Page 101 - Bird R.B. Transport phenomena
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86  Chapter 3  The Equations of Change for  Isothermal Systems


       EXAMPLE   3.5-1     The  Bernoulli equation  for  steady flow  of  inviscid  fluids  is one of  the most famous  equations
                           in  classical  fluid  dynamics.  Show how  it is obtained from the Euler equation  of motion.
                                                 6
      The Bernoulli Equation
      for  the  Steady  Flow of  SOLUTION
      Inviscid Fluids      Omit  the  time-derivative  term  in  Eq.  3.5-9,  and  then  use  the  vector  identity  [v  • Vv]  =
                           iy(v  •  v)  -  [v  X  [V  X v]]  (Eq. A.4-23) to rewrite the equation as
                                                     2
                                                 pV\v  -  p[v  X  [V  X v]]  = -Vp  -  pgVh     (3.5-10)
                            In  writing  the last term, we have expressed  g as  -  УФ  = —gVh, where h is the elevation in the
                            gravitational  field.
                               Next  we  divide  Eq.  3.5-10  by  p  and  then  form  the  dot  product  with  the  unit  vector
                            s  = v/|v|  in the flow direction. When  this  is  done the term involving  the curl  of  the  velocity
                            field  can be shown  to vanish  (a nice exercise  in vector analysis), and  (s •  V) can be replaced  by
                           d/ds, where s is the distance along a streamline. Thus we  get

                                                                     -x4-h                      (3.5-11)

                           When  this is integrated along a streamline from point 1 to point 2, we  get

                                                                                                (3.5-12)
                            which  is  called  the Bernoulli  equation. It relates  the  velocity,  pressure,  and  elevation  of  two
                            points along a streamline in a fluid in steady-state flow. It is used  in situations where it can be
                            assumed  that viscosity plays  a rather minor role.


      §3.6  USE OF THE EQUATIONS        OF  CHANGE
            TO  SOLVE   FLOW   PROBLEMS

                            For  most  applications  of  the equation  of  motion, we  have  to insert  the expression  for  т
                            from  Eq.  1.2-7  into Eq. 3.2-9  (or, equivalently,  the components of  т from  Eq.  1.2-6  or  Ap-
                            pendix  B.I  into  Eqs.  3.2-5,  3.2-6, and  3.2-7).  Then  to  describe  the  flow  of  a Newtonian
                            fluid  at  constant temperature, we  need in  general
                            The  equation  of continuity  Eq.  3.1-4
                            The  equation  of motion   Eq.  3.2-9
                            The  components of т       Eq.  1.2-6
                            The  equation of state     P  =  pip)
                            The  equations for the  viscosities  /JL  =  /X(p), К  =  К(р)
                            These  equations, along  with  the  necessary  boundary  and  initial  conditions, determine
                            completely  the pressure, density, and velocity  distributions  in the fluid. They are  seldom
                            used  in their complete form  to solve  fluid  dynamics  problems.  Usually  restricted  forms
                            are used  for  convenience, as in this chapter.
                               If it is appropriate to assume  constant density  and viscosity, then we  use
                            The  equation of continuity  Eq.  3.1-4 and Table  B.4
                            The  Navier-Stokes equation  Eq.  3.5-6 and Tables  B.5,6, 7
                            along with  initial and boundary conditions. From these one determines the pressure  and
                            velocity  distributions.


                               6
                                 Daniel Bernoulli  (1700-1782)  was  one of the early  researchers  in fluid  dynamics and also  the
                            kinetic theory  of gases. His hydrodynamical  ideas were  summarized  in D. Bernoulli, Hydrodynamica  sive
                            de viribus et motibus fluidorum  commentarii, Argentorati  (1738), however  he did  not actually give Eq. 3.5-12.
                            The  credit  for  the derivation  of  Eq. 3.5-12 goes to L. Euler, Histoires de YAcademie de Berlin (1755).
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