Page 239 - Bird R.B. Transport phenomena
P. 239

§7.8  Derivation  of the Macroscopic Mechanical Energy Balance  223

                   When  all  the  contributions  are  inserted  into  Eq.  7.8-2  we  finally  obtain  the  macro-
                scopic mechanical energy balance:

                           |  (X tot  +  O tot) =  (b

                                                    + (v 2)S 2)  +  W m E c -        (7.8-8)
                                                                   -
                                             & ) S 2  p 2                E v
                If,  now, we  introduce  the  symbols  w x  = p^{v^)S A  and  zv 2 = p 2(v 2)S 2 for  the mass  rates  of
                flow  in and  out, then  Eq. 7.8-8 can be rewritten  in the form  of Eq. 7.4-2. Several assump-
                tions have been made  in this development, but normally they are not serious.  If the situ-
                ation warrants, one can go back and include the neglected  effects.
                   It should  be noted  that  the above derivation  of the mechanical  energy balance  does
                not require that the system be isothermal. Therefore the results in Eqs. 7.4-2 and  7.8-8 are
                valid  for nonisothermal  systems.
                   To get the mechanical energy balance in the form  of Eq. 7.4-7 we have to develop  an
                approximate expression  for  E c. We imagine  that  there  is a representative  streamline  run-
                ning through  the system, and  we introduce  a coordinate  s along the streamline.  We as-
                sume that pressure, density, and  velocity do not vary over the cross section. We  further
                imagine that at each position along the streamline, there is a cross section S(s) perpendic-
                ular to the s-coordinate, so that we can write dV  = S(s)ds. If there are moving parts in the
                system and  if the system geometry is complex, it may not be possible to do this.
                   We start by using the fact that  (V • pv)  =  0 at steady state so that

                                                           V
                                    Ec = ~j  p(V • v) dV = + j - (v • Vp) dV         (7.8-9)
                                          V              V
                Then  we  use  the  assumption  that  the  pressure  and  density  are  constant  over  the  cross
                section to write  approximately


                                                       ,  )S(s)ds                   (7.8-10)
                                                       as/
                Even though p, v, and  S are functions  of the streamline coordinate s, their product, w = pvS,
                is a constant  for steady-state operation and hence may be taken outside the integral. This
                gives


                                               2
                                                                \
                                            i  p  ds      J i  ds P/
                Then an integration by parts can be  performed:
                                                                      2
                                          2   f2  -i dp d s  I  =  w A /w\  JrW  f i  (7 8 12)
                                                                      v
                                          i "  Ji  ^ J   " W )M                      *"
                When this result  is put  into Eq. 7.4-5, the approximate relation  in Eq. 7.4-7 is obtained. Be-
                cause of the questionable nature  of the assumptions made (the existence of a representative
                streamline and the constancy  of p and p over a cross section), it seems preferable  to use Eq.
                7.4-5 rather than Eq. 7.4-7. Also, Eq. 7.4-5 is easily generalized to systems with multiple inlet
                and outlet ports, whereas Eq. 7.4-7 is not; the generalization is given in Eq. (D) of Table 7.6-1.


                QUESTIONS FOR      DISCUSSION
             1.  Discuss the origin, meaning, and use  of the macroscopic balances, and explain what assump-
                tions have been made in deriving them.
             2.  How does one decide which macroscopic balances to use for a given problem? What auxiliary
                information  might one need in order to solve problems with the macroscopic balances?
             3.  Are friction  factors and friction  loss factors related?  If so, how?
   234   235   236   237   238   239   240   241   242   243   244