1 | SUBROUTINE boundary_conds( range ) |
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2 | |
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3 | !--------------------------------------------------------------------------------! |
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4 | ! This file is part of PALM. |
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5 | ! |
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6 | ! PALM is free software: you can redistribute it and/or modify it under the terms |
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7 | ! of the GNU General Public License as published by the Free Software Foundation, |
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8 | ! either version 3 of the License, or (at your option) any later version. |
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9 | ! |
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10 | ! PALM is distributed in the hope that it will be useful, but WITHOUT ANY |
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11 | ! WARRANTY; without even the implied warranty of MERCHANTABILITY or FITNESS FOR |
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12 | ! A PARTICULAR PURPOSE. See the GNU General Public License for more details. |
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13 | ! |
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14 | ! You should have received a copy of the GNU General Public License along with |
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15 | ! PALM. If not, see <http://www.gnu.org/licenses/>. |
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16 | ! |
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17 | ! Copyright 1997-2012 Leibniz University Hannover |
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18 | !--------------------------------------------------------------------------------! |
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19 | ! |
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20 | ! Current revisions: |
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21 | ! ----------------- |
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22 | ! |
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23 | ! Former revisions: |
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24 | ! ----------------- |
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25 | ! $Id: boundary_conds.f90 1054 2012-11-13 17:30:09Z raasch $ |
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26 | ! |
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27 | ! 1053 2012-11-13 17:11:03Z hoffmann |
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28 | ! boundary conditions for the two new prognostic equations (nr, qr) of the |
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29 | ! two-moment cloud scheme |
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30 | ! |
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31 | ! 1036 2012-10-22 13:43:42Z raasch |
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32 | ! code put under GPL (PALM 3.9) |
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33 | ! |
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34 | ! 996 2012-09-07 10:41:47Z raasch |
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35 | ! little reformatting |
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36 | ! |
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37 | ! 978 2012-08-09 08:28:32Z fricke |
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38 | ! Neumann boudnary conditions are added at the inflow boundary for the SGS-TKE. |
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39 | ! Outflow boundary conditions for the velocity components can be set to Neumann |
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40 | ! conditions or to radiation conditions with a horizontal averaged phase |
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41 | ! velocity. |
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42 | ! |
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43 | ! 875 2012-04-02 15:35:15Z gryschka |
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44 | ! Bugfix in case of dirichlet inflow bc at the right or north boundary |
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45 | ! |
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46 | ! 767 2011-10-14 06:39:12Z raasch |
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47 | ! ug,vg replaced by u_init,v_init as the Dirichlet top boundary condition |
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48 | ! |
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49 | ! 667 2010-12-23 12:06:00Z suehring/gryschka |
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50 | ! nxl-1, nxr+1, nys-1, nyn+1 replaced by nxlg, nxrg, nysg, nyng |
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51 | ! Removed mirror boundary conditions for u and v at the bottom in case of |
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52 | ! ibc_uv_b == 0. Instead, dirichelt boundary conditions (u=v=0) are set |
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53 | ! in init_3d_model |
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54 | ! |
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55 | ! 107 2007-08-17 13:54:45Z raasch |
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56 | ! Boundary conditions for temperature adjusted for coupled runs, |
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57 | ! bugfixes for the radiation boundary conditions at the outflow: radiation |
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58 | ! conditions are used for every substep, phase speeds are calculated for the |
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59 | ! first Runge-Kutta substep only and then reused, several index values changed |
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60 | ! |
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61 | ! 95 2007-06-02 16:48:38Z raasch |
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62 | ! Boundary conditions for salinity added |
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63 | ! |
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64 | ! 75 2007-03-22 09:54:05Z raasch |
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65 | ! The "main" part sets conditions for time level t+dt instead of level t, |
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66 | ! outflow boundary conditions changed from Neumann to radiation condition, |
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67 | ! uxrp, vynp eliminated, moisture renamed humidity |
