Page 172 - Bird R.B. Transport phenomena
P. 172

156   Chapter 5  Velocity  Distributions in Turbulent Flow

                           Table 5.1-1  Dependence of Jet Parameters on Distance z from Wall
                                                Laminar  flow                  Turbulent  flow

                                        Width   Centerline    Mass     Width   Centerline   Mass
                                        of jet   velocity   flow rate   of jet  velocity   flow rate

                           Circular jet   z        z"  1       z         z        z" 1        z
                           Plane jet     z 2/3     z -l/3      z l/3     z       z" 1/2      2  1 / 2



                               For turbulent flow, on the other hand, the dependence on the geometrical and  phys-
                           ical properties is quite  different: 1
                                                   L W vl    (turbulent) (5 X 10 5  <  Re  <  10 )  (5.1-8)
                                                                                       7
                                                       5
                                                    4
                                                                                  L
                           Thus  the force  is proportional to the |-power  of  the approach velocity  for  laminar  flow,
                           but to the |-power  for turbulent flow. The stronger dependence on the approach velocity
                           reflects  the extra energy  needed to maintain the irregular eddy motions in the  fluid.
     Circular and  Plane Jets
                           Next we  examine the behavior  of  jets  that emerge  from  a  flat  wall,  which  is  taken to be
                           the  xy-plane  (see  Fig. 5.6-1).  The fluid  comes out  from  a  circular  tube  or  a  long  narrow
                           slot, and  flows  into a large  body  of  the same  fluid.  Various  observations  on the jets  can
                           be  made: the width  of  the jet, the centerline velocity  of  the jet, and  the mass  flow  rate
                           through  a cross  section parallel  to the xy-plane.  All  these properties can be measured  as
                           functions  of  the distance z from  the wall.  In Table  5.1-1  we  summarize the properties  of
                           the circular and  two-dimensional jets  for  laminar and turbulent flow. 1  It is curious that,
                           for  the circular jet, the jet width, centerline velocity, and mass  flow  rate have  exactly  the
                           same dependence on z in both laminar and turbulent flow.  We  shall  return to this point
                           later in §5.6.
                               The above  examples  should  make it clear that the gross  features  of laminar and tur-
                           bulent  flow  are generally  quite different.  One of  the many challenges  in turbulence the-
                           ory is to try to explain these  differences.


     §5.2   TIME-SMOOTHED       EQUATIONS      OF  CHANGE
            FOR  INCOMPRESSIBLE       FLUIDS
                           We  begin  by  considering  a  turbulent  flow  in  a  tube  with  a  constant imposed  pressure
                           gradient.  If at one point in the fluid  we  observe  one component of the velocity  as  a  func-
                           tion  of  time, we  find  that it  is  fluctuating  in  a  chaotic fashion  as  shown  in  Fig.  5.2-1 (я).
                           The fluctuations  are irregular  deviations  from  a mean value.  The actual velocity  can be
                           regarded  as  the sum  of  the mean value  (designated  by  an  overbar)  and  the  fluctuation
                           (designated by  a prime). For example, for  the z-component of the velocity  we  write
                                                           v z  = v z  + v z                    (5.2-1)

                           which  is  sometimes  called  the Reynolds decomposition.  The mean value  is  obtained  from
                           v (t) by  making a time average  over  a large number of  fluctuations
                            z
                                                                 2
                                                                  ° v (s) ds                    (5.2-2)
                                                                   z
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