1 | SUBROUTINE GFLUXI(NLL,TLEV,NW,DW,DTAU,TAUCUM,W0,COSBAR,UBARI, |
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2 | * RSF,BTOP,BSURF,FTOPUP,FMIDP,FMIDM) |
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3 | |
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4 | C THIS SUBROUTINE TAKES THE OPTICAL CONSTANTS AND BOUNDARY CONDITIONS |
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5 | C FOR THE INFRARED FLUX AT ONE WAVELENGTH AND SOLVES FOR THE FLUXES AT |
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6 | C THE LEVELS. THIS VERSION IS SET UP TO WORK WITH LAYER OPTICAL DEPTHS |
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7 | C MEASURED FROM THE TOP OF EACH LAYER. THE TOP OF EACH LAYER HAS |
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8 | C OPTICAL DEPTH ZERO. IN THIS SUB LEVEL N IS ABOVE LAYER N. THAT IS LAYER N |
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9 | C HAS LEVEL N ON TOP AND LEVEL N+1 ON BOTTOM. OPTICAL DEPTH INCREASES |
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10 | C FROM TOP TO BOTTOM. SEE C.P. MCKAY, TGM NOTES. |
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11 | C THE TRI-DIAGONAL MATRIX SOLVER IS DSOLVER AND IS DOUBLE PRECISION SO MANY |
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12 | C VARIABLES ARE PASSED AS SINGLE THEN BECOME DOUBLE IN DSOLVER |
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13 | C |
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14 | C NLL = NUMBER OF LEVELS (NLAYERS + 1) MUST BE LESS THAT NL (101) |
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15 | C TLEV(L_LEVELS) = ARRAY OF TEMPERATURES AT GCM LEVELS |
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16 | C WAVEN = WAVELENGTH FOR THE COMPUTATION |
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17 | C DW = WAVENUMBER INTERVAL |
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18 | C DTAU(NLAYER) = ARRAY OPTICAL DEPTH OF THE LAYERS |
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19 | C W0(NLEVEL) = SINGLE SCATTERING ALBEDO |
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20 | C COSBAR(NLEVEL) = ASYMMETRY FACTORS, 0=ISOTROPIC |
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21 | C UBARI = AVERAGE ANGLE, MUST BE EQUAL TO 0.5 IN IR |
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22 | C RSF = SURFACE REFLECTANCE |
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23 | C BTOP = UPPER BOUNDARY CONDITION ON IR INTENSITY (NOT FLUX) |
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24 | C BSURF = SURFACE EMISSION = (1-RSFI)*PLANCK, INTENSITY (NOT FLUX) |
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25 | C FP(NLEVEL) = UPWARD FLUX AT LEVELS |
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26 | C FM(NLEVEL) = DOWNWARD FLUX AT LEVELS |
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27 | C FMIDP(NLAYER) = UPWARD FLUX AT LAYER MIDPOINTS |
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28 | C FMIDM(NLAYER) = DOWNWARD FLUX AT LAYER MIDPOINTS |
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29 | C |
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30 | C----------------------------------------------------------------------C |
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31 | |
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32 | use radinc_h |
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33 | use radcommon_h, only: planckir |
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34 | |
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35 | implicit none |
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36 | |
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37 | #include "comcstfi.h" |
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38 | |
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39 | INTEGER NLP |
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40 | PARAMETER (NLP=101) ! MUST BE LARGER THAN NLEVEL |
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41 | |
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42 | INTEGER NLL, NLAYER, L, NW, NT, NT2 |
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43 | REAL*8 TERM, CPMID, CMMID |
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44 | REAL*8 PLANCK |
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45 | REAL*8 EM,EP |
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46 | REAL*8 COSBAR(L_NLAYRAD), W0(L_NLAYRAD), DTAU(L_NLAYRAD) |
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47 | REAL*8 TAUCUM(L_LEVELS), DTAUK |
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48 | REAL*8 TLEV(L_LEVELS) |
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49 | REAL*8 WAVEN, DW, UBARI, RSF |
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50 | REAL*8 BTOP, BSURF, FMIDP(L_NLAYRAD), FMIDM(L_NLAYRAD) |
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51 | REAL*8 B0(NLP),B1(NLP),ALPHA(NLP),LAMDA(NLP),XK1(NLP),XK2(NLP) |
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52 | REAL*8 GAMA(NLP),CP(NLP),CM(NLP),CPM1(NLP),CMM1(NLP),E1(NLP) |
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53 | REAL*8 E2(NLP),E3(NLP),E4(NLP) |
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54 | |
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55 | REAL*8 FTOPUP, FLUXUP, FLUXDN |
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56 | |
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57 | real*8 :: TAUMAX = L_TAUMAX |
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58 | |
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59 | C======================================================================C |
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60 | |
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61 | C WE GO WITH THE HEMISPHERIC CONSTANT APPROACH IN THE INFRARED |
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62 | |
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63 | |
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64 | IF (NLL .GT. NLP) STOP 'PARAMETER NL TOO SMALL IN GFLUXI' |
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65 | |
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66 | NLAYER = L_NLAYRAD |
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67 | |
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68 | DO L=1,L_NLAYRAD-1 |
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69 | |
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70 | !---------------------------------------------------- |
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71 | ! There is a problem when W0 = 1 |
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72 | ! open(888,file='W0') |