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68 | ! |
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69 | ! 19 2007-02-23 04:53:48Z raasch |
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70 | ! Boundary conditions for e(nzt), pt(nzt), and q(nzt) removed because these |
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71 | ! gridpoints are now calculated by the prognostic equation, |
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72 | ! Dirichlet and zero gradient condition for pt established at top boundary |
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73 | ! |
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74 | ! RCS Log replace by Id keyword, revision history cleaned up |
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75 | ! |
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76 | ! Revision 1.15 2006/02/23 09:54:55 raasch |
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77 | ! Surface boundary conditions in case of topography: nzb replaced by |
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78 | ! 2d-k-index-arrays (nzb_w_inner, etc.). Conditions for u and v remain |
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79 | ! unchanged (still using nzb) because a non-flat topography must use a |
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80 | ! Prandtl-layer, which don't requires explicit setting of the surface values. |
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81 | ! |
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82 | ! Revision 1.1 1997/09/12 06:21:34 raasch |
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83 | ! Initial revision |
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84 | ! |
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85 | ! |
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86 | ! Description: |
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87 | ! ------------ |
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88 | ! Boundary conditions for the prognostic quantities (range='main'). |
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89 | ! In case of non-cyclic lateral boundaries the conditions for velocities at |
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90 | ! the outflow are set after the pressure solver has been called (range= |
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91 | ! 'outflow_uvw'). |
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92 | ! One additional bottom boundary condition is applied for the TKE (=(u*)**2) |
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93 | ! in prandtl_fluxes. The cyclic lateral boundary conditions are implicitly |
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94 | ! handled in routine exchange_horiz. Pressure boundary conditions are |
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95 | ! explicitly set in routines pres, poisfft, poismg and sor. |
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96 | !------------------------------------------------------------------------------! |
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97 | |
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98 | USE arrays_3d |
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99 | USE control_parameters |
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100 | USE grid_variables |
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101 | USE indices |
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102 | USE pegrid |
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103 | |
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104 | IMPLICIT NONE |
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105 | |
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106 | CHARACTER (LEN=*) :: range |
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107 | |
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108 | INTEGER :: i, j, k |
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109 | |
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110 | REAL :: c_max, denom |
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111 | |
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112 | |
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113 | IF ( range == 'main') THEN |
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114 | ! |
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115 | !-- Bottom boundary |
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116 | IF ( ibc_uv_b == 1 ) THEN |
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117 | u_p(nzb,:,:) = u_p(nzb+1,:,:) |
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118 | v_p(nzb,:,:) = v_p(nzb+1,:,:) |
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119 | ENDIF |
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120 | DO i = nxlg, nxrg |
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121 | DO j = nysg, nyng |
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122 | w_p(nzb_w_inner(j,i),j,i) = 0.0 |
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123 | ENDDO |
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124 | ENDDO |
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125 | |
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126 | ! |
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127 | !-- Top boundary |
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128 | IF ( ibc_uv_t == 0 ) THEN |
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129 | u_p(nzt+1,:,:) = u_init(nzt+1) |
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130 | v_p(nzt+1,:,:) = v_init(nzt+1) |
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131 | ELSE |
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132 | u_p(nzt+1,:,:) = u_p(nzt,:,:) |
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133 | v_p(nzt+1,:,:) = v_p(nzt,:,:) |
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134 | ENDIF |
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135 | w_p(nzt:nzt+1,:,:) = 0.0 ! nzt is not a prognostic level (but cf. pres) |
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136 | |
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137 | ! |
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138 | !-- Temperature at bottom boundary. |
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139 | !-- In case of coupled runs (ibc_pt_b = 2) the temperature is given by |
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140 | !-- the sea surface temperature of the coupled ocean model. |
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141 | IF ( ibc_pt_b == 0 ) THEN |
