| 1 | ! |
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| 2 | ! $Header: /home/cvsroot/LMDZ4/libf/phylmd/diagphy.F,v 1.1.1.1 2004/05/19 12:53:08 lmdzadmin Exp $ |
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| 3 | ! |
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| 4 | SUBROUTINE diagphy(airephy,tit,iprt |
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| 5 | $ , tops, topl, sols, soll, sens |
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| 6 | $ , evap, rain_fall, snow_fall, ts |
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| 7 | $ , d_etp_tot, d_qt_tot, d_ec_tot |
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| 8 | $ , fs_bound, fq_bound) |
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| 9 | C====================================================================== |
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| 10 | C |
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| 11 | C Purpose: |
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| 12 | C Compute the thermal flux and the watter mass flux at the atmosphere |
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| 13 | c boundaries. Print them and also the atmospheric enthalpy change and |
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| 14 | C the atmospheric mass change. |
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| 15 | C |
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| 16 | C Arguments: |
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| 17 | C airephy-------input-R- grid area |
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| 18 | C tit---------input-A15- Comment to be added in PRINT (CHARACTER*15) |
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| 19 | C iprt--------input-I- PRINT level ( <=0 : no PRINT) |
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| 20 | C tops(klon)--input-R- SW rad. at TOA (W/m2), positive up. |
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| 21 | C topl(klon)--input-R- LW rad. at TOA (W/m2), positive down |
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| 22 | C sols(klon)--input-R- Net SW flux above surface (W/m2), positive up |
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| 23 | C (i.e. -1 * flux absorbed by the surface) |
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| 24 | C soll(klon)--input-R- Net LW flux above surface (W/m2), positive up |
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| 25 | C (i.e. flux emited - flux absorbed by the surface) |
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| 26 | C sens(klon)--input-R- Sensible Flux at surface (W/m2), positive down |
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| 27 | C evap(klon)--input-R- Evaporation + sublimation watter vapour mass flux |
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| 28 | C (kg/m2/s), positive up |
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| 29 | C rain_fall(klon) |
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| 30 | C --input-R- Liquid watter mass flux (kg/m2/s), positive down |
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| 31 | C snow_fall(klon) |
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| 32 | C --input-R- Solid watter mass flux (kg/m2/s), positive down |
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| 33 | C ts(klon)----input-R- Surface temperature (K) |
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| 34 | C d_etp_tot---input-R- Heat flux equivalent to atmospheric enthalpy |
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| 35 | C change (W/m2) |
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| 36 | C d_qt_tot----input-R- Mass flux equivalent to atmospheric watter mass |
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| 37 | C change (kg/m2/s) |
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| 38 | C d_ec_tot----input-R- Flux equivalent to atmospheric cinetic energy |
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| 39 | C change (W/m2) |
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| 40 | C |
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| 41 | C fs_bound---output-R- Thermal flux at the atmosphere boundaries (W/m2) |
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| 42 | C fq_bound---output-R- Watter mass flux at the atmosphere boundaries (kg/m2/s) |
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| 43 | C |
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| 44 | C J.L. Dufresne, July 2002 |
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| 45 | C====================================================================== |
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| 46 | C |
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| 47 | implicit none |
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| 48 | |
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| 49 | #include "dimensions.h" |
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| 50 | #include "dimphy.h" |
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| 51 | #include "YOMCST.h" |
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| 52 | C |
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| 53 | C Input variables |
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| 54 | real airephy(klon) |
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| 55 | CHARACTER*15 tit |
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| 56 | INTEGER iprt |
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| 57 | real tops(klon),topl(klon),sols(klon),soll(klon) |
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| 58 | real sens(klon),evap(klon),rain_fall(klon),snow_fall(klon) |
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| 59 | REAL ts(klon) |
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| 60 | REAL d_etp_tot, d_qt_tot, d_ec_tot |
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| 61 | c Output variables |
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| 62 | REAL fs_bound, fq_bound |
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| 63 | C |
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| 64 | C Local variables |
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| 65 | real stops,stopl,ssols,ssoll |
