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182  HEAT TRANSFER  AND  HEAT  EXCHANGERS



                                                                     transfer units is
                     EXAMPLE 8.5
                     Application of the Effectiveness and the B Method     N = UA/Cmin = 2000/800 = 2.5,
                  Operating  data  of  an  exchanger are  shown on  the  sketch.  These   C = Cmin/Cmax = 0.8,
                  data include
                                                                           D =       = 1.2806,
                      UA = 2000,                                           P=                2               = 0.6271,
                     m'c' = 1000,  mc = 800,                                  1 + C + D[1+ exp(-ND)]/l-  exp(-ND)
                       C = Cmin/Cmax = 0.8.                                 0 = PIN = 0.2508,
                                                                         AT,  = 0(200 - 80) = 30.1,
                                                                           Q = UA(AT),  = 2000(30.1) = 60,200,
                                                                             = 800(200 - &) = 1000(T; - SO),
                                   m'c' = 1000
                                                                          :.  T2 = 124.75,
                                                                          Ti  = 140.2.
                                                                     T, also may be found from the definition of P:
                                   UA = 2000
                                                 T;                     P=    actual AT   2oo - T2 = 0.6271,
                                                                           max possible AT - 200 - 80
                                                                        :.  T,=  124.78.
                  The equation for effectiveness P is given by item 6 of  Table 8.3 or it
                  can be  read off  Figure 8.4(a).  Both  P and  0 also can be read off   With  this  method,  unknown terminal temperatures  are found
                  Figure  8.4(a)  at  known  N  and  R = C,/C, = 0.8.  The  number  of   without trial calculations.




                  compared with a normal value of                        The Nusselt number,  hL/k = h/(k/L),  is the ratio of  effective
                                                                     heat transfer to that which would take place by conduction through
                     U = 10,000/(57 + 50) = 93,                      a film of thickness L.
                                                                         The Peclet number, DGC/k = GC/(k/D) and its modification,
                  where the averages of  the listed numbers in Table 8.6 are taken in   the Graetz number wC/kL,  are ratios of sensible heat change of the
                  each case.                                         flowing  fluid  to  the  rate  of  heat  conduction  through  a  film  of
                                                                     thickness D or L.
                  METAL WALL RESISTANCE                                  The Prandtl number, Cp/k = (y/p)/(k/pC),  compares the rate
                                                                     of  momentum transfer through friction to the thermal diffusivity or
                  With the usual materials of  construction of  heat transfer surfaces,   the transport of  heat by conduction.
                  the magnitudes of  their thermal resistances may he comparable with   The Grashof number is interpreted  as the ratio of  the product
                  the  other  prevailing  resistances.  For  example,  heat  exchanger   of  the  buoyancy  and  inertial  forces to  the  square  of  the  viscous
                  tubing of  1/16 in. wall thickness has these values of  l/h,  = L/k for   forces.
                  several common materials:                              The Stanton number is a ratio of  the temperature  change of  a
                                                                     fluid  to  the  temperature  drop  between  fluid  and  wall.  Also,
                             Carbon steel   l/h,  = 1.76 x            St = (Nu)/(Re)(Pr).
                             Stainless steel   5.54 x                    An  analogy exists between  the  transfers of  heat  and mass  in
                             Aluminum          0.40 x 1 o-~          moving fluids, such that  correlations of  heat transfer involving the
                             Glass             79.0 x                 Prandtl  number  are  valid  for  mass  transfer  when  the  Prandtl
                  which are in the range of  the given film and fouling resistances, and   number Cp/k is replaced by the Schmidt number p/pk,.  This is of
                  should not  be  neglected in  evaluating the  overall coefficient. For   particular value in correlating heat  transfer from small particles to
                  example, with the  data of  this list  a coefficient of  93 with  carbon   fluids  where  particle  temperatures  are  hard  to  measure  but
                  steel  tubing  is  reduced  to  88.9  when  stainless  steel  tubing  is   measurement  of  mass  transfer  may  be  feasible,  for  example,  in
                  substituted.                                        vaporization of  naphthalene.

                  DIMENSIONLESS GROUPS
                                                                      8.4. DATA  OF  HEAT TRANSFER COEFFICIENTS
                  The effects of  the  many variables that  bear  on  the  magnitudes of
                  individual heat  transfer  coefficients are  represented  most logically   Specific  correlations  of  individual film  coefficients necessarily are
                  and  compactly in  terms  of  dimensionless groups.  The  ones  most   restricted in scope. Among the distinctions that are made are those
                  pertinent to heat transfer are listed in Table 8.8. Some groups have   of  geometry, whether inside or outside of tubes for instance, or the
                  ready physical interpretations  that  may assist in selecting the ones   shapes  of  the  heat  transfer  surfaces;  free  or  forced  convection;
                  appropriate  to particular  heat  transfer  processes. Such interpreta-   laminar  or  turbulent  flow;  liquids,  gases,  liquid  metals,  non-
                  tions  are  discussed  for  example  by  Grober  et  al.  (1961,  pp.   Newtonian  fluids;  pure  substances  or  mixtures;  completely  or
                  193-198).  A few are given here.                    partially  condensable;  air,  water,  refrigerants,  or  other  specific
                     The Reynolds number, Dup/p = pu2/(pu/D), is a measure of   substances; fluidized or  fixed  particles;  combined convection and
                  the ratio of  inertial to viscous forces.           radiation;  and  others.  In  spite of  such qualifications, it should be
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