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142 | DO i = nxlg, nxrg |
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143 | DO j = nysg, nyng |
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144 | pt_p(nzb_s_inner(j,i),j,i) = pt(nzb_s_inner(j,i),j,i) |
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145 | ENDDO |
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146 | ENDDO |
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147 | ELSEIF ( ibc_pt_b == 1 ) THEN |
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148 | DO i = nxlg, nxrg |
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149 | DO j = nysg, nyng |
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150 | pt_p(nzb_s_inner(j,i),j,i) = pt_p(nzb_s_inner(j,i)+1,j,i) |
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151 | ENDDO |
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152 | ENDDO |
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153 | ENDIF |
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154 | |
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155 | ! |
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156 | !-- Temperature at top boundary |
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157 | IF ( ibc_pt_t == 0 ) THEN |
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158 | pt_p(nzt+1,:,:) = pt(nzt+1,:,:) |
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159 | ELSEIF ( ibc_pt_t == 1 ) THEN |
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160 | pt_p(nzt+1,:,:) = pt_p(nzt,:,:) |
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161 | ELSEIF ( ibc_pt_t == 2 ) THEN |
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162 | pt_p(nzt+1,:,:) = pt_p(nzt,:,:) + bc_pt_t_val * dzu(nzt+1) |
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163 | ENDIF |
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164 | |
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165 | ! |
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166 | !-- Boundary conditions for TKE |
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167 | !-- Generally Neumann conditions with de/dz=0 are assumed |
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168 | IF ( .NOT. constant_diffusion ) THEN |
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169 | DO i = nxlg, nxrg |
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170 | DO j = nysg, nyng |
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171 | e_p(nzb_s_inner(j,i),j,i) = e_p(nzb_s_inner(j,i)+1,j,i) |
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172 | ENDDO |
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173 | ENDDO |
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174 | e_p(nzt+1,:,:) = e_p(nzt,:,:) |
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175 | ENDIF |
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176 | |
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177 | ! |
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178 | !-- Boundary conditions for salinity |
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179 | IF ( ocean ) THEN |
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180 | ! |
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181 | !-- Bottom boundary: Neumann condition because salinity flux is always |
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182 | !-- given |
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183 | DO i = nxlg, nxrg |
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184 | DO j = nysg, nyng |
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185 | sa_p(nzb_s_inner(j,i),j,i) = sa_p(nzb_s_inner(j,i)+1,j,i) |
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186 | ENDDO |
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187 | ENDDO |
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188 | |
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189 | ! |
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190 | !-- Top boundary: Dirichlet or Neumann |
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191 | IF ( ibc_sa_t == 0 ) THEN |
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192 | sa_p(nzt+1,:,:) = sa(nzt+1,:,:) |
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193 | ELSEIF ( ibc_sa_t == 1 ) THEN |
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194 | sa_p(nzt+1,:,:) = sa_p(nzt,:,:) |
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195 | ENDIF |
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196 | |
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197 | ENDIF |
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198 | |
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199 | ! |
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200 | !-- Boundary conditions for total water content or scalar, |
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201 | !-- bottom and top boundary (see also temperature) |
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202 | IF ( humidity .OR. passive_scalar ) THEN |
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203 | ! |
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204 | !-- Surface conditions for constant_humidity_flux |
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205 | IF ( ibc_q_b == 0 ) THEN |
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206 | DO i = nxlg, nxrg |
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207 | DO j = nysg, nyng |
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208 | q_p(nzb_s_inner(j,i),j,i) = q(nzb_s_inner(j,i),j,i) |
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209 | ENDDO |
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210 | ENDDO |
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211 | ELSE |
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212 | DO i = nxlg, nxrg |
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213 | DO j = nysg, nyng |
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214 | q_p(nzb_s_inner(j,i),j,i) = q_p(nzb_s_inner(j,i)+1,j,i) |
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215 | ENDDO |
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216 | ENDDO |
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217 | ENDIF |
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218 | ! |
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219 | !-- Top boundary |
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220 | q_p(nzt+1,:,:) = q_p(nzt,:,:) + bc_q_t_val * dzu(nzt+1) |
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221 | |