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| 66 | real ssens,sfront,slat |
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| 67 | real airetot, zcpvap, zcwat, zcice |
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| 68 | REAL rain_fall_tot, snow_fall_tot, evap_tot |
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| 69 | C |
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| 70 | integer i |
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| 71 | C |
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| 72 | integer pas |
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| 73 | save pas |
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| 74 | data pas/0/ |
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| 75 | C |
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| 76 | pas=pas+1 |
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| 77 | stops=0. |
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| 78 | stopl=0. |
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| 79 | ssols=0. |
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| 80 | ssoll=0. |
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| 81 | ssens=0. |
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| 82 | sfront = 0. |
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| 83 | evap_tot = 0. |
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| 84 | rain_fall_tot = 0. |
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| 85 | snow_fall_tot = 0. |
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| 86 | airetot=0. |
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| 87 | C |
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| 88 | C Pour les chaleur specifiques de la vapeur d'eau, de l'eau et de |
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| 89 | C la glace, on travaille par difference a la chaleur specifique de l' |
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| 90 | c air sec. En effet, comme on travaille a niveau de pression donne, |
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| 91 | C toute variation de la masse d'un constituant est totalement |
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| 92 | c compense par une variation de masse d'air. |
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| 93 | C |
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| 94 | zcpvap=RCPV-RCPD |
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| 95 | zcwat=RCW-RCPD |
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| 96 | zcice=RCS-RCPD |
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| 97 | C |
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| 98 | do i=1,klon |
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| 99 | stops=stops+tops(i)*airephy(i) |
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| 100 | stopl=stopl+topl(i)*airephy(i) |
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| 101 | ssols=ssols+sols(i)*airephy(i) |
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| 102 | ssoll=ssoll+soll(i)*airephy(i) |
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| 103 | ssens=ssens+sens(i)*airephy(i) |
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| 104 | sfront = sfront |
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| 105 | $ + ( evap(i)*zcpvap-rain_fall(i)*zcwat-snow_fall(i)*zcice |
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| 106 | $ ) *ts(i) *airephy(i) |
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| 107 | evap_tot = evap_tot + evap(i)*airephy(i) |
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| 108 | rain_fall_tot = rain_fall_tot + rain_fall(i)*airephy(i) |
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| 109 | snow_fall_tot = snow_fall_tot + snow_fall(i)*airephy(i) |
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| 110 | airetot=airetot+airephy(i) |
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| 111 | enddo |
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| 112 | stops=stops/airetot |
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| 113 | stopl=stopl/airetot |
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| 114 | ssols=ssols/airetot |
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| 115 | ssoll=ssoll/airetot |
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| 116 | ssens=ssens/airetot |
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| 117 | sfront = sfront/airetot |
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| 118 | evap_tot = evap_tot /airetot |
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| 119 | rain_fall_tot = rain_fall_tot/airetot |
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| 120 | snow_fall_tot = snow_fall_tot/airetot |
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| 121 | C |
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| 122 | slat = RLVTT * rain_fall_tot + RLSTT * snow_fall_tot |
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| 123 | C Heat flux at atm. boundaries |
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| 124 | fs_bound = stops-stopl - (ssols+ssoll)+ssens+sfront |
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| 125 | $ + slat |
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| 126 | C Watter flux at atm. boundaries |
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| 127 | fq_bound = evap_tot - rain_fall_tot -snow_fall_tot |
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| 128 | C |
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| 129 | IF (iprt.ge.1) write(6,6666) |
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| 130 | $ tit, pas, fs_bound, d_etp_tot, fq_bound, d_qt_tot |
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| 131 | C |
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| 132 | IF (iprt.ge.1) write(6,6668) |
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| 133 | $ tit, pas, d_etp_tot+d_ec_tot-fs_bound, d_qt_tot-fq_bound |
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| 134 | C |
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| 135 | IF (iprt.ge.2) write(6,6667) |
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| 136 | $ tit, pas, stops,stopl,ssols,ssoll,ssens,slat,evap_tot |
