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16  Chapter 1  Viscosity and the Mechanisms of Momentum Transport

     §1.2  GENERALIZATION       OF NEWTON'S      LAW   OF  VISCOSITY
                          In  the  previous  section  the  viscosity  was  defined  by  Eq.  1.1-2,  in  terms  of  a  simple
                          steady-state  shearing  flow  in  which  v x  is  a  function  of  у  alone, and  v y  and  v z  are  zero.
                          Usually  we  are interested  in more complicated flows  in which  the three velocity  compo-
                          nents  may  depend  on  all  three  coordinates  and  possibly  on  time.  Therefore  we  must
                          have  an  expression  more  general  than  Eq.  1.1-2, but  it  must  simplify  to  Eq.  1.1-2  for
                          steady-state  shearing  flow.
                              This generalization  is not simple; in fact, it took mathematicians about a century and a
                          half  to do this. It is  not appropriate  for  us  to give all  the details  of  this development  here,
                                                                       1
                          since they can be found  in many fluid  dynamics books.  Instead we explain briefly  the main
                          ideas that led to the discovery  of the required generalization  of Newton's law  of viscosity.
                              To do this we  consider  a very  general  flow  pattern, in which  the fluid  velocity  may
                          be  in  various  directions  at  various  places  and  may  depend  on  the  time  t. The  velocity
                          components are then given  by

                                        v x  = v (x, y, z, t);  v y  = v (x,  y, z, t);  v z  = v (x, y, z, t)  (1.2-1)
                                                                               z
                                                              y
                                             x
                          In  such  a  situation, there will  be  nine stress  components  r /y  (where  / and / may  take  on
                          the designations  x, y, and  z), instead  of  the component r yx  that appears  in  Eq.  1.1-2.  We
                          therefore must begin  by  defining  these stress components.
                              In  Fig.  1.2-1  is  shown  a  small  cube-shaped  volume  element  within  the  flow  field,
                          each  face  having  unit area. The center  of  the volume  element is  at the position  x, y, z.  At





                                                                          -x,y,z













                                                                                               \

                                                                                               \

                                                                                          f  1
                                                                                           pS
                                                                                             z
                                      (a)                       (b)                        (c)
                           Fig. 1.2-1  Pressure and viscous  forces  acting on planes in the fluid  perpendicular to the three
                           coordinate systems.  The shaded planes have unit area.



                              1  W. Prager, Introduction  to Mechanics  ofContinua,  Ginn, Boston (1961), pp. 89-91; R. Aris,  Vectors,
                           Tensors, and the Basic Equations  of Fluid Mechanics, Prentice-Hall, Englewood  Cliffs,  N.J. (1962), pp. 30-34,
                           99-112;  L. Landau and  E. M. Lifshitz, Fluid Mechanics, Pergamon, London, 2nd edition (1987), pp. 44-45.
                           Lev  Davydovich Landau (1908-1968)  received  the Nobel prize in 1962  for  his work  on liquid helium and
                           superfluid  dynamics.
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