1 | |
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2 | ! $Id: cv3_cine.F90 1992 2014-03-05 13:19:12Z evignon $ |
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3 | |
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4 | SUBROUTINE cv3_cine(nloc, ncum, nd, icb, inb, pbase, plcl, p, ph, tv, tvp, & |
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5 | cina, cinb, plfc) |
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6 | |
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7 | ! ************************************************************** |
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8 | ! * |
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9 | ! CV3_CINE * |
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10 | ! * |
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11 | ! * |
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12 | ! written by : Frederique Cheruy * |
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13 | ! vectorization: Jean-Yves Grandpeix, 19/06/2003, 11.54.43 * |
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14 | ! modified by : * |
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15 | ! ************************************************************** |
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16 | |
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17 | IMPLICIT NONE |
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18 | |
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19 | include "YOMCST.h" |
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20 | include "cvthermo.h" |
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21 | include "cv3param.h" |
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22 | ! input: |
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23 | INTEGER ncum, nd, nloc |
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24 | INTEGER icb(nloc), inb(nloc) |
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25 | REAL pbase(nloc), plcl(nloc) |
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26 | REAL p(nloc, nd), ph(nloc, nd+1) |
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27 | REAL tv(nloc, nd), tvp(nloc, nd) |
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28 | |
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29 | ! output |
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30 | REAL cina(nloc), cinb(nloc), plfc(nloc) |
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31 | |
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32 | ! local variables |
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33 | INTEGER il, i, j, k |
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34 | INTEGER itop(nloc), ineg(nloc), ilow(nloc) |
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35 | INTEGER ifst(nloc), isublcl(nloc) |
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36 | LOGICAL lswitch(nloc), lswitch1(nloc), lswitch2(nloc) |
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37 | LOGICAL exist_lfc(nloc) |
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38 | REAL dpmax |
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39 | REAL deltap, dcin |
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40 | REAL buoylcl(nloc), tvplcl(nloc), tvlcl(nloc) |
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41 | REAL p0(nloc) |
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42 | REAL buoyz(nloc), buoy(nloc, nd) |
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43 | |
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44 | ! ------------------------------------------------------------- |
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45 | ! Initialization |
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46 | ! ------------------------------------------------------------- |
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47 | DO il = 1, ncum |
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48 | cina(il) = 0. |
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49 | cinb(il) = 0. |
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50 | END DO |
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51 | |
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52 | ! -------------------------------------------------------------- |
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53 | ! Recompute buoyancies |
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54 | ! -------------------------------------------------------------- |
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55 | DO k = 1, nd |
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56 | DO il = 1, ncum |
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57 | ! print*,'tvp tv=',tvp(il,k),tv(il,k) |
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58 | buoy(il, k) = tvp(il, k) - tv(il, k) |
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59 | END DO |
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60 | END DO |
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61 | ! --------------------------------------------------------------- |
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62 | |
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63 | ! calcul de la flottabilite a LCL (Buoylcl) |
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64 | ! ifst = first P-level above lcl |
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65 | ! isublcl = highest P-level below lcl. |
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66 | ! --------------------------------------------------------------- |
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67 | |
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68 | DO il = 1, ncum |
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69 | tvplcl(il) = tvp(il, 1)*(plcl(il)/p(il,1))**(2./7.) !For dry air, R/Cp=2/7 |
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70 | END DO |
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71 | |
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72 | DO il = 1, ncum |
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73 | IF (plcl(il)>p(il,icb(il))) THEN |
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74 | ifst(il) = icb(il) |
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75 | isublcl(il) = icb(il) - 1 |
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76 | ELSE |
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77 | ifst(il) = icb(il) + 1 |
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78 | isublcl(il) = icb(il) |
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79 | END IF |
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80 | END DO |
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81 | |
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82 | DO il = 1, ncum |
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83 | tvlcl(il) = tv(il, ifst(il)-1) + (tv(il,ifst(il))-tv(il,ifst(il)-1))*( & |
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84 | plcl(il)-p(il,ifst(il)-1))/(p(il,ifst(il))-p(il,ifst(il)-1)) |
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85 | END DO |
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86 | |
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87 | DO il = 1, ncum |
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88 | buoylcl(il) = tvplcl(il) - tvlcl(il) |
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89 | END DO |
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90 | |
