Page 48 - Fluid mechanics, heat transfer, and mass transfer
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FLOW PHENOMENA    25

                                                                         and r and m are fluid density and viscosity,
                                                                         respectively.

                                                                              Superficial velocity; V ¼ «v;  ð2:15Þ
                                                                                                 0
                                                                          where v is the actual velocity.
                                                                      ðiiiÞ Impeller Reynolds number;
                                                                                        2
                                                                                 N Re ¼ D Nr=m;            ð2:16Þ
                              Equivalent diameter for annulus.
                  FIGURE 2.4
                                                                         where D is the impeller diameter and N is rpm.
                                             2  2
                  equivalent diameter; D e ¼ 4½pðD  d Þ=4Š=pðD þ dÞ  . What is boundary layer? Illustrate.
                                                                     & Flow far from the surface of a solid object is inviscid
                                      ¼ D d:            ð2:9Þ
                                                                       and effects of viscosity are manifest only in a thin
                                                                       layer near the surface where steep velocity gradients
                  Rectangular duct:
                                                                       occur.
                              D e ¼ 4LW=2ðL þ WÞ;      ð2:10Þ
                                                                     & Boundary layer is where the fluid is influenced by
                  where L is the length and W is the width of the duct.  friction with its boundaries. Flow is zero at the
                                                                       boundary and increases away from the boundary
                  Square duct:                                         until it reaches the mean or maximum velocity of
                                    D e ¼ L:           ð2:11Þ          the flow. The zone of flow velocity increase is called
                                                                       boundary layer.
              . Give the equation for hydraulic radius of a packed   & In other words, the thin layer where velocity de-
                bed.                                                   creases from the inviscid potential flow velocity to
                 r H ¼ðvolume of voidsÞ=ðvolume of bedÞ=               zero at solid surfaces is called boundary layer.
                                                                     & Development of boundary layer is illustrated in
                  ðwetted surfaceÞ=ðvolume of bedÞ¼ «=a;  ð2:12Þ       Figure 2.5.
                                                                   . State Bernoulli’s principle.
                where a is 6(1   «)/D p ¼ [«/6(1   «)]D p .
                                                                     & Bernoulli’s principle states that in an ideal fluid with
              . How is Reynolds number defined for (i) noncircular
                                                                       no work being performed on the fluid, an increase in
                conduits, (ii) packed beds, and (iii) mixing?          velocity occurs simultaneously with decrease in
                & ðiÞ N Re ¼ D e r=m;                  ð2:13Þ
                                                                       pressure or a change in the gravitational potential
                                                                       energy of the fluid.
                     where D e is the equivalent diameter of the non-
                                                                     & This principle is a simplification of Bernoulli’s equa-
                     circular flow conduit.
                                                                       tion, which states that the sum of all forms of energy
                               0
                  ðiiÞ N Re;p ¼ D p V =½ð1 «ÞmŠ  ðErgun’s definitionÞ;  in a fluid flowing along an enclosed path (a stream-
                               r
                                                       ð2:14Þ          line) is the same at any two points in that path.
                                                                     & In fluid flow with no viscosity, and, therefore, one in
                     where D p is the particle/packing diameter, V is  which a pressure difference is the only accelerating
                                                         0
                     the superficial velocity, « is the void fraction,  force, it is equivalent to Newton’s laws of motion. It
















                                                        Development of boundary layer.
                                             FIGURE 2.5
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