| 1 | ! |
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| 2 | ! $Header$ |
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| 3 | ! |
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| 4 | SUBROUTINE advx(limit,dtx,pbaru,sm,s0, |
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| 5 | $ sx,sy,sz,lati,latf) |
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| 6 | IMPLICIT NONE |
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| 7 | |
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| 8 | CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC |
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| 9 | C C |
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| 10 | C first-order moments (FOM) advection of tracer in X direction C |
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| 11 | C C |
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| 12 | C Source : Pascal Simon (Meteo,CNRM) C |
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| 13 | C Adaptation : A.Armengaud (LGGE) juin 94 C |
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| 14 | C C |
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| 15 | C limit,dtx,pbaru,pbarv,sm,s0,sx,sy,sz C |
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| 16 | C sont des arguments d'entree pour le s-pg... C |
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| 17 | C C |
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| 18 | C sm,s0,sx,sy,sz C |
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| 19 | C sont les arguments de sortie pour le s-pg C |
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| 20 | C C |
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| 21 | CCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCCC |
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| 22 | C |
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| 23 | C parametres principaux du modele |
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| 24 | C |
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| 25 | !----------------------------------------------------------------------- |
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| 26 | ! INCLUDE 'dimensions.h' |
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| 27 | ! |
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| 28 | ! dimensions.h contient les dimensions du modele |
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| 29 | ! ndm est tel que iim=2**ndm |
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| 30 | !----------------------------------------------------------------------- |
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| 31 | |
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| 32 | INTEGER iim,jjm,llm,ndm |
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| 33 | |
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| 34 | PARAMETER (iim= 128,jjm=96,llm=64,ndm=1) |
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| 35 | |
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| 36 | !----------------------------------------------------------------------- |
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| 37 | ! |
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| 38 | ! $Header$ |
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| 39 | ! |
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| 40 | ! |
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| 41 | ! ATTENTION!!!!: ce fichier include est compatible format fixe/format libre |
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| 42 | ! veillez n'utiliser que des ! pour les commentaires |
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| 43 | ! et bien positionner les & des lignes de continuation |
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| 44 | ! (les placer en colonne 6 et en colonne 73) |
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| 45 | ! |
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| 46 | ! |
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| 47 | !----------------------------------------------------------------------- |
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| 48 | ! INCLUDE 'paramet.h' |
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| 49 | |
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| 50 | INTEGER iip1,iip2,iip3,jjp1,llmp1,llmp2,llmm1 |
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| 51 | INTEGER kftd,ip1jm,ip1jmp1,ip1jmi1,ijp1llm |
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| 52 | INTEGER ijmllm,mvar |
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| 53 | INTEGER jcfil,jcfllm |
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| 54 | |
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| 55 | PARAMETER( iip1= iim+1,iip2=iim+2,iip3=iim+3 & |
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| 56 | & ,jjp1=jjm+1-1/jjm) |
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| 57 | PARAMETER( llmp1 = llm+1, llmp2 = llm+2, llmm1 = llm-1 ) |
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| 58 | PARAMETER( kftd = iim/2 -ndm ) |
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| 59 | PARAMETER( ip1jm = iip1*jjm, ip1jmp1= iip1*jjp1 ) |
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| 60 | PARAMETER( ip1jmi1= ip1jm - iip1 ) |
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| 61 | PARAMETER( ijp1llm= ip1jmp1 * llm, ijmllm= ip1jm * llm ) |
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| 62 | PARAMETER( mvar= ip1jmp1*( 2*llm+1) + ijmllm ) |
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| 63 | PARAMETER( jcfil=jjm/2+5, jcfllm=jcfil*llm ) |
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| 64 | |
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| 65 | !----------------------------------------------------------------------- |
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| 66 | ! |
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| 67 | ! $Id: comconst.h 1437 2010-09-30 08:29:10Z emillour $ |
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| 68 | ! |
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| 69 | !----------------------------------------------------------------------- |
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| 70 | ! INCLUDE comconst.h |
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| 71 | |
