Page 410 - Bird R.B. Transport phenomena
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392  Chapter 12  Temperature Distributions with More Than One Independent  Variable

                                       Fluid approaching with temperature T^ and velocity v^
                                       ТТТТТТТТТГТТТТТТТТ
                                              Stagnation locus


                               Approximate limit of
                              thermal boundary layer







                                             Separated flow region

                              Fig. 12.4-2.  Heat transfer  from  a three-dimensional  surface.
                              The asymptotic analysis  applies upstream  of the separated and
                              turbulent flow regions. These regions are illustrated  for  cylin-
                              ders in Fig. 3.7-2.



         EXAMPLE   12.4-3     The technique introduced in the preceding example has been extended  to flow around  objects
                              of  arbitrary  shape. Consider  the steady  flow  of  a  fluid  over  a  stationary  object  as  shown  in
        Forced  Convection    Fig.  12.4-2. The fluid approaches at a uniform  temperature T ,  and the solid  surface  is main-
                                                                               x
        in  Steady  Three-    tained at a uniform temperature T . The temperature distribution and heat transfer  rate are to
                                                         o
        Dimensional  Flow     be found  for the region  of laminar flow, which extends downstream  from the stagnation locus
        at  High  Prandtl     to the place where  turbulence or flow separation begins.  The velocity  profiles  are considered
        Numbers 89            to be known.
                                 The thermal boundary  layer  is considered  to be very thin. This implies that the isotherms
                              nearly  coincide with  the solid  surface,  so that the heat flux q is nearly  normal to the  surface.
                              It also  implies  that the complete velocity  profiles  are not needed  here. We  need  to know  the
                              state  of the motion only near the solid  surface.
                                 To  capitalize  on  these  simplifications,  we  choose  the  coordinates  in  a  special  way  (see
                              Fig.  12.4-2).  We  define  у  as  the distance  from  the surface  into the fluid  just  as  in  Fig. 12.4-1.
                              We  further  define  x  and  z  as  the coordinates  of  the nearest  point  on  the surface,  measured
                              parallel  and perpendicular  to the tangential motion next to the surface.  We  express  elements
                              of  arc in the x and z directions as h dx and h dz, where h  and h  are position-dependent  "scale
                                                         x
                                                                               z
                                                                          x
                                                                z
                              factors"  discussed  in §A.7. Since we  are interested  here in the region  of  small  y, the scale  fac-
                              tors are treated as functions  only  of x and z.
                                 With  this choice of coordinates, the velocity  components for  small у become
                                                         v x  =  x, z)y                          (12.4-26)
                                                                                                 (12.4-27)
                                                                    i
                                                                2h x h z
                                                                                                 (12.4-28)
                              Here  /3(x, z) is  the local  value  of  dv /dy  on the surface;  it  is  positive  in the nonseparated re-
                                                          x
                              gion, but  may  vanish  at points  of  stagnation  or separation. These equations  are obtained  by
                              writing  Taylor  series  for v  and v , retaining terms through the first degree  in y, and then inte-
                                                  x
                                                        z
                                 8
                                   W.  E. Stewart, AlChE  Journal, 9, 528-535  (1963).
                                 9
                                  For related two-dimensional analyses,  see M. J. Lighthill, Proc. Roy.  Soc,  A202, 359-377  (1950);
                              V.  G. Levich, Physico-Chemical Hydrodynamics,  Chapter 2, Prentice-Hall, Englewood  Cliffs,  N.J. (1962);
                              A. Acrivos,  Physics of Fluids, 3, 657-658  (1960).
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