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222 | IF ( cloud_physics .AND. icloud_scheme == 0 ) THEN |
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223 | ! |
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224 | !-- Surface conditions for constant_humidity_flux |
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225 | IF ( ibc_qr_b == 0 ) THEN |
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226 | DO i = nxlg, nxrg |
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227 | DO j = nysg, nyng |
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228 | qr_p(nzb_s_inner(j,i),j,i) = qr(nzb_s_inner(j,i),j,i) |
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229 | ENDDO |
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230 | ENDDO |
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231 | ELSE |
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232 | DO i = nxlg, nxrg |
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233 | DO j = nysg, nyng |
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234 | qr_p(nzb_s_inner(j,i),j,i) = qr_p(nzb_s_inner(j,i)+1,j,i) |
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235 | ENDDO |
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236 | ENDDO |
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237 | ENDIF |
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238 | ! |
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239 | !-- Top boundary |
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240 | qr_p(nzt+1,:,:) = qr_p(nzt,:,:) + bc_qr_t_val * dzu(nzt+1) |
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241 | ! |
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242 | !-- Surface conditions for constant_humidity_flux |
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243 | IF ( ibc_nr_b == 0 ) THEN |
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244 | DO i = nxlg, nxrg |
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245 | DO j = nysg, nyng |
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246 | nr_p(nzb_s_inner(j,i),j,i) = nr(nzb_s_inner(j,i),j,i) |
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247 | ENDDO |
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248 | ENDDO |
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249 | ELSE |
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250 | DO i = nxlg, nxrg |
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251 | DO j = nysg, nyng |
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252 | nr_p(nzb_s_inner(j,i),j,i) = nr_p(nzb_s_inner(j,i)+1,j,i) |
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253 | ENDDO |
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254 | ENDDO |
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255 | ENDIF |
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256 | ! |
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257 | !-- Top boundary |
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258 | nr_p(nzt+1,:,:) = nr_p(nzt,:,:) + bc_nr_t_val * dzu(nzt+1) |
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259 | ENDIF |
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260 | |
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261 | ENDIF |
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262 | |
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263 | ! |
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264 | !-- In case of inflow at the south boundary the boundary for v is at nys |
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265 | !-- and in case of inflow at the left boundary the boundary for u is at nxl. |
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266 | !-- Since in prognostic_equations (cache optimized version) these levels are |
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267 | !-- handled as a prognostic level, boundary values have to be restored here. |
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268 | !-- For the SGS-TKE, Neumann boundary conditions are used at the inflow. |
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269 | IF ( inflow_s ) THEN |
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270 | v_p(:,nys,:) = v_p(:,nys-1,:) |
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271 | IF ( .NOT. constant_diffusion ) e_p(:,nys-1,:) = e_p(:,nys,:) |
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272 | ELSEIF ( inflow_n ) THEN |
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273 | IF ( .NOT. constant_diffusion ) e_p(:,nyn+1,:) = e_p(:,nyn,:) |
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274 | ELSEIF ( inflow_l ) THEN |
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275 | u_p(:,:,nxl) = u_p(:,:,nxl-1) |
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276 | IF ( .NOT. constant_diffusion ) e_p(:,:,nxl-1) = e_p(:,:,nxl) |
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277 | ELSEIF ( inflow_r ) THEN |
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278 | IF ( .NOT. constant_diffusion ) e_p(:,:,nxr+1) = e_p(:,:,nxr) |
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279 | ENDIF |
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280 | |
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281 | ! |
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282 | !-- Lateral boundary conditions for scalar quantities at the outflow |
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283 | IF ( outflow_s ) THEN |
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284 | pt_p(:,nys-1,:) = pt_p(:,nys,:) |
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285 | IF ( .NOT. constant_diffusion ) e_p(:,nys-1,:) = e_p(:,nys,:) |
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286 | IF ( humidity .OR. passive_scalar ) THEN |
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287 | q_p(:,nys-1,:) = q_p(:,nys,:) |
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288 | IF ( cloud_physics .AND. icloud_scheme == 0 ) THEN |
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289 | qr_p(:,nys-1,:) = qr_p(:,nys,:) |
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290 | nr_p(:,nys-1,:) = nr_p(:,nys,:) |
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291 | ENDIF |
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292 | ENDIF |
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293 | ELSEIF ( outflow_n ) THEN |
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294 | pt_p(:,nyn+1,:) = pt_p(:,nyn,:) |
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295 | IF ( .NOT. constant_diffusion ) e_p(:,nyn+1,:) = e_p(:,nyn,:) |
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296 | IF ( humidity .OR. passive_scalar ) THEN |