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73 | ! if ((W0(L).eq.0.).or.(W0(L).eq.1.)) then |
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74 | ! write(888,*) W0(L), L, 'gfluxi' |
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75 | ! endif |
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76 | ! Prevent this with an if statement: |
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77 | if (W0(L).eq.1.D0) then |
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78 | W0(L) = 0.99999D0 |
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79 | endif |
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80 | !---------------------------------------------------- |
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81 | |
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82 | ALPHA(L) = SQRT( (1.0D0-W0(L))/(1.0D0-W0(L)*COSBAR(L)) ) |
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83 | LAMDA(L) = ALPHA(L)*(1.0D0-W0(L)*COSBAR(L))/UBARI |
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84 | |
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85 | NT = int(TLEV(2*L)*NTfac) - NTstar+1 |
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86 | NT2 = int(TLEV(2*L+2)*NTfac) - NTstar+1 |
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87 | |
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88 | B1(L) = (PLANCKIR(NW,NT2)-PLANCKIR(NW,NT))/DTAU(L) |
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89 | B0(L) = PLANCKIR(NW,NT) |
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90 | END DO |
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91 | |
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92 | C Take care of special lower layer |
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93 | |
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94 | L = L_NLAYRAD |
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95 | |
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96 | if (W0(L).eq.1.) then |
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97 | W0(L) = 0.99999D0 |
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98 | end if |
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99 | |
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100 | ALPHA(L) = SQRT( (1.0D0-W0(L))/(1.0D0-W0(L)*COSBAR(L)) ) |
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101 | LAMDA(L) = ALPHA(L)*(1.0D0-W0(L)*COSBAR(L))/UBARI |
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102 | |
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103 | ! Tsurf is used for 1st layer source function |
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104 | ! -- same results for most thin atmospheres |
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105 | ! -- and stabilizes integrations |
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106 | NT = int(TLEV(2*L+1)*NTfac) - NTstar+1 |
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107 | !! For deep, opaque, thick first layers (e.g. Saturn) |
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108 | !! what is below works much better, not unstable, ... |
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109 | !! ... and actually fully accurate because 1st layer temp (JL) |
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110 | !NT = int(TLEV(2*L)*NTfac) - NTstar+1 |
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111 | !! (or this one yields same results |
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112 | !NT = int( (TLEV(2*L)+TLEV(2*L+1))*0.5*NTfac ) - NTstar+1 |
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113 | |
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114 | NT2 = int(TLEV(2*L)*NTfac) - NTstar+1 |
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115 | B1(L) = (PLANCKIR(NW,NT)-PLANCKIR(NW,NT2))/DTAU(L) |
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116 | B0(L) = PLANCKIR(NW,NT2) |
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117 | |
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118 | DO L=1,L_NLAYRAD |
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119 | GAMA(L) = (1.0D0-ALPHA(L))/(1.0D0+ALPHA(L)) |
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120 | TERM = UBARI/(1.0D0-W0(L)*COSBAR(L)) |
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121 | |
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122 | C CP AND CM ARE THE CPLUS AND CMINUS TERMS EVALUATED AT THE |
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123 | C BOTTOM OF THE LAYER. THAT IS AT DTAU OPTICAL DEPTH |
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124 | |
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125 | CP(L) = B0(L)+B1(L)*DTAU(L) +B1(L)*TERM |
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126 | CM(L) = B0(L)+B1(L)*DTAU(L) -B1(L)*TERM |
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127 | |
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128 | C CPM1 AND CMM1 ARE THE CPLUS AND CMINUS TERMS EVALUATED |
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129 | C AT THE TOP OF THE LAYER, THAT IS ZERO OPTICAL DEPTH |
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130 | |
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131 | CPM1(L) = B0(L)+B1(L)*TERM |
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132 | CMM1(L) = B0(L)-B1(L)*TERM |
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133 | END DO |
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134 | |
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135 | C NOW CALCULATE THE EXPONENTIAL TERMS NEEDED |
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136 | C FOR THE TRIDIAGONAL ROTATED LAYERED METHOD |
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137 | C WARNING IF DTAU(J) IS GREATER THAN ABOUT 35 (VAX) |
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138 | C WE CLIP IT TO AVOID OVERFLOW. |
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139 | |
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140 | DO L=1,L_NLAYRAD |
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141 | |
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142 | C CLIP THE EXPONENTIAL HERE. |
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143 | |
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144 | EP = EXP( MIN((LAMDA(L)*DTAU(L)),TAUMAX)) |
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145 | EM = 1.0D0/EP |
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146 | E1(L) = EP+GAMA(L)*EM |
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147 | E2(L) = EP-GAMA(L)*EM |
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148 | E3(L) = GAMA(L)*EP+EM |
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149 | E4(L) = GAMA(L)*EP-EM |
