Page 100 - Bird R.B. Transport phenomena
P. 100

§3.5  The Equations  of Change in Terms  of the Substantial  Derivative  85


                                                 Fig. 3.5-1.  The equation  of state for a slightly  com-
                             ^  Slightly compressible  pressible  fluid  and an incompressible  fluid  when T
                             I      fluid  with
                             |   p-p o  =  K(p-p o )  is constant.
                                where К = constant


                             ^  Incompressible  fluid
                                   with p =  p 0


                            Po


                 potential energy  per unit mass. Equation 3.5-6  is  a standard  starting  point  for  describing
                 isothermal flows  of gases and  liquids.
                     It must  be  kept  in mind  that, when  constant p is  assumed,  the equation  of  state  (at
                 constant  T) is  a  vertical  line  on a plot  of  p  vs.  p  (see  Fig.  3.5-1).  Thus, the absolute  pres-
                 sure  is  no longer  determinable  from  p and  T, although  pressure  gradients  and instanta-
                 neous  differences  remain  determinate by  Eq.  3.5-6  or  Eq.  3.5-7. Absolute  pressures  are
                 also obtainable  if p is known  at some point in the  system.
                     (ii)  When  the acceleration terms in the Navier-Stokes  equation are neglected—that is,
                 when p(Dv/Dt)  = 0—we get

                                                         2
                                             0  =  -Vp  + fiV v  + pg                 (3.5-8)
                 which  is called  the Stokes flow equation. It is sometimes called  the creeping flow equation, be-
                 cause  the term  p[v  •  Vv],  which  is  quadratic  in  the velocity,  can be  discarded  when  the
                 flow  is extremely  slow. For some flows, such as the Hagen-Poiseuille  tube flow, the term
                 p[v •  Vv]  drops out, and a restriction to slow flow  is not implied. The Stokes flow equation
                 is  important  in  lubrication  theory,  the  study  of  particle  motions  in  suspension,  flow
                 through  porous  media,  and  swimming  of  microbes.  There  is  a  vast  literature  on  this
                 subject. 3
                     (iii)  When  viscous forces are  neglected—that  is,  [V  •  т]  =  0—the  equation  of  motion
                 becomes
                                               P§y=-Vp    + pg                        (3.5-9)

                 which  is known  as  the Euler equation for  "inviscid"  fluids. 4  Of  course, there are no  truly
                 "inviscid"  fluids,  but  there  are  many  flows  in  which  the  viscous  forces  are  relatively
                 unimportant.  Examples  are  the  flow  around  airplane  wings  (except  near  the  solid
                 boundary), flow  of rivers  around the upstream surfaces  of bridge  abutments, some prob-
                 lems  in compressible  gas  dynamics, and flow  of  ocean currents. 5



                     J. Happel  and  H. Brenner,  Low Reynolds Number Hydrodynamics, Martinus  Nijhoff,  The Hague
                     3
                 (1983); S. Kim  and  S. J. Karrila, Microhydrodynamics: Principles and Selected Applications, Butterworth-
                 Heinemann,  Boston (1991).
                      L. Euler, Mem. Acad.  Sci. Berlin, 11, 217-273, 274-315, 316-361 (1755). The Swiss-born
                     4
                 mathematician  Leonhard Euler (1707-1783) (pronounced  "Oiler") taught in St. Petersburg, Basel, and
                 Berlin and published extensively in many  fields  of  mathematics  and  physics.
                     5
                      See,  for  example, D. J. Acheson, Elementary Fluid Mechanics, Clarendon  Press, Oxford  (1990),
                 Chapters  3-5; and  G. K. Batchelor, An  Introduction to Fluid Dynamics, Cambridge University Press (1967),
                 Chapter  6.
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