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| 137 | $ ,rain_fall_tot+snow_fall_tot |
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| 138 | |
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| 139 | return |
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| 140 | |
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| 141 | 6666 format('Phys. Flux Budget ',a15,1i6,x,2(f10.2,x),2(1pE13.5)) |
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| 142 | 6667 format('Phys. Boundary Flux ',a15,1i6,x,6(f10.2,x),2(1pE13.5)) |
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| 143 | 6668 format('Phys. Total Budget ',a15,1i6,x,f10.2,2(1pE13.5)) |
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| 144 | |
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| 145 | end |
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| 146 | |
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| 147 | C====================================================================== |
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| 148 | SUBROUTINE diagetpq(airephy,tit,iprt,idiag,idiag2,dtime |
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| 149 | e ,t,q,ql,qs,u,v,paprs,pplay |
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| 150 | s , d_h_vcol, d_qt, d_qw, d_ql, d_qs, d_ec) |
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| 151 | C====================================================================== |
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| 152 | C |
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| 153 | C Purpose: |
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| 154 | C Calcul la difference d'enthalpie et de masse d'eau entre 2 appels, |
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| 155 | C et calcul le flux de chaleur et le flux d'eau necessaire a ces |
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| 156 | C changements. Ces valeurs sont moyennees sur la surface de tout |
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| 157 | C le globe et sont exprime en W/2 et kg/s/m2 |
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| 158 | C Outil pour diagnostiquer la conservation de l'energie |
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| 159 | C et de la masse dans la physique. Suppose que les niveau de |
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| 160 | c pression entre couche ne varie pas entre 2 appels. |
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| 161 | C |
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| 162 | C Plusieurs de ces diagnostics peuvent etre fait en parallele: les |
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| 163 | c bilans sont sauvegardes dans des tableaux indices. On parlera |
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| 164 | C "d'indice de diagnostic" |
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| 165 | c |
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| 166 | C |
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| 167 | c====================================================================== |
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| 168 | C Arguments: |
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| 169 | C airephy-------input-R- grid area |
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| 170 | C tit-----imput-A15- Comment added in PRINT (CHARACTER*15) |
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| 171 | C iprt----input-I- PRINT level ( <=1 : no PRINT) |
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| 172 | C idiag---input-I- indice dans lequel sera range les nouveaux |
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| 173 | C bilans d' entalpie et de masse |
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| 174 | C idiag2--input-I-les nouveaux bilans d'entalpie et de masse |
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| 175 | C sont compare au bilan de d'enthalpie de masse de |
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| 176 | C l'indice numero idiag2 |
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| 177 | C Cas parriculier : si idiag2=0, pas de comparaison, on |
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| 178 | c sort directement les bilans d'enthalpie et de masse |
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| 179 | C dtime----input-R- time step (s) |
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| 180 | c t--------input-R- temperature (K) |
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| 181 | c q--------input-R- vapeur d'eau (kg/kg) |
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| 182 | c ql-------input-R- liquid watter (kg/kg) |
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| 183 | c qs-------input-R- solid watter (kg/kg) |
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| 184 | c u--------input-R- vitesse u |
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| 185 | c v--------input-R- vitesse v |
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| 186 | c paprs----input-R- pression a intercouche (Pa) |
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| 187 | c pplay----input-R- pression au milieu de couche (Pa) |
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| 188 | c |
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| 189 | C the following total value are computed by UNIT of earth surface |
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| 190 | C |
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| 191 | C d_h_vcol--output-R- Heat flux (W/m2) define as the Enthalpy |
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| 192 | c change (J/m2) during one time step (dtime) for the whole |
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| 193 | C atmosphere (air, watter vapour, liquid and solid) |
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| 194 | C d_qt------output-R- total water mass flux (kg/m2/s) defined as the |
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| 195 | C total watter (kg/m2) change during one time step (dtime), |
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| 196 | C d_qw------output-R- same, for the watter vapour only (kg/m2/s) |
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| 197 | C d_ql------output-R- same, for the liquid watter only (kg/m2/s) |
