1 | ! |
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2 | ! $Header$ |
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3 | ! |
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4 | MODULE mod_clvent |
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5 | |
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6 | REAL, DIMENSION(:), ALLOCATABLE, PRIVATE :: flux_u1 |
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7 | REAL, DIMENSION(:), ALLOCATABLE, PRIVATE :: flux_v1 |
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8 | |
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9 | CONTAINS |
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10 | |
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11 | SUBROUTINE clvent(knon,dtime, u1lay,v1lay,coef,t,ven, & |
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12 | paprs,pplay,delp, & |
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13 | d_ven,flux_v) |
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14 | |
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15 | use dimphy |
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16 | IMPLICIT none |
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17 | !c====================================================================== |
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18 | !c Auteur(s): Z.X. Li (LMD/CNRS) date: 19930818 |
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19 | !c Objet: diffusion vertical de la vitesse "ven" |
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20 | !c====================================================================== |
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21 | !c Arguments: |
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22 | !c dtime----input-R- intervalle du temps (en second) |
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23 | !c u1lay----input-R- vent u de la premiere couche (m/s) |
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24 | !c v1lay----input-R- vent v de la premiere couche (m/s) |
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25 | !c coef-----input-R- le coefficient d'echange (m**2/s) multiplie par |
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26 | !c le cisaillement du vent (dV/dz); la premiere |
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27 | !c valeur indique la valeur de Cdrag (sans unite) |
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28 | !c t--------input-R- temperature (K) |
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29 | !c ven------input-R- vitesse horizontale (m/s) |
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30 | !c paprs----input-R- pression a inter-couche (Pa) |
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31 | !c pplay----input-R- pression au milieu de couche (Pa) |
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32 | !c delp-----input-R- epaisseur de couche (Pa) |
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33 | !c |
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34 | !c |
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35 | !c d_ven----output-R- le changement de "ven" |
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36 | !c flux_v---output-R- (diagnostic) flux du vent: (kg m/s)/(m**2 s) |
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37 | !c====================================================================== |
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38 | !cym#include "dimensions.h" |
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39 | !cym#include "dimphy.h" |
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40 | #include "iniprint.h" |
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41 | INTEGER, INTENT(IN) :: knon |
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42 | REAL, INTENT(IN) :: dtime |
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43 | REAL, INTENT(IN) :: u1lay(klon), v1lay(klon) |
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44 | REAL, INTENT(IN) :: coef(klon,klev) |
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45 | REAL, INTENT(IN) :: t(klon,klev), ven(klon,klev) |
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46 | REAL, INTENT(IN) :: paprs(klon,klev+1), pplay(klon,klev), delp(klon,klev) |
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47 | REAL, INTENT(OUT) :: d_ven(klon,klev) |
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48 | REAL, INTENT(OUT) :: flux_v(klon,klev) |
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49 | !c====================================================================== |
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50 | include "YOMCST.h" |
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51 | !c====================================================================== |
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52 | INTEGER i, k |
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53 | REAL zx_cv(klon,2:klev) |
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54 | REAL zx_dv(klon,2:klev) |
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55 | REAL zx_buf(klon) |
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56 | REAL zx_coef(klon,klev) |
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57 | REAL local_ven(klon,klev) |
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58 | REAL zx_alf1(klon), zx_alf2(klon) |
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59 | |
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60 | |
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61 | d_ven(:,:) = 0.0 |
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62 | flux_v(:,:) = 0.0 |
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63 | !c====================================================================== |
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64 | DO k = 1, klev |
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65 | DO i = 1, knon |
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66 | local_ven(i,k) = ven(i,k) |
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67 | ENDDO |
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68 | ENDDO |
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69 | !c====================================================================== |
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70 | DO i = 1, knon |
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71 | !ccc zx_alf1(i) = (paprs(i,1)-pplay(i,2))/(pplay(i,1)-pplay(i,2)) |
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72 | zx_alf1(i) = 1.0 |
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73 | zx_alf2(i) = 1.0 - zx_alf1(i) |
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74 | zx_coef(i,1) = coef(i,1) & |
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75 | * (1.0+SQRT(u1lay(i)**2+v1lay(i)**2)) & |
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76 | * pplay(i,1)/(RD*t(i,1)) |
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77 | zx_coef(i,1) = zx_coef(i,1) * dtime*RG |
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78 | ENDDO |
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79 | !c====================================================================== |
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80 | DO k = 2, klev |
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81 | DO i = 1, knon |
