Page 546 - Design and Operation of Heat Exchangers and their Networks
P. 546

Appendix  529


                     Re_tb = G_s_max ∗ d_o / mu_s; % shellside Reynolds number
                     Hg_lam = 140 ∗ Re_tb ∗ (((s_l / d_o)  ^  0.5 - 0.6)  ^  2 + 0.75) ...
                        / (s_t_ / d_o)  ^  1.6 / (4 ∗ (s_l / d_o) ∗ (s_t / d_o) ...
                        / pi - 1); % Hagen number for laminar flow
                     if (N_rc >= 0)
                         phi_t_n = 0;
                     else
                       if (s_l >= s_l_min)
                             phi_t_n = (1 / N_rc - 0.1) / 2 / (s_t / d_o)  ^  2;
                       else
                             phi_t_n = (1 / N_rc - 0.1) ∗ 2 ∗ ((s_d / d_o - 1) ...
                                / (s_t / d_o) / (s_t / d_o - 1))  ^  2;
                       end
                     end
                     Hg_tur_s_0 = phi_t_n ∗ Re_tb  ^  2 + Re_tb  ^  1.75 ∗ (1.25 + 0.6 ...
                        / (s_t / d_o - 0.85)  ^  1.08 + 0.2 ∗ (s_l / s_t - 1)  ^  3 ...
                        -0.005 ∗ (s_t / s_l - 1)  ^  3);
                     Hg_tur_s = Hg_tur_s_0;
                     % Hagen number for turbulent flow for staggered tube bundles
                     if (Re_tb > 2.5E5)
                          Hg_tur_s = Hg_tur_s ∗ (1 + (Re_tb -2.5E5) / 3.25E5);
                     end
                     Hg = Hg_lam;
                     if (Re_tb > 800)
                          Hg = Hg + Hg_tur_s ∗ (1 - exp(1 - (Re_tb + 200) / 1000));
                     end
                     if (s_l >= s_l_min)
                          Nu_id = 0.404 ∗ (0.92 ∗ Hg ∗ Pr_s ...
                             ∗ (4 ∗ s_t / pi - d_o) / s_d)  ^  (1 / 3);
                          % Nusselt number for the staggered tube bundles
                     else
                          Nu_id = 0.404 ∗ (0.92 ∗ Hg ∗ Pr_s ...
                             ∗ (4 ∗ s_t ∗ s_l / pi - d_o  ^  2) / (s_l ∗ s_d))  ^  (1 / 3);
                          % Nusselt number for the staggered tube bundles
                     end
                     alpha_id = Nu_id ∗ lambda_s / d_o;
                     % heat transfer coefficient for ideal crossflow

                     % correction factor for baffle configuration
                     J_c = 0.55 + 0.72 ∗ F_c;
   541   542   543   544   545   546   547   548   549   550   551