Page 76 - Modelling in Transport Phenomena A Conceptual Approach
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3.5.  TRANSPORT ANALOGIES                                            57


           Reynolds further assumed that Pr = Sc = 1. Under these circumstances Eq. (3.5-9)
           reduces to

                                                                           (3.510)

           which is known as the Reynolds analogy. Physical properties in Eq.  (3.510) must
           be evaluated at T = (T, + T,)/2.
              The Reynolds analogy is reasonably valid for gas systems but  should not  be
           considered for liquid systems.


           3.5.2  The Chilton-Colburn Analogy
           In the Chilton-Colburn analogy the relationships between the effective film thick-
           nesses are expressed as
                                   6             6
                                   - = pr'l3     - = sc1/3                 (3.51 1)
                                   6t            6,
           Substitution of  Eq.  (3.5-11) into Eq.  (3.57) yields


                                                                           (3.512)

           and
                                     I
                                                                           (3.513)
                                                    j,
                                     - = StM SC213
           where jH and jM are the  Colburn j-factors  for  heat and mass transfer, respec-
           tively.
              Physical properties in Eqs.  (3.512) and  (3.513) must  be evaluated  at T =
           (T, + T,)/2.   The Chilton-Colburn analogy is valid  when 0.6  5 Pr  5  60 and
           0.6 5 Sc 5 3000. Note that Eqs.  (3.512) and (3.5-13) reduce to Reynolds analogy,
           Eq.  (3.5-lo), for fluids with Pr = 1 and Sc = 1.
              As stated in Section 3.1,  the drag force is the component of  the force in the
           direction of  mean flow.  In general, both viscous and pressure forces contribute to
           this force5.  In Eq. (3.1-3),  only viscous force is considered in the evaluation of
           the drag force.  The reason for this is that the pressure always acts normal to the
           surface of  the flat plate and the component of  this force in the direction of  mean
           flow  is zero.  In the case of  curved surfaces, however,  the component of  normal
           force to the surface in the direction of  mean flow  is not necessarily zero as shown
           in Figure 3.8.  Therefore, the friction factor for flow  over flat plates and for flow
           inside circular ducts includes only friction drag, whereas the friction factor for flow
           around cylinders, spheres, and other bluff objects includes both friction and form
           drags. As a result, f/2 term for flow around cylinders and spheres is greater than

             5The drag force arising from viscous and pressure forces are called friction (or, skin) drag and
           form  drag, respectively.
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