1 | ! |
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2 | ! $Header$ |
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3 | ! |
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4 | SUBROUTINE suphel |
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5 | C |
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6 | #include "YOMCST.h" |
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7 | #include "YOETHF.h" |
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8 | cIM cf. JLD |
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9 | LOGICAL firstcall |
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10 | SAVE firstcall |
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11 | c$OMP THREADPRIVATE(firstcall) |
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12 | DATA firstcall /.TRUE./ |
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13 | |
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14 | IF (firstcall) THEN |
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15 | PRINT*, 'suphel initialise les constantes du GCM' |
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16 | firstcall = .FALSE. |
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17 | ELSE |
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18 | PRINT*, 'suphel DEJA APPELE ' |
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19 | RETURN |
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20 | ENDIF |
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21 | C ----------------------------------------------------------------- |
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22 | C |
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23 | C* 1. DEFINE FUNDAMENTAL CONSTANTS. |
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24 | C ----------------------------- |
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25 | C |
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26 | WRITE(UNIT=6,FMT='(''0*** Constants of the ICM ***'')') |
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27 | RPI=2.*ASIN(1.) |
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28 | RCLUM=299792458. |
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29 | RHPLA=6.6260755E-34 |
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30 | RKBOL=1.380658E-23 |
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31 | RNAVO=6.0221367E+23 |
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32 | WRITE(UNIT=6,FMT='('' *** Fundamental constants ***'')') |
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33 | WRITE(UNIT=6,FMT='('' PI = '',E13.7,'' -'')')RPI |
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34 | WRITE(UNIT=6,FMT='('' c = '',E13.7,''m s-1'')') |
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35 | S RCLUM |
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36 | WRITE(UNIT=6,FMT='('' h = '',E13.7,''J s'')') |
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37 | S RHPLA |
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38 | WRITE(UNIT=6,FMT='('' K = '',E13.7,''J K-1'')') |
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39 | S RKBOL |
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40 | WRITE(UNIT=6,FMT='('' N = '',E13.7,''mol-1'')') |
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41 | S RNAVO |
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42 | C |
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43 | C ---------------------------------------------------------------- |
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44 | C |
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45 | C* 2. DEFINE ASTRONOMICAL CONSTANTS. |
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46 | C ------------------------------ |
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47 | C |
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48 | RDAY=86400. |
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49 | REA=149597870000. |
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50 | REPSM=0.409093 |
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51 | C |
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52 | RSIYEA=365.25*RDAY*2.*RPI/6.283076 |
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53 | RSIDAY=RDAY/(1.+RDAY/RSIYEA) |
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54 | ROMEGA=2.*RPI/RSIDAY |
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55 | c |
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56 | c exp1 R_ecc = 0.05 |
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57 | c exp1 R_peri = 102.04 |
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58 | c exp1 R_incl = 22.5 |
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59 | c exp1 print*, 'Parametres orbitaux modifies' |
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60 | c ref R_ecc = 0.016724 |
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61 | c ref R_peri = 102.04 |
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62 | c ref R_incl = 23.5 |
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63 | c |
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64 | cIM 161002 : pour avoir les ctes AMIP II |
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65 | cIM 161002 R_ecc = 0.016724 |
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66 | cIM 161002 R_peri = 102.04 |
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67 | cIM 161002 R_incl = 23.5 |
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68 | cIM on mets R_ecc, R_peri, R_incl dans conf_phys.F90 |
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69 | c R_ecc = 0.016715 |
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70 | c R_peri = 102.7 |
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71 | c R_incl = 23.441 |
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72 | c |
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73 | WRITE(UNIT=6,FMT='('' *** Astronomical constants ***'')') |
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74 | WRITE(UNIT=6,FMT='('' day = '',E13.7,'' s'')')RDAY |
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75 | WRITE(UNIT=6,FMT='('' half g. axis = '',E13.7,'' m'')')REA |