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91 | ! --------------------------------------------------------------- |
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92 | ! premiere couche contenant un niveau de flotabilite positive |
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93 | ! et premiere couche contenant un niveau de flotabilite negative |
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94 | ! au dessus du niveau de condensation |
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95 | ! --------------------------------------------------------------- |
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96 | DO il = 1, ncum |
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97 | itop(il) = nl - 1 |
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98 | ineg(il) = nl - 1 |
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99 | exist_lfc(il) = .FALSE. |
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100 | END DO |
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101 | DO k = nl - 1, 1, -1 |
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102 | DO il = 1, ncum |
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103 | IF (k>=ifst(il)) THEN |
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104 | IF (buoy(il,k)>0.) THEN |
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105 | itop(il) = k |
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106 | exist_lfc(il) = .TRUE. |
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107 | ELSE |
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108 | ineg(il) = k |
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109 | END IF |
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110 | END IF |
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111 | END DO |
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112 | END DO |
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113 | |
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114 | ! --------------------------------------------------------------- |
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115 | ! When there is no positive buoyancy level, set Plfc, Cina and Cinb |
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116 | ! to arbitrary extreme values. |
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117 | ! --------------------------------------------------------------- |
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118 | DO il = 1, ncum |
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119 | IF (.NOT. exist_lfc(il)) THEN |
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120 | plfc(il) = 1.111 |
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121 | cinb(il) = -1111. |
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122 | cina(il) = -1112. |
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123 | END IF |
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124 | END DO |
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125 | |
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126 | |
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127 | ! --------------------------------------------------------------- |
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128 | ! -- Two cases : BUOYlcl >= 0 and BUOYlcl < 0. |
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129 | ! --------------------------------------------------------------- |
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130 | |
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131 | ! -------------------- |
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132 | ! -- 1.0 BUOYlcl >=0. |
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133 | ! -------------------- |
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134 | |
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135 | dpmax = 50. |
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136 | DO il = 1, ncum |
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137 | lswitch1(il) = buoylcl(il) >= 0. .AND. exist_lfc(il) |
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138 | lswitch(il) = lswitch1(il) |
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139 | END DO |
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140 | |
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141 | ! 1.1 No inhibition case |
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142 | ! ---------------------- |
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143 | ! If buoyancy is positive at LCL and stays positive over a large enough |
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144 | ! pressure interval (=DPMAX), inhibition is set to zero, |
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145 | |
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146 | DO il = 1, ncum |
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147 | IF (lswitch(il)) THEN |
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148 | IF (p(il,ineg(il))<p(il,icb(il))-dpmax) THEN |
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149 | plfc(il) = plcl(il) |
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150 | cina(il) = 0. |
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151 | cinb(il) = 0. |
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152 | END IF |
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153 | END IF |
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154 | END DO |
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155 | |
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156 | ! 1.2 Upper inhibition only case |
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157 | ! ------------------------------ |
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158 | DO il = 1, ncum |
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159 | lswitch2(il) = p(il, ineg(il)) >= p(il, icb(il)) - dpmax |
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160 | lswitch(il) = lswitch1(il) .AND. lswitch2(il) |
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161 | END DO |
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162 | |
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163 | DO il = 1, ncum |
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164 | IF (lswitch(il)) THEN |
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165 | cinb(il) = 0. |
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166 | |
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167 | ! 1.2.1 Calcul de la pression du niveau de flot. nulle juste au-dessus |
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168 | ! de LCL |
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169 | ! --------------------------------------------------------------------------- |
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170 | IF (ineg(il)>isublcl(il)+1) THEN |
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171 | ! In order to get P0, one may interpolate linearly buoyancies |
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172 | ! between P(ineg) and P(ineg-1). |
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173 | p0(il) = (buoy(il,ineg(il))*p(il,ineg(il)-1)-buoy(il,ineg( & |
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174 | il)-1)*p(il,ineg(il)))/(buoy(il,ineg(il))-buoy(il,ineg(il)-1)) |
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175 | ELSE |
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176 | ! In order to get P0, one has to interpolate between P(ineg) and |
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177 | ! Plcl. |