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297 | q_p(:,nyn+1,:) = q_p(:,nyn,:) |
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298 | IF ( cloud_physics .AND. icloud_scheme == 0 ) THEN |
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299 | qr_p(:,nyn+1,:) = qr_p(:,nyn,:) |
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300 | nr_p(:,nyn+1,:) = nr_p(:,nyn,:) |
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301 | ENDIF |
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302 | ENDIF |
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303 | ELSEIF ( outflow_l ) THEN |
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304 | pt_p(:,:,nxl-1) = pt_p(:,:,nxl) |
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305 | IF ( .NOT. constant_diffusion ) e_p(:,:,nxl-1) = e_p(:,:,nxl) |
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306 | IF ( humidity .OR. passive_scalar ) THEN |
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307 | q_p(:,:,nxl-1) = q_p(:,:,nxl) |
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308 | IF ( cloud_physics .AND. icloud_scheme == 0 ) THEN |
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309 | qr_p(:,:,nxl-1) = qr_p(:,:,nxl) |
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310 | nr_p(:,:,nxl-1) = nr_p(:,:,nxl) |
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311 | ENDIF |
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312 | ENDIF |
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313 | ELSEIF ( outflow_r ) THEN |
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314 | pt_p(:,:,nxr+1) = pt_p(:,:,nxr) |
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315 | IF ( .NOT. constant_diffusion ) e_p(:,:,nxr+1) = e_p(:,:,nxr) |
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316 | IF ( humidity .OR. passive_scalar ) THEN |
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317 | q_p(:,:,nxr+1) = q_p(:,:,nxr) |
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318 | IF ( cloud_physics .AND. icloud_scheme == 0 ) THEN |
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319 | qr_p(:,:,nxr+1) = qr_p(:,:,nxr) |
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320 | nr_p(:,:,nxr+1) = nr_p(:,:,nxr) |
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321 | ENDIF |
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322 | ENDIF |
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323 | ENDIF |
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324 | |
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325 | ENDIF |
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326 | |
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327 | ! |
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328 | !-- Neumann or Radiation boundary condition for the velocities at the |
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329 | !-- respective outflow |
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330 | IF ( outflow_s ) THEN |
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331 | |
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332 | IF ( bc_ns_dirneu ) THEN |
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333 | u(:,-1,:) = u(:,0,:) |
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334 | v(:,0,:) = v(:,1,:) |
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335 | w(:,-1,:) = w(:,0,:) |
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336 | ELSEIF ( bc_ns_dirrad ) THEN |
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337 | |
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338 | c_max = dy / dt_3d |
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339 | |
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340 | c_u_m_l = 0.0 |
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341 | c_v_m_l = 0.0 |
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342 | c_w_m_l = 0.0 |
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343 | |
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344 | c_u_m = 0.0 |
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345 | c_v_m = 0.0 |
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346 | c_w_m = 0.0 |
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347 | |
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348 | ! |
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349 | !-- Calculate the phase speeds for u, v, and w, first local and then |
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350 | !-- average along the outflow boundary. |
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351 | DO k = nzb+1, nzt+1 |
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352 | DO i = nxl, nxr |
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353 | |
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354 | denom = u_m_s(k,0,i) - u_m_s(k,1,i) |
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355 | |
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356 | IF ( denom /= 0.0 ) THEN |
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357 | c_u(k,i) = -c_max * ( u(k,0,i) - u_m_s(k,0,i) ) / ( denom * tsc(2) ) |
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358 | IF ( c_u(k,i) < 0.0 ) THEN |
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359 | c_u(k,i) = 0.0 |
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360 | ELSEIF ( c_u(k,i) > c_max ) THEN |
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361 | c_u(k,i) = c_max |
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362 | ENDIF |
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363 | ELSE |
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364 | c_u(k,i) = c_max |
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365 | ENDIF |
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366 | |
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367 | denom = v_m_s(k,1,i) - v_m_s(k,2,i) |
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368 | |
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369 | IF ( denom /= 0.0 ) THEN |
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370 | c_v(k,i) = -c_max * ( v(k,1,i) - v_m_s(k,1,i) ) / ( denom * tsc(2) ) |
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371 | IF ( c_v(k,i) < 0.0 ) THEN |
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372 | c_v(k,i) = 0.0 |
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373 | ELSEIF ( c_v(k,i) > c_max ) THEN |
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374 | c_v(k,i) = c_max |
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375 | ENDIF |
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376 | ELSE |
