Page 518 - Elements of Chemical Reaction Engineering Ebook
P. 518

488                       Steady-State Nonisothermal Reactor Design   Chap. 8

                                  The POLYMATH program is given in Table E8- 10.1.


                                        TABLE E8-10.1.  SO3 OXIDATION POLYMATH PROGRAM
                                                   Equations:                     Initial Values:
                            d(P) /d(w)=(-1.12*10**(-8) *(1-.055*x) *T)* (55OO*visc+2288) /P   2
                            d(x) /d(w)=-(ra) /fa0                                     0
                            d(T)/d(w)=(5.11*(Ta-T)+(-ra)*(-deltdh) !/(fao*(sum+x*dcp))   1400
                            fao= .E38
                            visc=. 090
                            Ta=1264.67
                            de1tah=-42471-i.563*(T-1~60}+.00136*(T**2-1260**2)-2.459*1~*
                                    *
                               * (-7) (T**3-1260**3)
                            sum=57.23+.014*T-1.94*10**(-6)*TR+2
                            dcp=-l.5625+2.72*10**(-3)*T-7.38*10**(-7)*T**2
                            k=3600*exp(-176008/T-(110.l*ln(T) )+912.8)
                            thetaso=O
                            €0=2
                            Pao=. 22
                            thetao=.91
                            eps=-. 055
                            R=l. 987
                            Kp=exp(42311/R/T-11.241
                            ra=if(x<=.05)then(-k*(.848-.012/(Kp**2)))else(-k*( (1-x) /(the
                               taso+x))**.5*(P/Po*Pao*((thetao-.5*~)/
                                                                     1)
                               (lteps*x))-( (thetaso+x)/(l-x))**2/(Kp**2)
                            wO  =  "'   =  28.54


                              11.  Discussion of results. Figure E8-10.1 shows the profiles for inlet tempera-
                                  tures of  1200"R and 1400"R, respectively. Only 68.5% conversion is achieved
                                  for  To =  1200"R, even though  X,  = 0.99. For  an  entering temperature of
                                  1400"R, the major portion of  the reaction takes place in the first 6 ft of the
                                  reactor. At  this point, the conversion is 0.81, with only another 0.06 of  the
                                  conversion occurring  in  the remaining  14 ft, as shown in  Figure E8-10.Ib.
                                 The cause of  this low amount of  conversion in'the final 14 ft is the steadily
                                  dropping temperature in the reactor. Beyond the 6-ft point, the temperature is
                                 too  low  Lor  much  reaction to  take  place,  which  means  that  the  reactor is
                                 cooled too much.
                                     This detrimental situation indicates that the coolant temperature is too
                                  low for obtaining maximum conversion. Thus even boiling Dowtherm A at its
                                 highest possible operating temperature is not a suitable coolant. Perhaps a gas
                                 would give a better performance as a coolant in  this  reaction  system. Two
                                 problems at the end of the chapter pursue this aspect. One of them s;eks  the
                                 optimum coolant temperature for a constant-coolant-temperature system, and
                                 the other uses inlet gas as a coolant.
   513   514   515   516   517   518   519   520   521   522   523