Page 280 - Modelling in Transport Phenomena A Conceptual Approach
P. 280

260   CHAPTER 8.  STEADY MICROSCOPIC BALANCES WITHOUT GEN.

                       Left Side  Right Side
             Part (a)    5.9        9.7
             Part (b)    0.2        0.3


            Note that the physical  significance  of  the Biot number was given by Eq.  (7.1.141,
            2.e.,
                                    (Difference in driving force),,lid
                               Bi =
                                    (Difference in driving
            Therefore,  when Bi is large,  the temperature  drop between the surface of the wall
            and the bulk temperature is small and the physical properties can be  calculated at the
            bulk fluid temperature rather than the film temperature in engineering calculations.
            On the other hand, when Bi is small, the temperature drop  between the surface of
            the wall and  the bulk fluid temperature is large and the physical properties must be
            evaluated at the film temperature.  Evaluation of  the physical properties at the bulk
            fluid temperature for small values  of  Bi  may lead to erroneous results especially if
            the physical properties of  the fluid  are strongly  dependent  on temperature.


            8.2.2  Conduction in Cylindrical Coordinates
            Consider a onedimensional transfer of energy in the r-direction  in a hollow cylin-
            drical pipe with inner and outer radii of R1  and Rz, respectively, as shown in Figure
            8.14.  Since T = T(r), Table C.5 in Appendix C indicates that the only non-zero
            energy flux component is e, and it is given by
                                                    dT
                                        e,.  = q,.  = - k -                 (8.2-20)
                                                    dr
            For a cylindrical differential volume element of  thickness AT, as shown in Figure
            8.14, Eq. (8.2-1) is expressed in the form

                                                                            (8.2-21)

            Dividing Eq.  (8.2-21) by AT and taking the limit as AT -+  0 gives

                                   lim   (Aqr)lT - (Aqr)lr+ar   =O          (8.2-22)
                                  Ar+a         Ar
            or,
                                                                            (8.2-23)

            Since flux times area gives the heat transfer rate, Q, it is possible to conclude that

                                       A qr = constant = Q                  (8.2-24)
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