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178 | p0(il) = (buoy(il,ineg(il))*plcl(il)-buoylcl(il)*p(il,ineg(il)))/ & |
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179 | (buoy(il,ineg(il))-buoylcl(il)) |
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180 | END IF |
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181 | END IF |
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182 | END DO |
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183 | |
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184 | ! 1.2.2 Recompute itop (=1st layer with positive buoyancy above ineg) |
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185 | ! ------------------------------------------------------------------- |
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186 | DO il = 1, ncum |
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187 | IF (lswitch(il)) THEN |
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188 | itop(il) = nl - 1 |
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189 | END IF |
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190 | END DO |
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191 | |
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192 | DO k = nl, 1, -1 |
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193 | DO il = 1, ncum |
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194 | IF (lswitch(il)) THEN |
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195 | IF (k>=ineg(il) .AND. buoy(il,k)>0) THEN |
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196 | itop(il) = k |
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197 | END IF |
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198 | END IF |
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199 | END DO |
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200 | END DO |
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201 | |
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202 | ! 1.2.3 Computation of PLFC |
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203 | ! ------------------------- |
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204 | DO il = 1, ncum |
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205 | IF (lswitch(il)) THEN |
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206 | plfc(il) = (buoy(il,itop(il))*p(il,itop(il)-1)-buoy(il,itop( & |
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207 | il)-1)*p(il,itop(il)))/(buoy(il,itop(il))-buoy(il,itop(il)-1)) |
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208 | END IF |
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209 | END DO |
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210 | |
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211 | ! 1.2.4 Computation of CINA |
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212 | ! ------------------------- |
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213 | |
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214 | ! Upper part of CINA : integral from P(itop-1) to Plfc |
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215 | DO il = 1, ncum |
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216 | IF (lswitch(il)) THEN |
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217 | deltap = p(il, itop(il)-1) - plfc(il) |
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218 | dcin = rd*buoy(il, itop(il)-1)*deltap/(p(il,itop(il)-1)+plfc(il)) |
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219 | cina(il) = min(0., dcin) |
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220 | END IF |
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221 | END DO |
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222 | |
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223 | ! Middle part of CINA : integral from P(ineg) to P(itop-1) |
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224 | DO k = 1, nl |
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225 | DO il = 1, ncum |
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226 | IF (lswitch(il)) THEN |
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227 | IF (k>=ineg(il) .AND. k<=itop(il)-2) THEN |
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228 | deltap = p(il, k) - p(il, k+1) |
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229 | dcin = 0.5*rd*(buoy(il,k)+buoy(il,k+1))*deltap/ph(il, k+1) |
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230 | cina(il) = cina(il) + min(0., dcin) |
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231 | END IF |
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232 | END IF |
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233 | END DO |
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234 | END DO |
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235 | |
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236 | ! Lower part of CINA : integral from P0 to P(ineg) |
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237 | DO il = 1, ncum |
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238 | IF (lswitch(il)) THEN |
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239 | deltap = p0(il) - p(il, ineg(il)) |
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240 | dcin = rd*buoy(il, ineg(il))*deltap/(p(il,ineg(il))+p0(il)) |
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241 | cina(il) = cina(il) + min(0., dcin) |
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242 | END IF |
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243 | END DO |
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244 | |
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245 | |
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246 | ! ------------------ |
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247 | ! -- 2.0 BUOYlcl <0. |
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248 | ! ------------------ |
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249 | |
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250 | DO il = 1, ncum |
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251 | lswitch1(il) = buoylcl(il) < 0. .AND. exist_lfc(il) |
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252 | lswitch(il) = lswitch1(il) |
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253 | END DO |
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254 | |
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255 | ! 2.0.1 Premiere couche ou la flotabilite est negative au dessus du sol |
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256 | ! ---------------------------------------------------- |
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257 | ! au cas ou elle existe sinon ilow=1 (nk apres) |
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258 | ! on suppose que la parcelle part de la premiere couche |
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259 | |
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260 | DO il = 1, ncum |
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261 | IF (lswitch(il)) THEN |
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262 | ilow(il) = 1 |
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263 | END IF |
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264 | END DO |
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265 | |
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266 | DO k = nl, 1, -1 |
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267 | DO il = 1, ncum |
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268 | IF (lswitch(il) .AND. k<=icb(il)-1) THEN |
