Page 307 - Bird R.B. Transport phenomena
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§10.1  Shell Energy Balances; Boundary Conditions  291

                           somewhat  idealized,  the results  find  application  in numerous  standard  engineering  cal-
                           culations. The problems were chosen to introduce the beginner to a number  of important
                           physical concepts associated  with  the heat transfer  field.  In addition, they serve to show
                           how  to use a variety  of boundary  conditions  and  to illustrate problem  solving  in Carte-
                           sian, cylindrical, and spherical coordinates. In §§10.2-10.5 we consider  four kinds  of heat
                           sources: electrical, nuclear, viscous, and  chemical. In §§10.6 and  10.7 we cover two topics
                           with  widespread  applications—namely,  heat  flow  through  composite  walls  and  heat
                           loss from  fins. Finally, in  §§10.8 and  10.9, we analyze  two limiting  cases  of heat  transfer
                           in moving  fluids:  forced  convection and  free  convection. The study  of these topics paves
                           the way for the general equations in Chapter 11.


      §10.1  SHELL ENERGY BALANCES; BOUNDARY              CONDITIONS
                           The problems discussed  in this chapter are set up by means  of shell energy balances. We
                           select  a slab  (or shell), the surfaces  of which  are normal  to the direction  of heat  conduc-
                           tion, and  then we write  for this system  a statement  of the law  of conservation  of  energy.
                           For steady-state (i.e., time-independent)  systems, we write:
                                 (rate  of   1    rate of        I rate of        rate of
                                  energy in       energy out   +  j energy in     energy out
                                 1 by convective [  by  convective  1 by molecular |  by  molecular
                                 [transport  J    transport      [transport  J    transport
                                  rate of        rate of         rate of
                                  work done      work done       work  done    rate of   j
                                  on system      by system       on system    I energy   > = 0  (10.1-1)
                                  by molecular   by  molecular   by external   production!
                                  transport      .transport      forces
                           The convective transport of energy was discussed  in §9.7, and  the molecular transport (heat
                           conduction)  in  §9.1. The  molecular work terms were  explained  in  §9.8. These three  terms
                           can be added  to give the  "combined  energy  flux"  e, as shown  in  Eq. 9.8-6. In setting  up
                           problems  here  (and  in the next chapter)  we will use the  e vector  along  with  the expres-
                           sion for the enthalpy in Eq. 9.8-8. Note that in nonflow  systems  (for which v is zero) the e
                           vector simplifies  to the q vector, which is given by Fourier's law.
                               The energy production term  in  Eq.  10.1-1 includes  (i) the degradation  of electrical  en-
                           ergy  into  heat,  (ii)  the  heat  produced  by  slowing  down  of  neutrons  and  nuclear  frag-
                           ments liberated  in the fission  process, (iii) the heat produced  by viscous dissipation,  and
                           (iv) the  heat  produced  in  chemical  reactions. The chemical  reaction  heat  source  will  be
                           discussed  further  in Chapter  19. Equation  10.1-1 is a statement  of the first law  of thermo-
                           dynamics,  written  for  an  "open"  system  at  steady-state  conditions.  In  Chapter  11  this
                           same statement—extended  to unsteady-state  systems—will be written as an equation  of
                           change.
                               After  Eq.  10.1-1 has been written  for  a thin  slab or shell  of material, the thickness  of
                           the  slab or  shell  is allowed  to approach  zero. This procedure  leads  ultimately  to an  ex-
                           pression  for  the temperature  distribution  containing  constants  of  integration,  which  we
                           evaluate by use  of boundary  conditions. The commonest  types  of boundary  conditions
                           are:
                               a.  The temperature may be specified  at a surface.
                               b.  The heat  flux  normal  to  a  surface  may be  given  (this  is equivalent  to  specifying
                                 the normal component  of the temperature gradient).
                               c.  At interfaces  the continuity  of temperature and  of the heat flux normal to the in-
                                 terface are required.
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