Page 374 - Bird R.B. Transport phenomena
P. 374

356   Chapter 11  The Equations  of Change for  Nonisothermal  Systems

                           Table  11.5-3  Physical  Interpretation of  Dimensionless Groups
                                              _  pvp/lp _  inertial  force
                                                /XV Q /IQ  viscous  force

                                              _  pvp/lo _  inertial  force
                                                 PS    gravity  force
                                        Gr  _  PgP(T\ ~ o> _  buoyant  force
                                                     T
                                        Re 2    pvl/l 0   inertial  force
                                        pC v (T  -  T )/l  heat transport by  convection
                              Pe = RePr =  p 0  ]  0  0
                                          k(T }  -  T )/IQ  heat transport  by  conduction
                                                0
                                    fjb(v /l ) 2  heat production by viscous  dissipation
                               B r  = •  o  o
                                   «T,  -  T )// 2  heat transport by conduction
                                         0


                               A low  value  for  the Reynolds  number means that viscous forces  are large in compar-
                           ison  with  inertial  forces.  A  low  value  of  the  Brinkman  number  indicates  that  the  heat
                           produced  by  viscous  dissipation  can  be  transported  away  quickly  by  heat  conduction.
                           When  Gr/Re  2  is large, the buoyant  force  is important in determining  the flow pattern.
                               Since  dimensional  analysis  is  an  art  requiring  judgment  and  experience,  we  give
                           three illustrative  examples.  In the first  two we  analyze  forced  and  free  convection  in  sim-
                           ple  geometries.  In the third  we  discuss  scale-up  problems  in  a  relatively  complex  piece
                           of  equipment.


       EXAMPLE   11.5-1    It is  desired  to predict  the temperature distribution  in a gas  flowing  about  a long,  internally
                           cooled  cylinder  (system  I)  from  experimental  measurements  on  a  one-quarter  scale  model
     Temperature           (system  II). If possible the same  fluid  should  be used  in the model as  in the full-scale  system.
     Distribution  about  a  The system,  shown  in  Fig.  11.5-1, is  the same  as  that  in  Example  3.7-1  except  that  it  is  now
     Long  Cylinder        nonisothermal. The fluid  approaching  the cylinder  has a speed  v x  and a temperature T ,  and
                                                                                                x
                           the cylinder  surface  is maintained at T , for  example, by  the boiling  of a refrigerant  contained
                                                          o
                           within  it.
                               Show  by  means  of  dimensional  analysis  how  suitable  experimental  conditions  can  be
                           chosen  for  the model studies.  Perform  the dimensional analysis for  the "intermediate case"  in
                           Table  11.5-1.

     SOLUTION              The  two  systems,  I  and  II, are  geometrically  similar.  To  ensure  dynamical  similarity,  as
                           pointed  out  in  §3.7, the dimensionless  differential  equations  and  boundary  conditions  must
                           be the same, and the dimensionless  groups  appearing  in them must have  the same numerical
                           values.
                               Here we  choose the characteristic  length  to be the diameter D of  the cylinder,  the charac-
                           teristic velocity  to be the approach velocity  v x  of the fluid, the characteristic pressure  to be the
                           pressure  at x  = -  °°  and у  = 0, and the characteristic temperatures to be the temperature T x  of
                           the approaching  fluid  and the temperature T o  of  the cylinder  wall. These characteristic  quan-
                           tities will carry  a label  I or II corresponding  to the system  being  described.
                               Both  systems  are  described  by  the  dimensionless  differential  equations  given  in  Eqs.
                           11.5-7  to 9, and by boundary  conditions
                                                        2
                           B.C.I                asiP  + j/ -»»,  v-»6. ,  f-»l                (11.5-10)
                                                                    Y
                           B.C. 2               at x 2  + f  = i  v  = 0,  f  = 0             (11.5-11)
                           B.C.3                at*-»  -oo and у =  О,   Ф -» 0               (11.5-12)
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