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269 | IF (buoy(il,k)<0.) THEN |
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270 | ilow(il) = k |
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271 | END IF |
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272 | END IF |
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273 | END DO |
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274 | END DO |
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275 | |
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276 | ! 2.0.2 Calcul de la pression du niveau de flot. nulle sous le nuage |
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277 | ! ---------------------------------------------------- |
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278 | DO il = 1, ncum |
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279 | IF (lswitch(il)) THEN |
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280 | IF (ilow(il)>1) THEN |
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281 | p0(il) = (buoy(il,ilow(il))*p(il,ilow(il)-1)-buoy(il,ilow( & |
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282 | il)-1)*p(il,ilow(il)))/(buoy(il,ilow(il))-buoy(il,ilow(il)-1)) |
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283 | buoyz(il) = 0. |
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284 | ELSE |
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285 | p0(il) = p(il, 1) |
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286 | buoyz(il) = buoy(il, 1) |
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287 | END IF |
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288 | END IF |
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289 | END DO |
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290 | |
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291 | ! 2.1. Computation of CINB |
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292 | ! ----------------------- |
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293 | |
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294 | DO il = 1, ncum |
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295 | lswitch2(il) = (isublcl(il)==1 .AND. ilow(il)==1) .OR. & |
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296 | (isublcl(il)==ilow(il)-1) |
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297 | lswitch(il) = lswitch1(il) .AND. lswitch2(il) |
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298 | END DO |
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299 | ! c IF ( (isublcl .EQ. 1 .AND. ilow .EQ. 1) |
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300 | ! c $ .OR.(isublcl .EQ. ilow-1)) THEN |
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301 | |
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302 | ! 2.1.1 First case : Plcl just above P0 |
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303 | ! ------------------------------------- |
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304 | DO il = 1, ncum |
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305 | IF (lswitch(il)) THEN |
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306 | deltap = p0(il) - plcl(il) |
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307 | dcin = rd*(buoyz(il)+buoylcl(il))*deltap/(p0(il)+plcl(il)) |
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308 | cinb(il) = min(0., dcin) |
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309 | END IF |
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310 | END DO |
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311 | |
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312 | DO il = 1, ncum |
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313 | lswitch(il) = lswitch1(il) .AND. .NOT. lswitch2(il) |
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314 | END DO |
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315 | ! c ELSE |
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316 | |
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317 | ! 2.1.2 Second case : there is at least one P-level between P0 and Plcl |
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318 | ! --------------------------------------------------------------------- |
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319 | |
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320 | ! Lower part of CINB : integral from P0 to P(ilow) |
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321 | DO il = 1, ncum |
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322 | IF (lswitch(il)) THEN |
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323 | deltap = p0(il) - p(il, ilow(il)) |
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324 | dcin = rd*(buoyz(il)+buoy(il,ilow(il)))*deltap/(p0(il)+p(il,ilow(il))) |
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325 | cinb(il) = min(0., dcin) |
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326 | END IF |
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327 | END DO |
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328 | |
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329 | |
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330 | ! Middle part of CINB : integral from P(ilow) to P(isublcl) |
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331 | ! c DO k = ilow,isublcl-1 |
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332 | DO k = 1, nl |
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333 | DO il = 1, ncum |
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334 | IF (lswitch(il) .AND. k>=ilow(il) .AND. k<=isublcl(il)-1) THEN |
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335 | deltap = p(il, k) - p(il, k+1) |
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336 | dcin = 0.5*rd*(buoy(il,k)+buoy(il,k+1))*deltap/ph(il, k+1) |
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337 | cinb(il) = cinb(il) + min(0., dcin) |
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338 | END IF |
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339 | END DO |
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340 | END DO |
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341 | |
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342 | ! Upper part of CINB : integral from P(isublcl) to Plcl |
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343 | DO il = 1, ncum |
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344 | IF (lswitch(il)) THEN |
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345 | deltap = p(il, isublcl(il)) - plcl(il) |
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346 | dcin = rd*(buoy(il,isublcl(il))+buoylcl(il))*deltap/ & |
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347 | (p(il,isublcl(il))+plcl(il)) |
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348 | cinb(il) = cinb(il) + min(0., dcin) |
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349 | END IF |
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350 | END DO |
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351 | |
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352 | |
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353 | ! c ENDIF |
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354 | |
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355 | ! 2.2 Computation of CINA |
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356 | ! --------------------- |
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357 | |
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358 | DO il = 1, ncum |
