Page 188 - Fluid mechanics, heat transfer, and mass transfer
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MIXING
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                         Power number as a function of Reynolds number for different turbine impellers. D: impeller diameter; W: blade width.
             FIGURE 6.1
                  sensitive to anything that changes flow patterns    & Figure 6.1 illustrates the relationship between N Re
                  produced by the impeller.                            and P o .
                 & Power number is inversely proportional to N Re in the  & In most industrial situations, power number of an
                  laminar regime, has weaker dependence on N Re in the  impeller is constant under turbulent conditions. This
                                                                       means that under turbulent conditions, power is pro-
                  transition regime, and is almost independent of N Re
                  under highly turbulent conditions.                   portionaltofluiddensityandindependentofviscosity.
                 & Power number will be low for impellers that produce  & Under laminar conditions, power number is inversely
                  a uniform flow with relatively low levels of local    proportional to Reynolds number, which means that
                  turbulence (e.g., narrow blade hydrofoils, P o ffi 0.3)  power is proportional to viscosity and independent of
                  and much higher for impellers that produce a highly  density.
                  nonuniform flow with high local turbulence intensity  & Under transitional conditions, impeller power is
                  (e.g., the disk turbine, P o ffi 5).                   influenced by both viscosity and density.
                 & It is used to predict impeller power directly and  & Under turbulent conditions, typical power numbers
                  torque indirectly.                                   are listed in Table 6.1 for different impeller designs.
               . How is power number related to Reynolds number for  . What is pumping number/flow number?
                mixing?                                                               N Q ¼ Q=ND :           ð6:7Þ
                                                                                                3
                                              m
                                         n
                              P o ¼ KðN Re Þ ðN Fr Þ :  ð6:5Þ
                                                                     & It is a dimensionless number used to represent actual
                 & K, n, and m are constants, whosevalues depend on the
                                                                       flow during mixing in a vessel.
                  type of impeller. For example, for a propeller with a
                  pitch equal to the diameter, n ¼ 1 and K ¼ 41,
                  according to one reference, based on experimental
                                                                 TABLE 6.1  Power Numbers for Different Impeller Designs
                  data.
                                                                                            Number         Power
                 & The Froude number correlates the effects of gravi-
                                                                 Impeller Type             of Blades       Number
                  tational forces and it becomes significant only when

                  the propeller disturbs the liquid surface. Below  45 pitched blade turbine  4             1.37
                  Reynolds numbers of about 300, the Froude number  Straight blade turbine    4             3.96
                                                                 Straight blade turbine       6             4.92
                  is found to have little or no effect and
                                                                 Disk turbine                 6             5.0
                                            n
                                 P o   KðN Re Þ :       ð6:6Þ    Hydrofoil impeller           3             0.31
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