid-span, with an under-turning at the hub and the shroud, suggesting the occurrence of significant secondary flows.

Influence of the diffuser vane setting angle on the flow field in a radial pump

Boccazzi A;
2011

Abstract

Particle image velocimetry (2D-PIV) has been used for the investigation of the time averaged flow field inside the vaned diffuser of a centrifugal pump operating at best efficiency point. Pump performances and the diffuser flow field were analysed for three different vane setting angles. It was evidenced that the best efficiency point flow coefficient decreases with the diffuser setting angle reduction. A boundary layer thickness growth on the pressure side, which increases as the flow coefficient decreases, was also shown. No evident separation was ever seen on the diffuser vane suction side even with a sharp diffuser vane LE, used in a previous investigation. The total pressure loss coefficient, obtained from the classical expression proposed by Lieblein for linear cascades, was found to decrease as the setting angle increases. It was evidenced an influence of the diffuser vane setting angle on the impeller slip and an over-turning of the diffuser flow field, at mid-span, with an under-turning at the hub and the shroud, suggesting the occurrence of significant secondary flows.
2011
Istituto di Chimica della Materia Condensata e di Tecnologie per l'Energia - ICMATE
Inglese
ETC 2011 - Conference Proceedings
The 9th European Turbomachinery Conference
721
732
9789755613901
http://www.etc9.itu.edu.tr/
Sì, ma tipo non specificato
21-25/03/2011
Istanbul-Turkey
Boundary layer flow
Boundary layers
Pumps
Thermodynamics
Velocity measurement
1
none
Boccazzi A.; Sala R.; Gaetani P.
273
info:eu-repo/semantics/conferenceObject
04 Contributo in convegno::04.01 Contributo in Atti di convegno
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/61218
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