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76 | WRITE(UNIT=6,FMT='('' mean anomaly = '',E13.7,'' -'')')REPSM |
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77 | WRITE(UNIT=6,FMT='('' sideral year = '',E13.7,'' s'')')RSIYEA |
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78 | WRITE(UNIT=6,FMT='('' sideral day = '',E13.7,'' s'')')RSIDAY |
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79 | WRITE(UNIT=6,FMT='('' omega = '',E13.7,'' s-1'')') |
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80 | S ROMEGA |
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81 | c write(unit=6,fmt='('' excentricite = '',e13.7,''-'')')R_ecc |
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82 | c write(unit=6,fmt='('' equinoxe = '',e13.7,''-'')')R_peri |
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83 | c write(unit=6,fmt='('' inclinaison = '',e13.7,''-'')')R_incl |
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84 | C |
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85 | C ------------------------------------------------------------------ |
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86 | C |
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87 | C* 3. DEFINE GEOIDE. |
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88 | C -------------- |
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89 | C |
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90 | RG=9.80665 |
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91 | RA=6371229. |
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92 | R1SA=SNGL(1.D0/DBLE(RA)) |
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93 | WRITE(UNIT=6,FMT='('' *** Geoide ***'')') |
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94 | WRITE(UNIT=6,FMT='('' Gravity = '',E13.7,'' m s-2'')') |
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95 | S RG |
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96 | WRITE(UNIT=6,FMT='('' Earth radius = '',E13.7,'' m'')')RA |
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97 | WRITE(UNIT=6,FMT='('' Inverse E.R. = '',E13.7,'' m'')')R1SA |
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98 | C |
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99 | C ----------------------------------------------------------------- |
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100 | C |
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101 | C* 4. DEFINE RADIATION CONSTANTS. |
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102 | C --------------------------- |
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103 | C |
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104 | c z.x.li RSIGMA=2. * RPI**5 * RKBOL**4 /(15.* RCLUM**2 * RHPLA**3) |
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105 | rsigma = 2.*rpi**5 * (rkbol/rhpla)**3 * rkbol/rclum/rclum/15. |
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106 | cIM init. dans conf_phys.F90 RI0=1365. |
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107 | WRITE(UNIT=6,FMT='('' *** Radiation ***'')') |
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108 | WRITE(UNIT=6,FMT='('' Stefan-Bol. = '',E13.7,'' W m-2 K-4'' |
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109 | S )') RSIGMA |
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110 | cIM init. dans conf_phys.F90 WRITE(UNIT=6,FMT='('' Solar const. = '',E13.7,'' W m-2'')') |
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111 | cIM init. dans conf_phys.F90 S RI0 |
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112 | C |
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113 | C ----------------------------------------------------------------- |
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114 | C |
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115 | C* 5. DEFINE THERMODYNAMIC CONSTANTS, GAS PHASE. |
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116 | C ------------------------------------------ |
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117 | C |
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118 | R=RNAVO*RKBOL |
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119 | RMD=28.9644 |
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120 | RMO3=47.9942 |
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121 | RMV=18.0153 |
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122 | RD=1000.*R/RMD |
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123 | RV=1000.*R/RMV |
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124 | RCPD=3.5*RD |
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125 | RCVD=RCPD-RD |
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126 | RCPV=4. *RV |
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127 | RCVV=RCPV-RV |
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128 | RKAPPA=RD/RCPD |
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129 | RETV=RV/RD-1. |
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130 | WRITE(UNIT=6,FMT='('' *** Thermodynamic, gas ***'')') |
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131 | WRITE(UNIT=6,FMT='('' Perfect gas = '',e13.7)') R |
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132 | WRITE(UNIT=6,FMT='('' Dry air mass = '',e13.7)') RMD |
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133 | WRITE(UNIT=6,FMT='('' Ozone mass = '',e13.7)') RMO3 |
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134 | WRITE(UNIT=6,FMT='('' Vapour mass = '',e13.7)') RMV |
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135 | WRITE(UNIT=6,FMT='('' Dry air cst. = '',e13.7)') RD |
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136 | WRITE(UNIT=6,FMT='('' Vapour cst. = '',e13.7)') RV |
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137 | WRITE(UNIT=6,FMT='('' Cpd = '',e13.7)') RCPD |
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138 | WRITE(UNIT=6,FMT='('' Cvd = '',e13.7)') RCVD |
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139 | WRITE(UNIT=6,FMT='('' Cpv = '',e13.7)') RCPV |
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140 | WRITE(UNIT=6,FMT='('' Cvv = '',e13.7)') RCVV |
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141 | WRITE(UNIT=6,FMT='('' Rd/Cpd = '',e13.7)') RKAPPA |
