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100     2 Nonlinear algebraic systems



                   Table 2.2 Drag coefficient for flow around a
                   smooth sphere at Reynolds’ numbers between
                   350 000 and 1 000 000. From Table 5–22 of Perry
                   & Green (1984)

                     Re                                C D
                   350 000                            0.396
                   400 000                            0.0891
                   500 000                            0.0799
                   700 000                            0.0945
                   1 000 000                          0.110




                   Between Reynolds’ numbers of 350 000 and 1 000 000, there is a transient drop in the
                   drag constant as the boundary layer first becomes turbulent, delaying separation on the
                   downstream side. In this regime, we may use interpolation (MATLAB function interp1)of
                   the data in Table 2.2.
                                                                                         3
                     Estimate the terminal velocity of a smooth spherical iron particle (density 7850 kg/m )
                                         3
                   in water (density 1000 kg/m , viscosity 0.001 Pa s) as a function of the particle diameter
                   (in meters) over the range 0.1 mm to 10 cm.
                   2.B.1 Consider a CSTR, with the single gas-phase elementary reaction

                                                  A + B → C                          (2.164)
                   that has a rate constant k of 0.05 l/(mol/s). The feed stream to the reactor, at a volumetric
                   flow rate υ 0 in liters per second, is at a total pressure P 0 = 5 atm. It comprises reactants
                   A and B, and a nonreacting diluent gas. The partial pressures of the reactants are P A0 =
                   0.5 atm and P B0 = 0.5 atm. Assume that the ideal gas law holds, and that the reactor is
                   operated isothermally at 350 K. Assume that the inlet stream is at the same temperature and
                   pressure as the reactor contents. For a reactor volume of 1000 l, plot the conversion of A as
                   a function of υ 0 . Make sure to account for the fact that the total number of moles in the gas
                   phase decreases with increasing conversion, so that the outlet volumetric flow rate will be
                   somewhat smaller than υ 0 . For further discussion, consult Fogler (1999).
                   2.B.2. Consider a 1000-l CSTR in which the following reactions are taking place:

                                           A + B → C r R1 = k 1 c A c B
                                                                                     (2.165)
                                           C + B → D r R2 = k 2 c B c C
                                             A → E r R3 = k 3 c A
                   We have the following kinetic data
                                                  l                     −2   l
                                              −2
                             k 1 (298 K) = 2.1 × 10    k 1 (315 K) = 3.6 × 10
                                                mol s                      mol s
                                                  l                     −2   l
                                              −2
                             k 2 (298 K) = 1.5 × 10    k 2 (315 K) = 4.5 × 10        (2.166)
                                                mol s                      mol s
                                 k 3 (298 K) = 0.00012 s −1  k 3 (315 K) = 0.00026 s −1
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