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154  Chapter 5  Velocity  Distributions in Turbulent Flow

     §5.1  COMPARISONS       OF LAMINAR AND       TURBULENT      FLOWS
                           Before  discussing  any  theoretical  ideas  about  turbulence,  it  is  important to  summarize
                           the  differences  between  laminar and  turbulent  flows  in several  simple  systems.  Specifi-
                           cally  we  consider the flow in conduits  of  circular and triangular  cross  section, flow along
                           a  flat plate, and flows  in jets. The first  three of  these were  considered  for  laminar flow in
                           §2.3, Problem 3B.2, and §4.4.

     Circular Tubes

                           For the steady,  fully  developed,  laminar flow in a circular tube  of radius  R we  know that
                           the velocity  distribution and the average  velocity  are given  by

                                                                iv )
                                              •  = 1 -  К-  and   z         (Re <  2100)      (5.1-1, 2)
                                           -,       К  /         r ma x
                           and  that the pressure drop and mass  flow rate w are linearly  related:

                                                                      (Re < 2100)               (5.1-3)

                           For turbulent flow, on the other hand, the velocity  is  fluctuating  with  time chaotically  at
                           each  point  in the tube. We  can measure  a  "time-smoothed velocity"  at  each point  with,
                           say,  a  Pitot tube. This  type  of  instrument  is  not sensitive  to rapid  velocity  fluctuations,
                           but  senses  the  velocity  averaged  over  several  seconds.  The  time-smoothed  velocity
                           (which  is  defined  in the next  section) will have  a z-component represented by  v , z  and  its
                           shape and average  value  will be given  very roughly  by  1

                                                     1/7       (v )  A
                                                                                       5
                                                                              4
                                                         and     z         (10  <  Re <  10 )  (5.1-4,5)
                                                                      5
                           This \-power  expression  for  the velocity  distribution is too crude to give a realistic  veloc-
                           ity  derivative  at  the wall.  The laminar  and  turbulent  velocity  profiles  are  compared  in
                           Fig. 5.1-1.



                                   Tube center












                                                                  Fig.  5.1-1.  Qualitative comparison  of lami-
                                                                  nar and turbulent velocity  profiles.  For a
                                                             0    more detailed description  of the turbulent
                                  1.0  0.8  0.6  0.4  0.2  0.2  0.4  0.6  0.8  1.0  velocity  distribution near the wall, see
                                                   r/R—+-         Fig. 5.5-3.


                              1
                                H. Schlichting, Boundary-Layer Theory, McGraw-Hill, New York, 7th edition (1979), Chapter  XX
                           (tube  flow), Chapters VII and  XXI  (flat plate  flow), Chapters IX and  XXIIV  (jet  flows).
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