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359 | lswitch2(il) = plcl(il) > p(il, itop(il)-1) |
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360 | lswitch(il) = lswitch1(il) .AND. lswitch2(il) |
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361 | END DO |
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362 | |
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363 | ! 2.2.1 FIrst case : Plcl > P(itop-1) |
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364 | ! --------------------------------- |
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365 | ! In order to get Plfc, one may interpolate linearly buoyancies |
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366 | ! between P(itop) and P(itop-1). |
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367 | DO il = 1, ncum |
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368 | IF (lswitch(il)) THEN |
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369 | plfc(il) = (buoy(il,itop(il))*p(il,itop(il)-1)-buoy(il,itop( & |
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370 | il)-1)*p(il,itop(il)))/(buoy(il,itop(il))-buoy(il,itop(il)-1)) |
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371 | END IF |
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372 | END DO |
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373 | |
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374 | ! Upper part of CINA : integral from P(itop-1) to Plfc |
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375 | DO il = 1, ncum |
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376 | IF (lswitch(il)) THEN |
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377 | deltap = p(il, itop(il)-1) - plfc(il) |
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378 | dcin = rd*buoy(il, itop(il)-1)*deltap/(p(il,itop(il)-1)+plfc(il)) |
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379 | cina(il) = min(0., dcin) |
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380 | END IF |
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381 | END DO |
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382 | |
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383 | ! Middle part of CINA : integral from P(icb+1) to P(itop-1) |
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384 | DO k = 1, nl |
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385 | DO il = 1, ncum |
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386 | IF (lswitch(il) .AND. k>=icb(il)+1 .AND. k<=itop(il)-2) THEN |
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387 | deltap = p(il, k) - p(il, k+1) |
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388 | dcin = 0.5*rd*(buoy(il,k)+buoy(il,k+1))*deltap/ph(il, k+1) |
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389 | cina(il) = cina(il) + min(0., dcin) |
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390 | END IF |
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391 | END DO |
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392 | END DO |
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393 | |
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394 | ! Lower part of CINA : integral from Plcl to P(icb+1) |
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395 | DO il = 1, ncum |
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396 | IF (lswitch(il)) THEN |
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397 | IF (plcl(il)>p(il,icb(il))) THEN |
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398 | IF (icb(il)<itop(il)-1) THEN |
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399 | deltap = p(il, icb(il)) - p(il, icb(il)+1) |
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400 | dcin = 0.5*rd*(buoy(il,icb(il))+buoy(il,icb(il)+1))*deltap/ & |
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401 | ph(il, icb(il)+1) |
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402 | cina(il) = cina(il) + min(0., dcin) |
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403 | END IF |
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404 | |
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405 | deltap = plcl(il) - p(il, icb(il)) |
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406 | dcin = rd*(buoylcl(il)+buoy(il,icb(il)))*deltap/ & |
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407 | (plcl(il)+p(il,icb(il))) |
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408 | cina(il) = cina(il) + min(0., dcin) |
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409 | ELSE |
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410 | deltap = plcl(il) - p(il, icb(il)+1) |
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411 | dcin = rd*(buoylcl(il)+buoy(il,icb(il)+1))*deltap/ & |
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412 | (plcl(il)+p(il,icb(il)+1)) |
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413 | cina(il) = cina(il) + min(0., dcin) |
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414 | END IF |
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415 | END IF |
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416 | END DO |
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417 | |
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418 | DO il = 1, ncum |
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419 | lswitch(il) = lswitch1(il) .AND. .NOT. lswitch2(il) |
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420 | END DO |
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421 | ! c ELSE |
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422 | |
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423 | ! 2.2.2 Second case : Plcl lies between P(itop-1) and P(itop); |
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424 | ! ---------------------------------------------------------- |
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425 | ! In order to get Plfc, one has to interpolate between P(itop) and Plcl. |
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426 | DO il = 1, ncum |
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427 | IF (lswitch(il)) THEN |
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428 | plfc(il) = (buoy(il,itop(il))*plcl(il)-buoylcl(il)*p(il,itop(il)))/ & |
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429 | (buoy(il,itop(il))-buoylcl(il)) |
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430 | END IF |
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431 | END DO |
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432 | |
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433 | DO il = 1, ncum |
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434 | IF (lswitch(il)) THEN |
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435 | deltap = plcl(il) - plfc(il) |
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436 | dcin = rd*buoylcl(il)*deltap/(plcl(il)+plfc(il)) |
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437 | cina(il) = min(0., dcin) |
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438 | END IF |
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439 | END DO |
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440 | ! c ENDIF |
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441 | |
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442 | |
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443 | |
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444 | RETURN |
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445 | END SUBROUTINE cv3_cine |
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