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| 198 | C d_qs------output-R- same, for the solid watter only (kg/m2/s) |
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| 199 | C d_ec------output-R- Cinetic Energy Budget (W/m2) for vertical air column |
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| 200 | C |
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| 201 | C other (COMMON...) |
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| 202 | C RCPD, RCPV, .... |
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| 203 | C |
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| 204 | C J.L. Dufresne, July 2002 |
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| 205 | c====================================================================== |
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| 206 | |
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| 207 | IMPLICIT NONE |
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| 208 | C |
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| 209 | #include "dimensions.h" |
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| 210 | #include "dimphy.h" |
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| 211 | #include "YOMCST.h" |
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| 212 | C |
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| 213 | c Input variables |
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| 214 | real airephy(klon) |
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| 215 | CHARACTER*15 tit |
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| 216 | INTEGER iprt,idiag, idiag2 |
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| 217 | REAL dtime |
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| 218 | REAL t(klon,klev), q(klon,klev), ql(klon,klev), qs(klon,klev) |
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| 219 | REAL u(klon,klev), v(klon,klev) |
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| 220 | REAL paprs(klon,klev+1), pplay(klon,klev) |
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| 221 | c Output variables |
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| 222 | REAL d_h_vcol, d_qt, d_qw, d_ql, d_qs, d_ec |
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| 223 | C |
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| 224 | C Local variables |
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| 225 | c |
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| 226 | REAL h_vcol_tot, h_dair_tot, h_qw_tot, h_ql_tot |
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| 227 | . , h_qs_tot, qw_tot, ql_tot, qs_tot , ec_tot |
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| 228 | c h_vcol_tot-- total enthalpy of vertical air column |
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| 229 | C (air with watter vapour, liquid and solid) (J/m2) |
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| 230 | c h_dair_tot-- total enthalpy of dry air (J/m2) |
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| 231 | c h_qw_tot---- total enthalpy of watter vapour (J/m2) |
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| 232 | c h_ql_tot---- total enthalpy of liquid watter (J/m2) |
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| 233 | c h_qs_tot---- total enthalpy of solid watter (J/m2) |
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| 234 | c qw_tot------ total mass of watter vapour (kg/m2) |
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| 235 | c ql_tot------ total mass of liquid watter (kg/m2) |
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| 236 | c qs_tot------ total mass of solid watter (kg/m2) |
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| 237 | c ec_tot------ total cinetic energy (kg/m2) |
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| 238 | C |
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| 239 | REAL zairm(klon,klev) ! layer air mass (kg/m2) |
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| 240 | REAL zqw_col(klon) |
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| 241 | REAL zql_col(klon) |
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| 242 | REAL zqs_col(klon) |
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| 243 | REAL zec_col(klon) |
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| 244 | REAL zh_dair_col(klon) |
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| 245 | REAL zh_qw_col(klon), zh_ql_col(klon), zh_qs_col(klon) |
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| 246 | C |
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| 247 | REAL d_h_dair, d_h_qw, d_h_ql, d_h_qs |
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| 248 | C |
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| 249 | REAL airetot, zcpvap, zcwat, zcice |
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| 250 | C |
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| 251 | INTEGER i, k |
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| 252 | C |
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| 253 | INTEGER ndiag ! max number of diagnostic in parallel |
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| 254 | PARAMETER (ndiag=10) |
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| 255 | integer pas(ndiag) |
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| 256 | save pas |
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| 257 | data pas/ndiag*0/ |
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| 258 | C |
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| 259 | REAL h_vcol_pre(ndiag), h_dair_pre(ndiag), h_qw_pre(ndiag) |
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| 260 | $ , h_ql_pre(ndiag), h_qs_pre(ndiag), qw_pre(ndiag) |
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| 261 | $ , ql_pre(ndiag), qs_pre(ndiag) , ec_pre(ndiag) |
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| 262 | SAVE h_vcol_pre, h_dair_pre, h_qw_pre, h_ql_pre |
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| 263 | $ , h_qs_pre, qw_pre, ql_pre, qs_pre , ec_pre |
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| 264 | |
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| 265 | c====================================================================== |