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377 | c_v(k,i) = c_max |
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378 | ENDIF |
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379 | |
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380 | denom = w_m_s(k,0,i) - w_m_s(k,1,i) |
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381 | |
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382 | IF ( denom /= 0.0 ) THEN |
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383 | c_w(k,i) = -c_max * ( w(k,0,i) - w_m_s(k,0,i) ) / ( denom * tsc(2) ) |
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384 | IF ( c_w(k,i) < 0.0 ) THEN |
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385 | c_w(k,i) = 0.0 |
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386 | ELSEIF ( c_w(k,i) > c_max ) THEN |
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387 | c_w(k,i) = c_max |
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388 | ENDIF |
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389 | ELSE |
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390 | c_w(k,i) = c_max |
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391 | ENDIF |
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392 | |
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393 | c_u_m_l(k) = c_u_m_l(k) + c_u(k,i) |
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394 | c_v_m_l(k) = c_v_m_l(k) + c_v(k,i) |
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395 | c_w_m_l(k) = c_w_m_l(k) + c_w(k,i) |
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396 | |
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397 | ENDDO |
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398 | ENDDO |
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399 | |
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400 | #if defined( __parallel ) |
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401 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dx, ierr ) |
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402 | CALL MPI_ALLREDUCE( c_u_m_l(nzb+1), c_u_m(nzb+1), nzt-nzb, MPI_REAL, & |
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403 | MPI_SUM, comm1dx, ierr ) |
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404 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dx, ierr ) |
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405 | CALL MPI_ALLREDUCE( c_v_m_l(nzb+1), c_v_m(nzb+1), nzt-nzb, MPI_REAL, & |
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406 | MPI_SUM, comm1dx, ierr ) |
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407 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dx, ierr ) |
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408 | CALL MPI_ALLREDUCE( c_w_m_l(nzb+1), c_w_m(nzb+1), nzt-nzb, MPI_REAL, & |
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409 | MPI_SUM, comm1dx, ierr ) |
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410 | #else |
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411 | c_u_m = c_u_m_l |
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412 | c_v_m = c_v_m_l |
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413 | c_w_m = c_w_m_l |
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414 | #endif |
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415 | |
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416 | c_u_m = c_u_m / (nx+1) |
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417 | c_v_m = c_v_m / (nx+1) |
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418 | c_w_m = c_w_m / (nx+1) |
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419 | |
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420 | ! |
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421 | !-- Save old timelevels for the next timestep |
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422 | IF ( intermediate_timestep_count == 1 ) THEN |
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423 | u_m_s(:,:,:) = u(:,0:1,:) |
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424 | v_m_s(:,:,:) = v(:,1:2,:) |
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425 | w_m_s(:,:,:) = w(:,0:1,:) |
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426 | ENDIF |
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427 | |
---|
428 | ! |
---|
429 | !-- Calculate the new velocities |
---|
430 | DO k = nzb+1, nzt+1 |
---|
431 | DO i = nxlg, nxrg |
---|
432 | u_p(k,-1,i) = u(k,-1,i) - dt_3d * tsc(2) * c_u_m(k) * & |
---|
433 | ( u(k,-1,i) - u(k,0,i) ) * ddy |
---|
434 | |
---|
435 | v_p(k,0,i) = v(k,0,i) - dt_3d * tsc(2) * c_v_m(k) * & |
---|
436 | ( v(k,0,i) - v(k,1,i) ) * ddy |
---|
437 | |
---|
438 | w_p(k,-1,i) = w(k,-1,i) - dt_3d * tsc(2) * c_w_m(k) * & |
---|
439 | ( w(k,-1,i) - w(k,0,i) ) * ddy |
---|
440 | ENDDO |
---|
441 | ENDDO |
---|
442 | |
---|
443 | ! |
---|
444 | !-- Bottom boundary at the outflow |
---|
445 | IF ( ibc_uv_b == 0 ) THEN |
---|
446 | u_p(nzb,-1,:) = 0.0 |
---|
447 | v_p(nzb,0,:) = 0.0 |
---|
448 | ELSE |
---|
449 | u_p(nzb,-1,:) = u_p(nzb+1,-1,:) |
---|
450 | v_p(nzb,0,:) = v_p(nzb+1,0,:) |
---|
451 | ENDIF |
---|
452 | w_p(nzb,-1,:) = 0.0 |
---|
453 | |
---|
454 | ! |
---|
455 | !-- Top boundary at the outflow |
---|
456 | IF ( ibc_uv_t == 0 ) THEN |
---|
457 | u_p(nzt+1,-1,:) = u_init(nzt+1) |
---|
458 | v_p(nzt+1,0,:) = v_init(nzt+1) |
---|
459 | ELSE |
---|
460 | u_p(nzt+1,-1,:) = u(nzt,-1,:) |
---|
461 | v_p(nzt+1,0,:) = v(nzt,0,:) |
---|
462 | ENDIF |
---|
463 | w_p(nzt:nzt+1,-1,:) = 0.0 |
---|
464 | |
---|
465 | ENDIF |
---|
466 | |
---|
467 | ENDIF |
---|
468 | |
---|
469 | IF ( outflow_n ) THEN |
---|
470 | |
---|
471 | IF ( bc_ns_neudir ) THEN |
---|
472 | u(:,ny+1,:) = u(:,ny,:) |
---|
473 | v(:,ny+1,:) = v(:,ny,:) |
---|
474 | w(:,ny+1,:) = w(:,ny,:) |
---|
475 | ELSEIF ( bc_ns_dirrad ) THEN |
---|
476 | |
---|
477 | c_max = dy / dt_3d |
---|
478 | |
---|
479 | c_u_m_l = 0.0 |
---|
480 | c_v_m_l = 0.0 |
---|
481 | c_w_m_l = 0.0 |
---|
482 | |
---|
483 | c_u_m = 0.0 |
---|
484 | c_v_m = 0.0 |
---|
485 | c_w_m = 0.0 |
---|
486 | |
---|
487 | ! |
---|
488 | !-- Calculate the phase speeds for u, v, and w, first local and then |
---|
489 | !-- average along the outflow boundary. |
---|
490 | DO k = nzb+1, nzt+1 |
---|
491 | DO i = nxl, nxr |
---|
492 | |
---|
493 | denom = u_m_n(k,ny,i) - u_m_n(k,ny-1,i) |
---|
494 | |
---|
495 | IF ( denom /= 0.0 ) THEN |
---|
496 | c_u(k,i) = -c_max * ( u(k,ny,i) - u_m_n(k,ny,i) ) / ( denom * tsc(2) ) |
---|
497 | IF ( c_u(k,i) < 0.0 ) THEN |
---|
498 | c_u(k,i) = 0.0 |
---|
499 | ELSEIF ( c_u(k,i) > c_max ) THEN |
---|
