Page 227 - Design and Operation of Heat Exchangers and their Networks
P. 227

216   Design and operation of heat exchangers and their networks




                   0
             With n ¼0.2 for Re sd >100, we also have
                              2 n 0      2 n 0
                        ð
                    ζ ¼ l bc =l bo Þ  + l bc =l bi Þ
                                   ð
                     s
                                    2 0:2             2 0:2
                                          ð
                        ð
                      ¼ 0:279=0:3365Þ   +0:279=0:3365Þ    ¼ 1:427
                The pressure drops in the crossflow section, in the window area and in
             the shell-side inlet and outlet sections can then be determined with
             Eq. (5.72), respectively, as follows:
                                    ð
              Δp c ¼ N b  1ð  ÞΔp b,id ζ ζ ¼ 14 1Þ 1092 0:6814 0:589 ¼ 5700 Pa
                                b l
                      Δp w ¼ N b Δp w,id ζ ¼ 14 6990 0:589 ¼ 57,641 Pa
                                    l
                    Δp io ¼ 2Δp b,id 1+ N rw =N rc Þζ ζ
                                ð
                                            b s
                        ¼ 2 1092  1+ 3=9Þ 0:6814 1:427 ¼ 2833 Pa
                                   ð
             The total shell-side pressure drop reads
                  Δp s ¼ Δp c + Δp w + Δp io ¼ 5700 + 57,641 + 2833 ¼ 66,173 Pa
              (8)  Optimization of the design
             We can carry out the following optimization calculation
                                     min   f xðÞ ¼ N t L
                                 x2 L, d s, l c, l bc Þ
                                   ð
             s:t:
                               Δp s L, d s , l c , l bc Þ Δp s,max   0
                                 ð
                               Δp t L, d s , l c , l bc Þ Δp t,max   0
                                 ð
                              t s,out L, d s , l c , l bc Þ t s,out,max   0
                                 ð
                           Δp s C RF L, d s , l c , C RF l bc Þ Δp s,max   0
                              ð
                           Δp t C RF L, d s , l c , C RF l bc Þ Δp t,max   0
                              ð
                           t s,out C RF L, d s , l c , C RF l bc Þ t s,out,max   0
                              ð
             to optimize the tube length L, shell inside diameter d s , baffle cut l c ,and
             central baffle spacing l bc . The detailed calculation procedure using
             nonlinear programming solver, genetic algorithm solver, and particle
             swarm optimization can be found in the MatLab code for Example 5.1
             in the appendix. For a conservative design, we take the area reserve
             factor of 20% (C RF ¼1.20). The best results were obtained by the use
             of the genetic algorithm solver with integer variables in millimeter as
             follows:
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