[2] | 1 | SUBROUTINE suphec |
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| 2 | C |
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| 3 | #include "YOMCST.h" |
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| 4 | #include "YOETHF.h" |
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| 5 | C ----------------------------------------------------------------- |
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| 6 | C |
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| 7 | C* 1. DEFINE FUNDAMENTAL CONSTANTS. |
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| 8 | C ----------------------------- |
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| 9 | C |
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| 10 | WRITE(UNIT=6,FMT='(''0*** Constants of the ICM ***'')') |
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| 11 | RPI=2.*ASIN(1.) |
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| 12 | RCLUM=299792458. |
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| 13 | RHPLA=6.6260755E-34 |
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| 14 | RKBOL=1.380658E-23 |
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| 15 | RNAVO=6.0221367E+23 |
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| 16 | WRITE(UNIT=6,FMT='('' *** Fundamental constants ***'')') |
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| 17 | WRITE(UNIT=6,FMT='('' PI = '',E13.7,'' -'')')RPI |
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| 18 | WRITE(UNIT=6,FMT='('' c = '',E13.7,''m s-1'')') |
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| 19 | S RCLUM |
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| 20 | WRITE(UNIT=6,FMT='('' h = '',E13.7,''J s'')') |
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| 21 | S RHPLA |
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| 22 | WRITE(UNIT=6,FMT='('' K = '',E13.7,''J K-1'')') |
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| 23 | S RKBOL |
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| 24 | WRITE(UNIT=6,FMT='('' N = '',E13.7,''mol-1'')') |
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| 25 | S RNAVO |
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| 26 | C |
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| 27 | C ---------------------------------------------------------------- |
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| 28 | C |
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| 29 | C* 2. DEFINE ASTRONOMICAL CONSTANTS. |
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| 30 | C ------------------------------ |
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| 31 | C |
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| 32 | RDAY=86400. |
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| 33 | REA=149597870000. |
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| 34 | REPSM=0.409093 |
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| 35 | C |
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| 36 | RSIYEA=365.25*RDAY*2.*RPI/6.283076 |
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| 37 | RSIDAY=RDAY/(1.+RDAY/RSIYEA) |
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| 38 | ROMEGA=2.*RPI/RSIDAY |
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| 39 | c |
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| 40 | c exp1 R_ecc = 0.05 |
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| 41 | c exp1 R_peri = 102.04 |
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| 42 | c exp1 R_incl = 22.5 |
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| 43 | c exp1 print*, 'Parametres orbitaux modifies' |
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| 44 | c ref R_ecc = 0.016724 |
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| 45 | c ref R_peri = 102.04 |
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| 46 | c ref R_incl = 23.5 |
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| 47 | R_ecc = 0.016724 |
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| 48 | R_peri = 102.04 |
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| 49 | R_incl = 23.5 |
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| 50 | c |
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| 51 | WRITE(UNIT=6,FMT='('' *** Astronomical constants ***'')') |
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| 52 | WRITE(UNIT=6,FMT='('' day = '',E13.7,'' s'')')RDAY |
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| 53 | WRITE(UNIT=6,FMT='('' half g. axis = '',E13.7,'' m'')')REA |
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| 54 | WRITE(UNIT=6,FMT='('' mean anomaly = '',E13.7,'' -'')')REPSM |
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| 55 | WRITE(UNIT=6,FMT='('' sideral year = '',E13.7,'' s'')')RSIYEA |
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| 56 | WRITE(UNIT=6,FMT='('' sideral day = '',E13.7,'' s'')')RSIDAY |
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| 57 | WRITE(UNIT=6,FMT='('' omega = '',E13.7,'' s-1'')') |
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| 58 | S ROMEGA |
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| 59 | write(unit=6,fmt='('' excentricite = '',e13.7,''-'')')R_ecc |
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| 60 | write(unit=6,fmt='('' equinoxe = '',e13.7,''-'')')R_peri |
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| 61 | write(unit=6,fmt='('' inclinaison = '',e13.7,''-'')')R_incl |
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| 62 | C |
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| 63 | C ------------------------------------------------------------------ |