500 | c_u(k,i) = c_max |
---|
501 | ENDIF |
---|
502 | ELSE |
---|
503 | c_u(k,i) = c_max |
---|
504 | ENDIF |
---|
505 | |
---|
506 | denom = v_m_n(k,ny,i) - v_m_n(k,ny-1,i) |
---|
507 | |
---|
508 | IF ( denom /= 0.0 ) THEN |
---|
509 | c_v(k,i) = -c_max * ( v(k,ny,i) - v_m_n(k,ny,i) ) / ( denom * tsc(2) ) |
---|
510 | IF ( c_v(k,i) < 0.0 ) THEN |
---|
511 | c_v(k,i) = 0.0 |
---|
512 | ELSEIF ( c_v(k,i) > c_max ) THEN |
---|
513 | c_v(k,i) = c_max |
---|
514 | ENDIF |
---|
515 | ELSE |
---|
516 | c_v(k,i) = c_max |
---|
517 | ENDIF |
---|
518 | |
---|
519 | denom = w_m_n(k,ny,i) - w_m_n(k,ny-1,i) |
---|
520 | |
---|
521 | IF ( denom /= 0.0 ) THEN |
---|
522 | c_w(k,i) = -c_max * ( w(k,ny,i) - w_m_n(k,ny,i) ) / ( denom * tsc(2) ) |
---|
523 | IF ( c_w(k,i) < 0.0 ) THEN |
---|
524 | c_w(k,i) = 0.0 |
---|
525 | ELSEIF ( c_w(k,i) > c_max ) THEN |
---|
526 | c_w(k,i) = c_max |
---|
527 | ENDIF |
---|
528 | ELSE |
---|
529 | c_w(k,i) = c_max |
---|
530 | ENDIF |
---|
531 | |
---|
532 | c_u_m_l(k) = c_u_m_l(k) + c_u(k,i) |
---|
533 | c_v_m_l(k) = c_v_m_l(k) + c_v(k,i) |
---|
534 | c_w_m_l(k) = c_w_m_l(k) + c_w(k,i) |
---|
535 | |
---|
536 | ENDDO |
---|
537 | ENDDO |
---|
538 | |
---|
539 | #if defined( __parallel ) |
---|
540 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dx, ierr ) |
---|
541 | CALL MPI_ALLREDUCE( c_u_m_l(nzb+1), c_u_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
542 | MPI_SUM, comm1dx, ierr ) |
---|
543 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dx, ierr ) |
---|
544 | CALL MPI_ALLREDUCE( c_v_m_l(nzb+1), c_v_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
545 | MPI_SUM, comm1dx, ierr ) |
---|
546 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dx, ierr ) |
---|
547 | CALL MPI_ALLREDUCE( c_w_m_l(nzb+1), c_w_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
548 | MPI_SUM, comm1dx, ierr ) |
---|
549 | #else |
---|
550 | c_u_m = c_u_m_l |
---|
551 | c_v_m = c_v_m_l |
---|
552 | c_w_m = c_w_m_l |
---|
553 | #endif |
---|
554 | |
---|
555 | c_u_m = c_u_m / (nx+1) |
---|
556 | c_v_m = c_v_m / (nx+1) |
---|
557 | c_w_m = c_w_m / (nx+1) |
---|
558 | |
---|
559 | ! |
---|
560 | !-- Save old timelevels for the next timestep |
---|
561 | IF ( intermediate_timestep_count == 1 ) THEN |
---|
562 | u_m_n(:,:,:) = u(:,ny-1:ny,:) |
---|
563 | v_m_n(:,:,:) = v(:,ny-1:ny,:) |
---|
564 | w_m_n(:,:,:) = w(:,ny-1:ny,:) |
---|
565 | ENDIF |
---|
566 | |
---|
567 | ! |
---|
568 | !-- Calculate the new velocities |
---|
569 | DO k = nzb+1, nzt+1 |
---|
570 | DO i = nxlg, nxrg |
---|
571 | u_p(k,ny+1,i) = u(k,ny+1,i) - dt_3d * tsc(2) * c_u_m(k) * & |
---|
572 | ( u(k,ny+1,i) - u(k,ny,i) ) * ddy |
---|
573 | |
---|
574 | v_p(k,ny+1,i) = v(k,ny+1,i) - dt_3d * tsc(2) * c_v_m(k) * & |
---|
575 | ( v(k,ny+1,i) - v(k,ny,i) ) * ddy |
---|
576 | |
---|
577 | w_p(k,ny+1,i) = w(k,ny+1,i) - dt_3d * tsc(2) * c_w_m(k) * & |
---|
578 | ( w(k,ny+1,i) - w(k,ny,i) ) * ddy |
---|
579 | ENDDO |
---|
580 | ENDDO |
---|
581 | |
---|
582 | ! |
---|
583 | !-- Bottom boundary at the outflow |
---|
584 | IF ( ibc_uv_b == 0 ) THEN |
---|
585 | u_p(nzb,ny+1,:) = 0.0 |
---|
586 | v_p(nzb,ny+1,:) = 0.0 |
---|
587 | ELSE |
---|
588 | u_p(nzb,ny+1,:) = u_p(nzb+1,ny+1,:) |
---|
589 | v_p(nzb,ny+1,:) = v_p(nzb+1,ny+1,:) |
---|
590 | ENDIF |
---|
591 | w_p(nzb,ny+1,:) = 0.0 |
---|
592 | |
---|
593 | ! |
---|
594 | !-- Top boundary at the outflow |
---|
595 | IF ( ibc_uv_t == 0 ) THEN |
---|
596 | u_p(nzt+1,ny+1,:) = u_init(nzt+1) |
---|
597 | v_p(nzt+1,ny+1,:) = v_init(nzt+1) |
---|
598 | ELSE |
---|
599 | u_p(nzt+1,ny+1,:) = u_p(nzt,nyn+1,:) |
---|
600 | v_p(nzt+1,ny+1,:) = v_p(nzt,nyn+1,:) |
---|
601 | ENDIF |
---|
602 | w_p(nzt:nzt+1,ny+1,:) = 0.0 |
---|
603 | |
---|
604 | ENDIF |
---|
605 | |
---|
606 | ENDIF |
---|
607 | |
---|
608 | IF ( outflow_l ) THEN |
---|
609 | |
---|
610 | IF ( bc_lr_neudir ) THEN |
---|
611 | u(:,:,-1) = u(:,:,0) |
---|
612 | v(:,:,0) = v(:,:,1) |
---|
613 | w(:,:,-1) = w(:,:,0) |
---|
614 | ELSEIF ( bc_ns_dirrad ) THEN |
---|
615 | |
---|
616 | c_max = dx / dt_3d |
---|
617 | |
---|
618 | c_u_m_l = 0.0 |
---|
619 | c_v_m_l = 0.0 |
---|
620 | c_w_m_l = 0.0 |
---|
621 | |
---|
622 | c_u_m = 0.0 |
---|
623 | c_v_m = 0.0 |
---|
624 | c_w_m = 0.0 |
---|
625 | |
---|
626 | ! |
---|
627 | !-- Calculate the phase speeds for u, v, and w, first local and then |
---|
628 | !-- average along the outflow boundary. |
---|
629 | DO k = nzb+1, nzt+1 |
---|
630 | DO j = nys, nyn |
---|
631 | |
---|
632 | denom = u_m_l(k,j,1) - u_m_l(k,j,2) |
---|
633 | |
---|
634 | IF ( denom /= 0.0 ) THEN |
---|
635 | c_u(k,j) = -c_max * ( u(k,j,1) - u_m_l(k,j,1) ) / ( denom * tsc(2) ) |
---|
636 | IF ( c_u(k,j) < 0.0 ) THEN |
---|
637 | c_u(k,j) = 0.0 |
---|
638 | ELSEIF ( c_u(k,j) > c_max ) THEN |
---|
639 | c_u(k,j) = c_max |
---|
640 | ENDIF |
---|
641 | ELSE |
---|
642 | c_u(k,j) = c_max |
---|
643 | ENDIF |
---|
644 | |
---|
645 | denom = v_m_l(k,j,0) - v_m_l(k,j,1) |
---|
646 | |
---|
647 | IF ( denom /= 0.0 ) THEN |
---|
648 | c_v(k,j) = -c_max * ( v(k,j,0) - v_m_l(k,j,0) ) / ( denom * tsc(2) ) |
---|
649 | IF ( c_v(k,j) < 0.0 ) THEN |
---|
650 | c_v(k,j) = 0.0 |
---|
651 | ELSEIF ( c_v(k,j) > c_max ) THEN |
---|
652 | c_v(k,j) = c_max |
---|
653 | ENDIF |
---|
654 | ELSE |
---|
655 | c_v(k,j) = c_max |
---|
656 | ENDIF |
---|
657 | |
---|
658 | denom = w_m_l(k,j,0) - w_m_l(k,j,1) |
---|
659 | |
---|
660 | IF ( denom /= 0.0 ) THEN |
---|
661 | c_w(k,j) = -c_max * ( w(k,j,0) - w_m_l(k,j,0) ) / ( denom * tsc(2) ) |
---|
662 | IF ( c_w(k,j) < 0.0 ) THEN |
---|
663 | c_w(k,j) = 0.0 |
---|
664 | ELSEIF ( c_w(k,j) > c_max ) THEN |
---|
665 | c_w(k,j) = c_max |
---|
666 | ENDIF |
---|
667 | ELSE |
---|
668 | c_w(k,j) = c_max |
---|
669 | ENDIF |
---|
670 | |
---|
671 | c_u_m_l(k) = c_u_m_l(k) + c_u(k,j) |
---|
672 | c_v_m_l(k) = c_v_m_l(k) + c_v(k,j) |
---|
673 | c_w_m_l(k) = c_w_m_l(k) + c_w(k,j) |
---|
674 | |
---|
675 | ENDDO |
---|
676 | ENDDO |
---|
677 | |
---|
678 | #if defined( __parallel ) |
---|
679 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dy, ierr ) |
---|
680 | CALL MPI_ALLREDUCE( c_u_m_l(nzb+1), c_u_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
681 | MPI_SUM, comm1dy, ierr ) |
---|
682 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dy, ierr ) |
---|
683 | CALL MPI_ALLREDUCE( c_v_m_l(nzb+1), c_v_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
684 | MPI_SUM, comm1dy, ierr ) |
---|
685 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dy, ierr ) |
---|
686 | CALL MPI_ALLREDUCE( c_w_m_l(nzb+1), c_w_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
687 | MPI_SUM, comm1dy, ierr ) |
---|
688 | #else |