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142 | WRITE(UNIT=6,FMT='('' Rv/Rd-1 = '',e13.7)') RETV |
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143 | C |
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144 | C ---------------------------------------------------------------- |
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145 | C |
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146 | C* 6. DEFINE THERMODYNAMIC CONSTANTS, LIQUID PHASE. |
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147 | C --------------------------------------------- |
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148 | C |
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149 | RCW=RCPV |
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150 | WRITE(UNIT=6,FMT='('' *** Thermodynamic, liquid ***'')') |
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151 | WRITE(UNIT=6,FMT='('' Cw = '',E13.7)') RCW |
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152 | C |
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153 | C ---------------------------------------------------------------- |
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154 | C |
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155 | C* 7. DEFINE THERMODYNAMIC CONSTANTS, SOLID PHASE. |
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156 | C -------------------------------------------- |
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157 | C |
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158 | RCS=RCPV |
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159 | WRITE(UNIT=6,FMT='('' *** thermodynamic, solid ***'')') |
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160 | WRITE(UNIT=6,FMT='('' Cs = '',E13.7)') RCS |
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161 | C |
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162 | C ---------------------------------------------------------------- |
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163 | C |
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164 | C* 8. DEFINE THERMODYNAMIC CONSTANTS, TRANSITION OF PHASE. |
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165 | C ---------------------------------------------------- |
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166 | C |
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167 | RTT=273.16 |
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168 | RLVTT=2.5008E+6 |
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169 | RLSTT=2.8345E+6 |
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170 | RLMLT=RLSTT-RLVTT |
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171 | RATM=100000. |
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172 | WRITE(UNIT=6,FMT='('' *** Thermodynamic, trans. ***'')') |
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173 | WRITE(UNIT=6,FMT='('' Fusion point = '',E13.7)') RTT |
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174 | WRITE(UNIT=6,FMT='('' RLvTt = '',E13.7)') RLVTT |
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175 | WRITE(UNIT=6,FMT='('' RLsTt = '',E13.7)') RLSTT |
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176 | WRITE(UNIT=6,FMT='('' RLMlt = '',E13.7)') RLMLT |
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177 | WRITE(UNIT=6,FMT='('' Normal press. = '',E13.7)') RATM |
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178 | WRITE(UNIT=6,FMT='('' Latent heat : '')') |
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179 | C |
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180 | C ---------------------------------------------------------------- |
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181 | C |
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182 | C* 9. SATURATED VAPOUR PRESSURE. |
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183 | C -------------------------- |
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184 | C |
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185 | RESTT=611.14 |
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186 | RGAMW=(RCW-RCPV)/RV |
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187 | RBETW=RLVTT/RV+RGAMW*RTT |
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188 | RALPW=LOG(RESTT)+RBETW/RTT+RGAMW*LOG(RTT) |
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189 | RGAMS=(RCS-RCPV)/RV |
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190 | RBETS=RLSTT/RV+RGAMS*RTT |
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191 | RALPS=LOG(RESTT)+RBETS/RTT+RGAMS*LOG(RTT) |
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192 | RGAMD=RGAMS-RGAMW |
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193 | RBETD=RBETS-RBETW |
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194 | RALPD=RALPS-RALPW |
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195 | C |
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196 | C ------------------------------------------------------------------ |
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197 | c |
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198 | c calculer les constantes pour les fonctions thermodynamiques |
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199 | c |
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200 | RVTMP2=RCPV/RCPD-1. |
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201 | RHOH2O=RATM/100. |
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202 | R2ES=RESTT*RD/RV |
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203 | R3LES=17.269 |
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204 | R3IES=21.875 |
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205 | R4LES=35.86 |
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206 | R4IES=7.66 |
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207 | R5LES=R3LES*(RTT-R4LES) |
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208 | R5IES=R3IES*(RTT-R4IES) |
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209 | C |
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210 | RETURN |
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211 | END |
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