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| 266 | C |
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| 267 | DO k = 1, klev |
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| 268 | DO i = 1, klon |
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| 269 | C layer air mass |
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| 270 | zairm(i,k) = (paprs(i,k)-paprs(i,k+1))/RG |
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| 271 | ENDDO |
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| 272 | END DO |
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| 273 | C |
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| 274 | C Reset variables |
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| 275 | DO i = 1, klon |
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| 276 | zqw_col(i)=0. |
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| 277 | zql_col(i)=0. |
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| 278 | zqs_col(i)=0. |
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| 279 | zec_col(i) = 0. |
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| 280 | zh_dair_col(i) = 0. |
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| 281 | zh_qw_col(i) = 0. |
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| 282 | zh_ql_col(i) = 0. |
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| 283 | zh_qs_col(i) = 0. |
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| 284 | ENDDO |
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| 285 | C |
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| 286 | zcpvap=RCPV |
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| 287 | zcwat=RCW |
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| 288 | zcice=RCS |
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| 289 | C |
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| 290 | C Compute vertical sum for each atmospheric column |
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| 291 | C ================================================ |
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| 292 | DO k = 1, klev |
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| 293 | DO i = 1, klon |
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| 294 | C Watter mass |
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| 295 | zqw_col(i) = zqw_col(i) + q(i,k)*zairm(i,k) |
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| 296 | zql_col(i) = zql_col(i) + ql(i,k)*zairm(i,k) |
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| 297 | zqs_col(i) = zqs_col(i) + qs(i,k)*zairm(i,k) |
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| 298 | C Cinetic Energy |
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| 299 | zec_col(i) = zec_col(i) |
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| 300 | $ +0.5*(u(i,k)**2+v(i,k)**2)*zairm(i,k) |
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| 301 | C Air enthalpy |
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| 302 | ! ADAPTATION GCM POUR CP(T) |
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| 303 | zh_dair_col(i) = zh_dair_col(i) |
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| 304 | $ + cpdet(t(i,k))*(1.-q(i,k)-ql(i,k)-qs(i,k))*zairm(i,k)*t(i,k) |
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| 305 | zh_qw_col(i) = zh_qw_col(i) |
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| 306 | $ + zcpvap*q(i,k)*zairm(i,k)*t(i,k) |
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| 307 | zh_ql_col(i) = zh_ql_col(i) |
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| 308 | $ + zcwat*ql(i,k)*zairm(i,k)*t(i,k) |
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| 309 | $ - RLVTT*ql(i,k)*zairm(i,k) |
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| 310 | zh_qs_col(i) = zh_qs_col(i) |
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| 311 | $ + zcice*qs(i,k)*zairm(i,k)*t(i,k) |
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| 312 | $ - RLSTT*qs(i,k)*zairm(i,k) |
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| 313 | END DO |
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| 314 | ENDDO |
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| 315 | C |
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| 316 | C Mean over the planete surface |
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| 317 | C ============================= |
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| 318 | qw_tot = 0. |
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| 319 | ql_tot = 0. |
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| 320 | qs_tot = 0. |
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| 321 | ec_tot = 0. |
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| 322 | h_vcol_tot = 0. |
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| 323 | h_dair_tot = 0. |
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| 324 | h_qw_tot = 0. |
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| 325 | h_ql_tot = 0. |
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| 326 | h_qs_tot = 0. |
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| 327 | airetot=0. |
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| 328 | C |
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| 329 | do i=1,klon |
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| 330 | qw_tot = qw_tot + zqw_col(i)*airephy(i) |
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| 331 | ql_tot = ql_tot + zql_col(i)*airephy(i) |
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| 332 | qs_tot = qs_tot + zqs_col(i)*airephy(i) |
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| 333 | ec_tot = ec_tot + zec_col(i)*airephy(i) |
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| 334 | h_dair_tot = h_dair_tot + zh_dair_col(i)*airephy(i) |
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| 335 | h_qw_tot = h_qw_tot + zh_qw_col(i)*airephy(i) |
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| 336 | h_ql_tot = h_ql_tot + zh_ql_col(i)*airephy(i) |
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| 337 | h_qs_tot = h_qs_tot + zh_qs_col(i)*airephy(i) |
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| 338 | airetot=airetot+airephy(i) |
