Page 185 - Bird R.B. Transport phenomena
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§5.6  Turbulent Flow in Jets  169







                           Circular hole


                                                                                  Fig.  5.6-1. Circular jet
                                                                                  emerging from a plane
                                                                                  wall.


      SOLUTION             In order to use Eq. 5.4-3 it is necessary to know how b and v z max  -  v 7 min  vary with z for the cir-
                           cular jet. We know that the total rate of flow  of z-momentum 7 will  be" the  same for all values
                           of  z. We presume that the convective momentum flux is  much greater than  the viscous mo-
                           mentum flux. This permits us to postulate that the jet width b depends on /, on the density p
                           and  the kinematic viscosity  v  of  the fluid, and on the downstream distance z  from  the wall.
                                                                                                  2
                           The  only combination of  these variables  that  has the dimensions of  length is  b  °c Jz/pv ,  so
                           that the jet width is proportional to z.
                               We next postulate that the velocity profiles are "similar/' that is,
                                                         = №     where £ = —^-                  (5.6-1)
                                                                          Hz)
                           which  seems  like a plausible  proposal; here v ZfTnax  is the velocity  along  the centerline.  When
                           this is substituted  into the expression  for the rate  of momentum flow in the jet (neglecting the
                                                        >=гг     pv\rdrde                       (5.6-2)
                           contribution  from  r vv)


                                                           Jo  Jo
                           we find  that

                                                                              2 2
                                                     2
                                                             2
                                               =
                                              ] =  27T b vl max  J  f £d£  = constant  X  pb v z>n  (5.6-3)
                                                    P
                           Since /  does not depend  on z and  since b is proportional  to z, then v~ z.max has to be inversely
                           proportional to z.
                                       in Eq. 5.4-3 occurs at the outer edge of the jet and is zero. Therefore because b  <*
                               The v zMn
                                                                  (0
                                      oc  z~\  we find  from  Eq. 5.4-3 that /x  is a constant. Thus we can use the equations
                           z and v z>max
                                                                                         (0
                            of motion for laminar flow and replace the viscosity /x by the eddy viscosity /x , or v by v {t)
                               In  the jet the main  motion  is in the z direction; that  is \v r\ «  \v z\. Hence we  can use a
                           boundary layer approximation  (see §4.4) for the time-smoothed equations of change and write
                            continuity:                                                         (5.6-4)
                            motion:                 V            v       r                      (5.6-5)
                                                     >  dr    z ~   r Tr[
                            These equations are to be solved with the following boundary conditions:

                            B.C.I:                       atr  =  0,  v r = 0                    (5.6-6)
                            B.C. 2:                      at r = 0,  dvjdr  = 0                  (5.6-7)
                            B.C. 3:                      at z =  °o,  у  =  Q                   (5.6-8)
                            The  last boundary condition  is  automatically satisfied,  inasmuch as  we  have already found
                            that u 2/max  is inversely proportional to z. We now seek a solution to Eq. 5.6-5 of the form of Eq
                            5.6-1 with b = z.
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