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| 64 | C |
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| 65 | C* 3. DEFINE GEOIDE. |
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| 66 | C -------------- |
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| 67 | C |
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| 68 | RG=9.80665 |
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| 69 | RA=6371229. |
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| 70 | R1SA=SNGL(1.D0/DBLE(RA)) |
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| 71 | WRITE(UNIT=6,FMT='('' *** Geoide ***'')') |
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| 72 | WRITE(UNIT=6,FMT='('' Gravity = '',E13.7,'' m s-2'')') |
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| 73 | S RG |
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| 74 | WRITE(UNIT=6,FMT='('' Earth radius = '',E13.7,'' m'')')RA |
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| 75 | WRITE(UNIT=6,FMT='('' Inverse E.R. = '',E13.7,'' m'')')R1SA |
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| 76 | C |
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| 77 | C ----------------------------------------------------------------- |
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| 78 | C |
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| 79 | C* 4. DEFINE RADIATION CONSTANTS. |
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| 80 | C --------------------------- |
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| 81 | C |
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| 82 | c z.x.li RSIGMA=2. * RPI**5 * RKBOL**4 /(15.* RCLUM**2 * RHPLA**3) |
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| 83 | rsigma = 2.*rpi**5 * (rkbol/rhpla)**3 * rkbol/rclum/rclum/15. |
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| 84 | RI0=1370. |
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| 85 | WRITE(UNIT=6,FMT='('' *** Radiation ***'')') |
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| 86 | WRITE(UNIT=6,FMT='('' Stefan-Bol. = '',E13.7,'' W m-2 K-4'' |
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| 87 | S )') RSIGMA |
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| 88 | WRITE(UNIT=6,FMT='('' Solar const. = '',E13.7,'' W m-2'')') |
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| 89 | S RI0 |
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| 90 | C |
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| 91 | C ----------------------------------------------------------------- |
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| 92 | C |
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| 93 | C* 5. DEFINE THERMODYNAMIC CONSTANTS, GAS PHASE. |
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| 94 | C ------------------------------------------ |
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| 95 | C |
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| 96 | R=RNAVO*RKBOL |
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| 97 | RMD=28.9644 |
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| 98 | RMV=18.0153 |
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| 99 | RD=1000.*R/RMD |
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| 100 | RV=1000.*R/RMV |
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| 101 | RCPD=3.5*RD |
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| 102 | RCVD=RCPD-RD |
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| 103 | RCPV=4. *RV |
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| 104 | RCVV=RCPV-RV |
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| 105 | RKAPPA=RD/RCPD |
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| 106 | RETV=RV/RD-1. |
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| 107 | WRITE(UNIT=6,FMT='('' *** Thermodynamic, gas ***'')') |
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| 108 | WRITE(UNIT=6,FMT='('' Perfect gas = '',e13.7)') R |
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| 109 | WRITE(UNIT=6,FMT='('' Dry air mass = '',e13.7)') RMD |
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| 110 | WRITE(UNIT=6,FMT='('' Vapour mass = '',e13.7)') RMV |
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| 111 | WRITE(UNIT=6,FMT='('' Dry air cst. = '',e13.7)') RD |
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| 112 | WRITE(UNIT=6,FMT='('' Vapour cst. = '',e13.7)') RV |
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| 113 | WRITE(UNIT=6,FMT='('' Cpd = '',e13.7)') RCPD |
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| 114 | WRITE(UNIT=6,FMT='('' Cvd = '',e13.7)') RCVD |
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| 115 | WRITE(UNIT=6,FMT='('' Cpv = '',e13.7)') RCPV |
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| 116 | WRITE(UNIT=6,FMT='('' Cvv = '',e13.7)') RCVV |
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| 117 | WRITE(UNIT=6,FMT='('' Rd/Cpd = '',e13.7)') RKAPPA |
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| 118 | WRITE(UNIT=6,FMT='('' Rv/Rd-1 = '',e13.7)') RETV |
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| 119 | C |
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| 120 | C ---------------------------------------------------------------- |
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| 121 | C |
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| 122 | C* 6. DEFINE THERMODYNAMIC CONSTANTS, LIQUID PHASE. |
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| 123 | C --------------------------------------------- |
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| 124 | C |
