Page 318 - Bird R.B. Transport phenomena
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302  Chapter  10  Shell  Energy  Balances  and Temperature Distributions  in Solids  and Laminar Flow


                           significantly  in the axial direction. Then in the second  term we  replace  v z  by  the  superfi-
                           cial  velocity  v ,  because  the latter  is  the  effective  fluid  velocity  in  the  reactor.  Then  Eq.
                                      0
                           10.5-4 becomes
                                                     pC v  Щ- = K  ^   + S                     (10.5-5)
                                                       p 0      eff zz    c
                                                          dz     '  dz 1
                           This  is  the  differential  equation  for  the  temperature  in  zone  II. The  same  equation  ap-
                           plies  in zones  I and  III with  the source  term  set  equal  to zero. The differential  equations
                           for  the temperature are then

                           Zone I                 (z <  0)  pC v  —  = K eiizz  — -            (10.5-6)
                                                                0
                                                               p
                                                                  dz     '  dz 1
                           Zone II             ( 0 < z < L )  pC^ ^r-  = «eff ^r  + S F(0)     (10.5-7)
                                                                  dz     '  dz
                                                              и  o        22  1   cl
                           Zone III               (z >  L)  C v  Ц-  = ic  ^—                  (10.5-8)
                                                           P  p 0       eff zz
                                                                 dz      '  dz 2
                           Here we  have  assumed  that we  can use  the same value  of  the effective  thermal conduc-
                           tivity in all three zones. These three second-order  differential  equations are subject  to the
                           following  six  boundary  conditions:

                           B.C.I:            atz  =  — с  T 1  = T,                            (10.5-9)
                           B.C. 2:           at z  = 0,  T 1  = T n                           (10.5-10)
                                                             dT l      dT n
                           B.C. 3:           at z  = 0,
                                                         ^ггЧ~=^2гЦ~                          (10.5-11)
                           B.C. 4:           at z  = L,     '  dz    '  dz
                                                         T u  = T m                           (10.5-12)
                           B.C. 5:           at z  = L,
                                                            '  dz     '  dz
                           B.C. 6:           atz  = oo,  T m  = finite                        (10.5-14)
                           Equations  10.5-10 to 13 express the continuity  of temperature and heat flux at the bound-
                           aries  between  the zones. Equations  10.5-9 and  14 specify  requirements  at the two  ends  of
                           the  system.
                              The solution  of  Eqs.  10.5-6 to  14 is considered  here  for  arbitrary  F(@). In many  cases
                           of  practical  interest,  the  convective  heat  transport  is  far  more  important  than  the axial
                           conductive  heat transport. Therefore,  here we  drop  the conductive  terms  entirely  (those
                           containing  /c cff/Z2 ).  This  treatment  of  the problem  still  contains  the salient  features  of  the
                           solution  in the limit  of large Pe = RePr (see Problem  10B.18 for  a fuller  treatment).
                              If  we  introduce  a  dimensiqnless  axial  coordinate  Z  =  z/L  and  a  dimensionless
                           chemical heat source N  = S L/pC v (T }  — T ), then Eqs.  10.5-6 to 8 become
                                                       p 0
                                                  c]
                                                                o
                           Zone I                           (z<0)    ^   = 0                  (10.5-15)
                                                                     dZ
                           Zone  II                     (0<z<L)      ^ -  = NF(®)             (10.5-16)
                                                                     dZ
                           Zone III                        (z>L)    ^ -  = 0                  (10.5-17)

                                                                     dZ
                           for  which  we  need three boundary  conditions:
                           B.C. 1:                     at Z = -oo,  0  1  = l                 (10.5-18)
                           B.C. 2:                     atZ  = 0,    &  = в и                  (10.5-19)
                           B.C. 3:                     at Z =  1,  в 11  = в 111              (10.5-20)
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