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              Fluid Mixing                                                                                 93

              coefficient K G a can entirely supercede any requirement
              for a particular type of visual description of the gas–liquid
              dispersion. In general, linear gas superficial velocity, nor-
              mally given the symbol F, in feet per second, is based on
              dividing the tank cross-sectional area by the flow of gas
              at the temperature and pressure of the gas at the midpoint
              of the tank. This quantity is very basic both in the scaleup
              correlation and in predicting the power imparted to the
              liquid by the gas stream.
                It is characteristic that this ratio F increases on scaleup,
              since if we maintain equal volumes of gas per volume of
              liquid per time on scaleup, which is necessary to provide  FIGURE  21  Schematic  representation  of  optimum  D /T  as  a
              the same stoichiometric percentage of gas absorbed from  function  of  flow  of  gas  compared  to  mixer  horsepower  input.
              the gas phase, then the linear velocity increases directly  Shaded area is optimum D /T. Two industrial examples, fermen-
                                                                tation and aeration of biological waste, are shown.
              proportional to the depth of the large tank.
                While the variables are many and complex, in a general
              concept, if the power in the tank is equal to the energy  sorption rate and the partical pressure in the incoming–
              provided by the gas stream, we will get a gas-controlled  outgoing gas stream, coupled with an estimate of the equi-
              flow pattern. This has different characteristic coefficients  librium partial pressure of gas related to the dissolved gas
              of the mass transfer rate than the case where the mixer  in the liquid, allows the calculation of the average con-
              horsepower  is  three  or  more  times  higher  than  the  gas  centration driving force and then the mass transfer coeffi-
              power. For radial flow impellers, this factor of three will  cient K G a when needed to provide that mass trasfer rate.
              provide a mixer-controlled flow pattern, which again, has  This then allows the mixer to be chosen for that particular
              different exponents on the correlating equation for mass  combination. It is typical to try different gas rates, differ-
              transfer coefficient K G a or K L a. To drive the gas down to  ent tank shapes, or perhaps different head pressures to see
              the bottom of the tank, below the sparge ring, the power  the effects on the mixer design and the cost for process
              level must be on the order of 5–10 times higher than the  optimization.
              gas power level.                                    Anotherconsiderationistheoptimumflow to fluidshear
                For axial flow impellers, the ratio of mixer power to  ratio involved for gas-liquid dispersion. Figure 21 shows
              gas stream power for a mixer-controlled flow pattern is  the optimum D/T for different combinations for gas flow
              approximately 8–10. This means that radial flow impellers  and mixer power level in conceptual form. At the left edge
              are more commonly used for gas–liquid dispersion than  of the curve, where gas rates are high and power levels are
              axial flow impellers.                              low, large D/T values are desired to produce high flow
                Figure 20 gives a typical curve for the effect of gas ve-  and low shear rates. In the middle of the graph, which is
              locity and power level on mass transfer coefficient K G a.  more common, where the gas flow pattern is controlled
              In a given application, knowledge of the required gas ab-  by the mixer, desired D/T values are very small (on the
                                                                order of 0.15–0.2). At the far right-hand side of the graph,
                                                                we have a mixer power level greater than 10 times the
                                                                gas power level, and it makes very little difference what
                                                                ratio of flow-to-fluid shear rate we have, as shown by the
                                                                effect of D/T . This relationship shows the difficulty in
                                                                comparing impellers in gas–liquid mass transfer systems,
                                                                because the comparison of fluid shear and fluid flow re-
                                                                quires a knowledge of the mixer power to gas flow ratio.
                                                                In addition, in a process such as fermentation, where there
                                                                are certain maximum shear rates possible without damag-
                                                                ing the organism, the D/T chosen for the process may not
                                                                be the optimum for the gas–liquid mass transfer step, and
                                                                correlations must be available for the effect of D/T ratio
                                                                on mass transfer coefficient to complete design of those
                                                                kinds of processes.
                                                                  Scaleupisnormallybasedonthefactthatthecorrelation
              FIGURE 20  Typical correlation of gas–liquid mass transfer co-
              efficient K G a as a function of impeller power and superficial gas  of K G a versus power per unit volume and superficial gas
              velocity.                                         velocity is the same for both pilot and full-scale tanks.
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