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[393] | 125 | RCW=RCPV |
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[2] | 126 | WRITE(UNIT=6,FMT='('' *** Thermodynamic, liquid ***'')') |
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| 127 | WRITE(UNIT=6,FMT='('' Cw = '',E13.7)') RCW |
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| 128 | C |
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| 129 | C ---------------------------------------------------------------- |
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| 130 | C |
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| 131 | C* 7. DEFINE THERMODYNAMIC CONSTANTS, SOLID PHASE. |
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| 132 | C -------------------------------------------- |
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| 133 | C |
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[393] | 134 | RCS=RCPV |
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[2] | 135 | WRITE(UNIT=6,FMT='('' *** thermodynamic, solid ***'')') |
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| 136 | WRITE(UNIT=6,FMT='('' Cs = '',E13.7)') RCS |
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| 137 | C |
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| 138 | C ---------------------------------------------------------------- |
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| 139 | C |
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| 140 | C* 8. DEFINE THERMODYNAMIC CONSTANTS, TRANSITION OF PHASE. |
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| 141 | C ---------------------------------------------------- |
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| 142 | C |
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| 143 | RTT=273.16 |
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| 144 | RLVTT=2.5008E+6 |
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| 145 | RLSTT=2.8345E+6 |
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| 146 | RLMLT=RLSTT-RLVTT |
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| 147 | RATM=100000. |
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| 148 | WRITE(UNIT=6,FMT='('' *** Thermodynamic, trans. ***'')') |
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| 149 | WRITE(UNIT=6,FMT='('' Fusion point = '',E13.7)') RTT |
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| 150 | WRITE(UNIT=6,FMT='('' RLvTt = '',E13.7)') RLVTT |
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| 151 | WRITE(UNIT=6,FMT='('' RLsTt = '',E13.7)') RLSTT |
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| 152 | WRITE(UNIT=6,FMT='('' RLMlt = '',E13.7)') RLMLT |
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| 153 | WRITE(UNIT=6,FMT='('' Normal press. = '',E13.7)') RATM |
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| 154 | WRITE(UNIT=6,FMT='('' Latent heat : '')') |
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| 155 | C |
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| 156 | C ---------------------------------------------------------------- |
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| 157 | C |
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| 158 | C* 9. SATURATED VAPOUR PRESSURE. |
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| 159 | C -------------------------- |
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| 160 | C |
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| 161 | RESTT=611.14 |
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| 162 | RGAMW=(RCW-RCPV)/RV |
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| 163 | RBETW=RLVTT/RV+RGAMW*RTT |
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| 164 | RALPW=LOG(RESTT)+RBETW/RTT+RGAMW*LOG(RTT) |
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| 165 | RGAMS=(RCS-RCPV)/RV |
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| 166 | RBETS=RLSTT/RV+RGAMS*RTT |
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| 167 | RALPS=LOG(RESTT)+RBETS/RTT+RGAMS*LOG(RTT) |
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| 168 | RGAMD=RGAMS-RGAMW |
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| 169 | RBETD=RBETS-RBETW |
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| 170 | RALPD=RALPS-RALPW |
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| 171 | C |
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| 172 | C ------------------------------------------------------------------ |
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| 173 | c |
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| 174 | c calculer les constantes pour les fonctions thermodynamiques |
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| 175 | c |
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| 176 | RVTMP2=RCPV/RCPD-1. |
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| 177 | RHOH2O=RATM/100. |
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| 178 | R2ES=RESTT*RD/RV |
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| 179 | R3LES=17.269 |
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| 180 | R3IES=21.875 |
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| 181 | R4LES=35.86 |
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| 182 | R4IES=7.66 |
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| 183 | R5LES=R3LES*(RTT-R4LES) |
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| 184 | R5IES=R3IES*(RTT-R4IES) |
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| 185 | C |
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| 186 | RETURN |
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| 187 | END |
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