1995
DOI: 10.1016/0009-2509(94)00250-u
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The characteristics of aerated 12- and 18-blade Rushton turbines at transitional Reynolds numbers

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Cited by 15 publications
(7 citation statements)
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“…The standard Rushton turbine design with a discblade intercepting angle of 90° was used to validate the accuracy of the system. The power number of the Rushton turbine found in this work was 5.47, which is in close agreement with those published in the literature (Bates et al, 1963;Houcine et al, 2000;Nienow et al, 1995;Wu et al, 2001). In the turbulent region with the Reynolds number ranging from 2×10 4 to 6.6×10 4 , the power number of all impellers showed insignificant variations with increasing Reynolds number (Figure 3).…”
Section: Power Numbersupporting
confidence: 90%
“…The standard Rushton turbine design with a discblade intercepting angle of 90° was used to validate the accuracy of the system. The power number of the Rushton turbine found in this work was 5.47, which is in close agreement with those published in the literature (Bates et al, 1963;Houcine et al, 2000;Nienow et al, 1995;Wu et al, 2001). In the turbulent region with the Reynolds number ranging from 2×10 4 to 6.6×10 4 , the power number of all impellers showed insignificant variations with increasing Reynolds number (Figure 3).…”
Section: Power Numbersupporting
confidence: 90%
“…Among radial impellers, the Scaba impeller has shown some promising characteristics in both single and multiphase systems as well as coaxial systems 17 . Nienow et al 18 stated that the gas handling capacity of the Scaba impeller was superior to the Rushton turbine in a system containing a non‐Newtonian liquid. In another study, Amanullah et al 19 showed the inferiority of the Rushton turbine compared to the Scaba impeller in Xanthan gum fermentation.…”
Section: Introductionmentioning
confidence: 99%
“…A few studies investigate the effect of number of impeller blades on power consumption in batch stirred vessels and show the power consumption to go up with increasing number of blades (Bates et al, 1963;Nienow et al, 1995). This could be explained in terms of the increase in total drag acting on impeller with increase in number of blades.…”
Section: Introductionmentioning
confidence: 99%