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| 339 | END DO |
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| 340 | C |
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| 341 | qw_tot = qw_tot/airetot |
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| 342 | ql_tot = ql_tot/airetot |
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| 343 | qs_tot = qs_tot/airetot |
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| 344 | ec_tot = ec_tot/airetot |
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| 345 | h_dair_tot = h_dair_tot/airetot |
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| 346 | h_qw_tot = h_qw_tot/airetot |
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| 347 | h_ql_tot = h_ql_tot/airetot |
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| 348 | h_qs_tot = h_qs_tot/airetot |
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| 349 | C |
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| 350 | h_vcol_tot = h_dair_tot+h_qw_tot+h_ql_tot+h_qs_tot |
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| 351 | c print*,'airetot=',airetot,' h_dair_tot=',h_dair_tot |
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| 352 | C |
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| 353 | C Compute the change of the atmospheric state compare to the one |
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| 354 | C stored in "idiag2", and convert it in flux. THis computation |
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| 355 | C is performed IF idiag2 /= 0 and IF it is not the first CALL |
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| 356 | c for "idiag" |
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| 357 | C =================================== |
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| 358 | C |
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| 359 | IF ( (idiag2.gt.0) .and. (pas(idiag2) .ne. 0) ) THEN |
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| 360 | d_h_vcol = (h_vcol_tot - h_vcol_pre(idiag2) )/dtime |
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| 361 | d_h_dair = (h_dair_tot- h_dair_pre(idiag2))/dtime |
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| 362 | d_h_qw = (h_qw_tot - h_qw_pre(idiag2) )/dtime |
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| 363 | d_h_ql = (h_ql_tot - h_ql_pre(idiag2) )/dtime |
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| 364 | d_h_qs = (h_qs_tot - h_qs_pre(idiag2) )/dtime |
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| 365 | d_qw = (qw_tot - qw_pre(idiag2) )/dtime |
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| 366 | d_ql = (ql_tot - ql_pre(idiag2) )/dtime |
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| 367 | d_qs = (qs_tot - qs_pre(idiag2) )/dtime |
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| 368 | d_ec = (ec_tot - ec_pre(idiag2) )/dtime |
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| 369 | d_qt = d_qw + d_ql + d_qs |
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| 370 | ELSE |
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| 371 | d_h_vcol = 0. |
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| 372 | d_h_dair = 0. |
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| 373 | d_h_qw = 0. |
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| 374 | d_h_ql = 0. |
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| 375 | d_h_qs = 0. |
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| 376 | d_qw = 0. |
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| 377 | d_ql = 0. |
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| 378 | d_qs = 0. |
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| 379 | d_ec = 0. |
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| 380 | d_qt = 0. |
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| 381 | ENDIF |
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| 382 | C |
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| 383 | IF (iprt.ge.2) THEN |
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| 384 | WRITE(6,9000) tit,pas(idiag),d_qt,d_qw,d_ql,d_qs |
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| 385 | 9000 format('Phys. Watter Mass Budget (kg/m2/s)',A15 |
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| 386 | $ ,1i6,10(1pE14.6)) |
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| 387 | WRITE(6,9001) tit,pas(idiag), d_h_vcol, h_vcol_tot/dtime |
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| 388 | 9001 format('Phys. Enthalpy Budget (W/m2) ',A15,1i6,10(E14.6,x)) |
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| 389 | WRITE(6,9002) tit,pas(idiag), d_ec |
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| 390 | 9002 format('Phys. Cinetic Energy Budget (W/m2) ',A15,1i6,10(F10.2)) |
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| 391 | END IF |
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| 392 | C |
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| 393 | C Store the new atmospheric state in "idiag" |
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| 394 | C |
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| 395 | pas(idiag)=pas(idiag)+1 |
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| 396 | h_vcol_pre(idiag) = h_vcol_tot |
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| 397 | h_dair_pre(idiag) = h_dair_tot |
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| 398 | h_qw_pre(idiag) = h_qw_tot |
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| 399 | h_ql_pre(idiag) = h_ql_tot |
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| 400 | h_qs_pre(idiag) = h_qs_tot |
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| 401 | qw_pre(idiag) = qw_tot |
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| 402 | ql_pre(idiag) = ql_tot |
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| 403 | qs_pre(idiag) = qs_tot |
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| 404 | ec_pre (idiag) = ec_tot |
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| 405 | C |
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| 406 | RETURN |
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| 407 | END |
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