1996
DOI: 10.1002/cjce.5450740103
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An LDA study of the turbulent flow field in a baffled vessel agitated by an axial, down‐pumping hydrofoil impeller

Abstract: The turbulent flow of water in a cylindrical, baffled vessel with an axial flow hydrofoil impeller, either a Chemineer HE3 (CHE3) or a Prochem Maxflo T (PMT), has been studied using a laser Doppler anemometer. Using ensemble averaging, the mean axial and radial flow and the associated fluctuating components were obtained for the whole of the vessel; plus similar data for the tangential component close to the impeller. Assuming axial symmetry, flow rates were calculated as were flow numbers and circulation flow… Show more

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Cited by 106 publications
(72 citation statements)
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“…(10) is very similar to a relationship previously reported by Jaworski et al (1991) and Vrábel et al (2000) for axial-flow impellers:…”
Section: Experimental Validationsupporting
confidence: 89%
“…(10) is very similar to a relationship previously reported by Jaworski et al (1991) and Vrábel et al (2000) for axial-flow impellers:…”
Section: Experimental Validationsupporting
confidence: 89%
“…In particular the discharge angle varied from 7.5° with respect to the horizontal plane for C = T/4 down to 2.5° for C = T/2. Jaworski et al (1991) circulation from the vessel axis towards the walls. For the higher clearance the impeller stream turned upwards before reaching the base of the vessel, generating also a reverse flow directed radially from the walls towards the vessel axis at the base of the vessel.…”
Section: Classification Of Flow Instabilitiesmentioning
confidence: 99%
“…The results presented indicated that the flow is directed upward over the outer part of the impeller, but, as Kresta and Wood (1993a) point out, this was due to an error in Ranade and Joshi's labeling of coordinates in the article. The bulk-flow patterns with 45" PBTs were reported to be different for low and high off-bottom clearances by Jaworski et al (1991) for six-blade and Kresta and Wood (1993a) for four-blade turbines. Hockey and Nouri (1996) employed a six-blade 60" PBT and measured mean and rms velocities in the bulk flow and around the turbine using ensemble-averaged and angle-resolved LDA techniques, respectively, and reported a peak velocity of 0.55 Ali et al (1981) observed that only a single trailing vortex was formed at the trailing edge of a four-blade 45" PBT, while Kresta and Wood (1993a) reported that a trailing vortex extending over approximately 20% of the blade was formed at the lower tip of the blade and a smaller one at the top corner of the blade.…”
Section: Introduction and Brief Literature Surveymentioning
confidence: 99%