---|
689 | c_u_m = c_u_m_l |
---|
690 | c_v_m = c_v_m_l |
---|
691 | c_w_m = c_w_m_l |
---|
692 | #endif |
---|
693 | |
---|
694 | c_u_m = c_u_m / (ny+1) |
---|
695 | c_v_m = c_v_m / (ny+1) |
---|
696 | c_w_m = c_w_m / (ny+1) |
---|
697 | |
---|
698 | ! |
---|
699 | !-- Save old timelevels for the next timestep |
---|
700 | IF ( intermediate_timestep_count == 1 ) THEN |
---|
701 | u_m_l(:,:,:) = u(:,:,1:2) |
---|
702 | v_m_l(:,:,:) = v(:,:,0:1) |
---|
703 | w_m_l(:,:,:) = w(:,:,0:1) |
---|
704 | ENDIF |
---|
705 | |
---|
706 | ! |
---|
707 | !-- Calculate the new velocities |
---|
708 | DO k = nzb+1, nzt+1 |
---|
709 | DO i = nxlg, nxrg |
---|
710 | u_p(k,j,0) = u(k,j,0) - dt_3d * tsc(2) * c_u_m(k) * & |
---|
711 | ( u(k,j,0) - u(k,j,1) ) * ddx |
---|
712 | |
---|
713 | v_p(k,j,-1) = v(k,j,-1) - dt_3d * tsc(2) * c_v_m(k) * & |
---|
714 | ( v(k,j,-1) - v(k,j,0) ) * ddx |
---|
715 | |
---|
716 | w_p(k,j,-1) = w(k,j,-1) - dt_3d * tsc(2) * c_w_m(k) * & |
---|
717 | ( w(k,j,-1) - w(k,j,0) ) * ddx |
---|
718 | ENDDO |
---|
719 | ENDDO |
---|
720 | |
---|
721 | ! |
---|
722 | !-- Bottom boundary at the outflow |
---|
723 | IF ( ibc_uv_b == 0 ) THEN |
---|
724 | u_p(nzb,:,0) = 0.0 |
---|
725 | v_p(nzb,:,-1) = 0.0 |
---|
726 | ELSE |
---|
727 | u_p(nzb,:,0) = u_p(nzb+1,:,0) |
---|
728 | v_p(nzb,:,-1) = v_p(nzb+1,:,-1) |
---|
729 | ENDIF |
---|
730 | w_p(nzb,:,-1) = 0.0 |
---|
731 | |
---|
732 | ! |
---|
733 | !-- Top boundary at the outflow |
---|
734 | IF ( ibc_uv_t == 0 ) THEN |
---|
735 | u_p(nzt+1,:,-1) = u_init(nzt+1) |
---|
736 | v_p(nzt+1,:,-1) = v_init(nzt+1) |
---|
737 | ELSE |
---|
738 | u_p(nzt+1,:,-1) = u_p(nzt,:,-1) |
---|
739 | v_p(nzt+1,:,-1) = v_p(nzt,:,-1) |
---|
740 | ENDIF |
---|
741 | w_p(nzt:nzt+1,:,-1) = 0.0 |
---|
742 | |
---|
743 | ENDIF |
---|
744 | |
---|
745 | ENDIF |
---|
746 | |
---|
747 | IF ( outflow_r ) THEN |
---|
748 | |
---|
749 | IF ( bc_lr_dirneu ) THEN |
---|
750 | u(:,:,nx+1) = u(:,:,nx) |
---|
751 | v(:,:,nx+1) = v(:,:,nx) |
---|
752 | w(:,:,nx+1) = w(:,:,nx) |
---|
753 | ELSEIF ( bc_ns_dirrad ) THEN |
---|
754 | |
---|
755 | c_max = dx / dt_3d |
---|
756 | |
---|
757 | c_u_m_l = 0.0 |
---|
758 | c_v_m_l = 0.0 |
---|
759 | c_w_m_l = 0.0 |
---|
760 | |
---|
761 | c_u_m = 0.0 |
---|
762 | c_v_m = 0.0 |
---|
763 | c_w_m = 0.0 |
---|
764 | |
---|
765 | ! |
---|
766 | !-- Calculate the phase speeds for u, v, and w, first local and then |
---|
767 | !-- average along the outflow boundary. |
---|
768 | DO k = nzb+1, nzt+1 |
---|
769 | DO j = nys, nyn |
---|
770 | |
---|
771 | denom = u_m_r(k,j,nx) - u_m_r(k,j,nx-1) |
---|
772 | |
---|
773 | IF ( denom /= 0.0 ) THEN |
---|
774 | c_u(k,j) = -c_max * ( u(k,j,nx) - u_m_r(k,j,nx) ) / ( denom * tsc(2) ) |
---|
775 | IF ( c_u(k,j) < 0.0 ) THEN |
---|
776 | c_u(k,j) = 0.0 |
---|
777 | ELSEIF ( c_u(k,j) > c_max ) THEN |
---|
778 | c_u(k,j) = c_max |
---|
779 | ENDIF |
---|
780 | ELSE |
---|
781 | c_u(k,j) = c_max |
---|
782 | ENDIF |
---|
783 | |
---|
784 | denom = v_m_r(k,j,nx) - v_m_r(k,j,nx-1) |
---|
785 | |
---|
786 | IF ( denom /= 0.0 ) THEN |
---|
787 | c_v(k,j) = -c_max * ( v(k,j,nx) - v_m_r(k,j,nx) ) / ( denom * tsc(2) ) |
---|
788 | IF ( c_v(k,j) < 0.0 ) THEN |
---|
789 | c_v(k,j) = 0.0 |
---|
790 | ELSEIF ( c_v(k,j) > c_max ) THEN |
---|
791 | c_v(k,j) = c_max |
---|
792 | ENDIF |
---|
793 | ELSE |
---|
794 | c_v(k,j) = c_max |
---|
795 | ENDIF |
---|
796 | |
---|
797 | denom = w_m_r(k,j,nx) - w_m_r(k,j,nx-1) |
---|
798 | |
---|
799 | IF ( denom /= 0.0 ) THEN |
---|
800 | c_w(k,j) = -c_max * ( w(k,j,nx) - w_m_r(k,j,nx) ) / ( denom * tsc(2) ) |
---|
801 | IF ( c_w(k,j) < 0.0 ) THEN |
---|
802 | c_w(k,j) = 0.0 |
---|
803 | ELSEIF ( c_w(k,j) > c_max ) THEN |
---|
804 | c_w(k,j) = c_max |
---|
805 | ENDIF |
---|
806 | ELSE |
---|
807 | c_w(k,j) = c_max |
---|
808 | ENDIF |
---|
809 | |
---|
810 | c_u_m_l(k) = c_u_m_l(k) + c_u(k,j) |
---|
811 | c_v_m_l(k) = c_v_m_l(k) + c_v(k,j) |
---|
812 | c_w_m_l(k) = c_w_m_l(k) + c_w(k,j) |
---|
813 | |
---|
814 | ENDDO |
---|
815 | ENDDO |
---|
816 | |
---|
817 | #if defined( __parallel ) |
---|
818 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dy, ierr ) |
---|
819 | CALL MPI_ALLREDUCE( c_u_m_l(nzb+1), c_u_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
820 | MPI_SUM, comm1dy, ierr ) |
---|
821 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dy, ierr ) |
---|
822 | CALL MPI_ALLREDUCE( c_v_m_l(nzb+1), c_v_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
823 | MPI_SUM, comm1dy, ierr ) |
---|
824 | IF ( collective_wait ) CALL MPI_BARRIER( comm1dy, ierr ) |
---|
825 | CALL MPI_ALLREDUCE( c_w_m_l(nzb+1), c_w_m(nzb+1), nzt-nzb, MPI_REAL, & |
---|
826 | MPI_SUM, comm1dy, ierr ) |
---|
827 | #else |
---|
828 | c_u_m = c_u_m_l |
---|
829 | c_v_m = c_v_m_l |
---|
830 | c_w_m = c_w_m_l |
---|
831 | #endif |
---|
832 | |
---|
833 | c_u_m = c_u_m / (ny+1) |
---|
834 | c_v_m = c_v_m / (ny+1) |
---|
835 | c_w_m = c_w_m / (ny+1) |
---|
836 | |
---|
837 | ! |
---|
838 | !-- Save old timelevels for the next timestep |
---|
839 | IF ( intermediate_timestep_count == 1 ) THEN |
---|
840 | u_m_r(:,:,:) = u(:,:,nx-1:nx) |
---|
841 | v_m_r(:,:,:) = v(:,:,nx-1:nx) |
---|
842 | w_m_r(:,:,:) = w(:,:,nx-1:nx) |
---|
843 | ENDIF |
---|
844 | |
---|
845 | ! |
---|
846 | !-- Calculate the new velocities |
---|
847 | DO k = nzb+1, nzt+1 |
---|
848 | DO i = nxlg, nxrg |
---|
849 | u_p(k,j,nx+1) = u(k,j,nx+1) - dt_3d * tsc(2) * c_u_m(k) * & |
---|
850 | ( u(k,j,nx+1) - u(k,j,nx) ) * ddx |
---|
851 | |
---|
852 | v_p(k,j,nx+1) = v(k,j,nx+1) - dt_3d * tsc(2) * c_v_m(k) * & |
---|
853 | ( v(k,j,nx+1) - v(k,j,nx) ) * ddx |
---|
854 | |
---|
855 | w_p(k,j,nx+1) = w(k,j,nx+1) - dt_3d * tsc(2) * c_w_m(k) * & |
---|
856 | ( w(k,j,nx+1) - w(k,j,nx) ) * ddx |
---|
857 | ENDDO |
---|
858 | ENDDO |
---|
859 | |
---|
860 | ! |
---|
861 | !-- Bottom boundary at the outflow |
---|
862 | IF ( ibc_uv_b == 0 ) THEN |
---|
863 | u_p(nzb,:,nx+1) = 0.0 |
---|
864 | v_p(nzb,:,nx+1) = 0.0 |
---|
865 | ELSE |
---|
866 | u_p(nzb,:,nx+1) = u_p(nzb+1,:,nx+1) |
---|
867 | v_p(nzb,:,nx+1) = v_p(nzb+1,:,nx+1) |
---|
868 | ENDIF |
---|
869 | w_p(nzb,:,nx+1) = 0.0 |
---|
870 | |
---|
871 | ! |
---|
872 | !-- Top boundary at the outflow |
---|
873 | IF ( ibc_uv_t == 0 ) THEN |
---|
874 | u_p(nzt+1,:,nx+1) = u_init(nzt+1) |
---|
875 | v_p(nzt+1,:,nx+1) = v_init(nzt+1) |
---|
876 | ELSE |
---|
877 | u_p(nzt+1,:,nx+1) = u_p(nzt,:,nx+1) |
---|
878 | v_p(nzt+1,:,nx+1) = v_p(nzt,:,nx+1) |
---|
879 | ENDIF |
---|
880 | w(nzt:nzt+1,:,nx+1) = 0.0 |
---|
881 | |
---|
882 | ENDIF |
---|
883 | |
---|
884 | ENDIF |
---|
885 | |
---|
886 | END SUBROUTINE boundary_conds |
---|