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150 | END DO |
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151 | |
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152 | c B81=BTOP ! RENAME BEFORE CALLING DSOLVER - used to be to set |
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153 | c B82=BSURF ! them to real*8 - but now everything is real*8 |
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154 | c R81=RSF ! so this may not be necessary |
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155 | |
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156 | C Double precision tridiagonal solver |
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157 | |
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158 | CALL DSOLVER(NLAYER,GAMA,CP,CM,CPM1,CMM1,E1,E2,E3,E4,BTOP, |
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159 | * BSURF,RSF,XK1,XK2) |
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160 | |
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161 | |
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162 | C NOW WE CALCULATE THE FLUXES AT THE MIDPOINTS OF THE LAYERS. |
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163 | |
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164 | DO L=1,L_NLAYRAD-1 |
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165 | DTAUK = TAUCUM(2*L+1)-TAUCUM(2*L) |
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166 | EP = EXP(MIN(LAMDA(L)*DTAUK,TAUMAX)) ! CLIPPED EXPONENTIAL |
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167 | EM = 1.0D0/EP |
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168 | TERM = UBARI/(1.D0-W0(L)*COSBAR(L)) |
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169 | |
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170 | C CP AND CM ARE THE CPLUS AND CMINUS TERMS EVALUATED AT THE |
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171 | C BOTTOM OF THE LAYER. THAT IS AT DTAU OPTICAL DEPTH |
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172 | |
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173 | CPMID = B0(L)+B1(L)*DTAUK +B1(L)*TERM |
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174 | CMMID = B0(L)+B1(L)*DTAUK -B1(L)*TERM |
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175 | FMIDP(L) = XK1(L)*EP + GAMA(L)*XK2(L)*EM + CPMID |
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176 | FMIDM(L) = XK1(L)*EP*GAMA(L) + XK2(L)*EM + CMMID |
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177 | |
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178 | C FOR FLUX WE INTEGRATE OVER THE HEMISPHERE TREATING INTENSITY CONSTANT |
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179 | |
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180 | FMIDP(L) = FMIDP(L)*PI |
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181 | FMIDM(L) = FMIDM(L)*PI |
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182 | END DO |
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183 | |
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184 | C And now, for the special bottom layer |
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185 | |
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186 | L = L_NLAYRAD |
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187 | |
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188 | EP = EXP(MIN((LAMDA(L)*DTAU(L)),TAUMAX)) ! CLIPPED EXPONENTIAL |
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189 | EM = 1.0D0/EP |
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190 | TERM = UBARI/(1.D0-W0(L)*COSBAR(L)) |
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191 | |
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192 | C CP AND CM ARE THE CPLUS AND CMINUS TERMS EVALUATED AT THE |
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193 | C BOTTOM OF THE LAYER. THAT IS AT DTAU OPTICAL DEPTH |
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194 | |
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195 | CPMID = B0(L)+B1(L)*DTAU(L) +B1(L)*TERM |
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196 | CMMID = B0(L)+B1(L)*DTAU(L) -B1(L)*TERM |
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197 | FMIDP(L) = XK1(L)*EP + GAMA(L)*XK2(L)*EM + CPMID |
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198 | FMIDM(L) = XK1(L)*EP*GAMA(L) + XK2(L)*EM + CMMID |
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199 | |
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200 | C FOR FLUX WE INTEGRATE OVER THE HEMISPHERE TREATING INTENSITY CONSTANT |
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201 | |
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202 | FMIDP(L) = FMIDP(L)*PI |
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203 | FMIDM(L) = FMIDM(L)*PI |
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204 | |
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205 | C FLUX AT THE PTOP LEVEL |
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206 | |
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207 | EP = 1.0D0 |
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208 | EM = 1.0D0 |
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209 | TERM = UBARI/(1.0D0-W0(1)*COSBAR(1)) |
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210 | |
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211 | C CP AND CM ARE THE CPLUS AND CMINUS TERMS EVALUATED AT THE |
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212 | C BOTTOM OF THE LAYER. THAT IS AT DTAU OPTICAL DEPTH |
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213 | |
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214 | CPMID = B0(1)+B1(1)*TERM |
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215 | CMMID = B0(1)-B1(1)*TERM |
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216 | |
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217 | FLUXUP = XK1(1)*EP + GAMA(1)*XK2(1)*EM + CPMID |
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218 | FLUXDN = XK1(1)*EP*GAMA(1) + XK2(1)*EM + CMMID |
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219 | |
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220 | C FOR FLUX WE INTEGRATE OVER THE HEMISPHERE TREATING INTENSITY CONSTANT |
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221 | |
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222 | FTOPUP = (FLUXUP-FLUXDN)*PI |
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223 | |
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224 | |
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225 | RETURN |
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226 | END |
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