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82 | zx_coef(i,k) = coef(i,k)*RG/(pplay(i,k-1)-pplay(i,k)) & |
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83 | *(paprs(i,k)*2/(t(i,k)+t(i,k-1))/RD)**2 |
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84 | zx_coef(i,k) = zx_coef(i,k) * dtime*RG |
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85 | ENDDO |
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86 | ENDDO |
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87 | !c====================================================================== |
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88 | DO i = 1, knon |
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89 | zx_buf(i) = delp(i,1) + zx_coef(i,1)*zx_alf1(i)+zx_coef(i,2) |
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90 | zx_cv(i,2) = local_ven(i,1)*delp(i,1) / zx_buf(i) |
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91 | zx_dv(i,2) = (zx_coef(i,2)-zx_alf2(i)*zx_coef(i,1)) & |
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92 | /zx_buf(i) |
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93 | ENDDO |
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94 | DO k = 3, klev |
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95 | DO i = 1, knon |
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96 | zx_buf(i) = delp(i,k-1) + zx_coef(i,k) & |
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97 | + zx_coef(i,k-1)*(1.-zx_dv(i,k-1)) |
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98 | zx_cv(i,k) = (local_ven(i,k-1)*delp(i,k-1) & |
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99 | +zx_coef(i,k-1)*zx_cv(i,k-1) )/zx_buf(i) |
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100 | zx_dv(i,k) = zx_coef(i,k)/zx_buf(i) |
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101 | ENDDO |
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102 | ENDDO |
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103 | DO i = 1, knon |
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104 | local_ven(i,klev) = ( local_ven(i,klev)*delp(i,klev) & |
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105 | +zx_coef(i,klev)*zx_cv(i,klev) ) & |
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106 | / ( delp(i,klev) + zx_coef(i,klev) & |
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107 | -zx_coef(i,klev)*zx_dv(i,klev) ) |
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108 | ENDDO |
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109 | DO k = klev-1, 1, -1 |
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110 | DO i = 1, knon |
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111 | local_ven(i,k) = zx_cv(i,k+1) + zx_dv(i,k+1)*local_ven(i,k+1) |
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112 | ENDDO |
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113 | ENDDO |
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114 | !c====================================================================== |
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115 | !c== flux_v est le flux de moment angulaire (positif vers bas) |
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116 | !c== dont l'unite est: (kg m/s)/(m**2 s) |
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117 | DO i = 1, knon |
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118 | flux_v(i,1) = zx_coef(i,1)/(RG*dtime) & |
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119 | *(local_ven(i,1)*zx_alf1(i) & |
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120 | +local_ven(i,2)*zx_alf2(i)) |
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121 | ENDDO |
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122 | DO k = 2, klev |
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123 | DO i = 1, knon |
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124 | flux_v(i,k) = zx_coef(i,k)/(RG*dtime) & |
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125 | * (local_ven(i,k)-local_ven(i,k-1)) |
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126 | ENDDO |
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127 | ENDDO |
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128 | !c |
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129 | DO k = 1, klev |
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130 | DO i = 1, knon |
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131 | d_ven(i,k) = local_ven(i,k) - ven(i,k) |
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132 | ENDDO |
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133 | ENDDO |
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134 | !c |
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135 | ! RETURN |
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136 | |
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137 | |
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138 | |
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139 | END SUBROUTINE clvent |
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140 | |
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141 | |
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142 | SUBROUTINE save_flux(klon, flux_u_in, flux_v_in) |
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143 | |
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144 | INTEGER, INTENT(IN) :: klon |
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145 | REAL, DIMENSION(klon), INTENT(IN) :: flux_u_in |
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146 | REAL, DIMENSION(klon), INTENT(IN) :: flux_v_in |
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147 | |
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148 | if (.not. allocated(flux_u1)) ALLOCATE(flux_u1(klon), flux_v1(klon)) |
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149 | |
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150 | flux_u1(:) = flux_u_in(:) |
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151 | flux_v1(:) = flux_v_in(:) |
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152 | |
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153 | |
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154 | END SUBROUTINE save_flux |
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155 | |
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156 | SUBROUTINE calcul_flux_vent(klon, flux_u, flux_v) |
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157 | |
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158 | INTEGER, INTENT(IN) :: klon |
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159 | ! Output |
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160 | REAL, DIMENSION(klon), INTENT(OUT) :: flux_u |
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161 | REAL, DIMENSION(klon), INTENT(OUT) :: flux_v |
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162 | |
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163 | flux_u = flux_u1 |
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164 | flux_v = flux_v1 |
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165 | |
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166 | END SUBROUTINE calcul_flux_vent |
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167 | |
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168 | END MODULE mod_clvent |
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