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| 72 | COMMON/comconsti/im,jm,lllm,imp1,jmp1,lllmm1,lllmp1,lcl, & |
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| 73 | & iflag_top_bound,mode_top_bound |
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| 74 | COMMON/comconstr/dtvr,daysec, & |
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| 75 | & pi,dtphys,dtdiss,rad,r,kappa,cotot,unsim,g,omeg & |
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| 76 | & ,dissip_fac_mid,dissip_fac_up,dissip_deltaz,dissip_hdelta & |
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| 77 | & ,dissip_pupstart ,tau_top_bound, & |
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| 78 | & daylen,molmass, ihf |
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| 79 | COMMON/cpdetvenus/cpp,nu_venus,t0_venus |
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| 80 | |
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| 81 | INTEGER im,jm,lllm,imp1,jmp1,lllmm1,lllmp1,lcl |
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| 82 | REAL dtvr ! dynamical time step (in s) |
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| 83 | REAL daysec !length (in s) of a standard day |
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| 84 | REAL pi ! something like 3.14159.... |
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| 85 | REAL dtphys ! (s) time step for the physics |
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| 86 | REAL dtdiss ! (s) time step for the dissipation |
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| 87 | REAL rad ! (m) radius of the planet |
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| 88 | REAL r ! Reduced Gas constant r=R/mu |
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| 89 | ! with R=8.31.. J.K-1.mol-1, mu: mol mass of atmosphere (kg/mol) |
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| 90 | REAL cpp ! Cp |
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| 91 | REAL kappa ! kappa=R/Cp |
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| 92 | REAL cotot |
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| 93 | REAL unsim ! = 1./iim |
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| 94 | REAL g ! (m/s2) gravity |
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| 95 | REAL omeg ! (rad/s) rotation rate of the planet |
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| 96 | ! Dissipation factors, for Earth model: |
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| 97 | REAL dissip_factz,dissip_zref !dissip_deltaz |
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| 98 | ! Dissipation factors, for other planets: |
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| 99 | REAL dissip_fac_mid,dissip_fac_up,dissip_deltaz,dissip_hdelta |
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| 100 | REAL dissip_pupstart |
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| 101 | INTEGER iflag_top_bound,mode_top_bound |
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| 102 | REAL tau_top_bound |
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| 103 | REAL daylen ! length of solar day, in 'standard' day length |
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| 104 | REAL molmass ! (g/mol) molar mass of the atmosphere |
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| 105 | |
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| 106 | REAL nu_venus,t0_venus ! coeffs needed for Cp(T), Venus atmosphere |
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| 107 | REAL ihf ! (W/m2) intrinsic heat flux for giant planets |
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| 108 | |
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| 109 | |
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| 110 | !----------------------------------------------------------------------- |
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| 111 | ! |
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| 112 | ! $Id: comvert.h 1654 2012-09-24 15:07:18Z aslmd $ |
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| 113 | ! |
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| 114 | !----------------------------------------------------------------------- |
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| 115 | ! INCLUDE 'comvert.h' |
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| 116 | |
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| 117 | COMMON/comvertr/ap(llm+1),bp(llm+1),presnivs(llm),dpres(llm), & |
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| 118 | & pa,preff,nivsigs(llm),nivsig(llm+1), & |
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| 119 | & aps(llm),bps(llm),scaleheight,pseudoalt(llm) |
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| 120 | |
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| 121 | common/comverti/disvert_type, pressure_exner |
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| 122 | |
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| 123 | real ap ! hybrid pressure contribution at interlayers |
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| 124 | real bp ! hybrid sigma contribution at interlayer |
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| 125 | real presnivs ! (reference) pressure at mid-layers |
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| 126 | real dpres |
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| 127 | real pa ! reference pressure (Pa) at which hybrid coordinates |
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| 128 | ! become purely pressure |
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| 129 | real preff ! reference surface pressure (Pa) |
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| 130 | real nivsigs |
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| 131 | real nivsig |
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| 132 | real aps ! hybrid pressure contribution at mid-layers |
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| 133 | real bps ! hybrid sigma contribution at mid-layers |
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| 134 | real scaleheight ! atmospheric (reference) scale height (km) |
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| 135 | real pseudoalt ! pseudo-altitude of model levels (km), based on presnivs(), |
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| 136 | ! preff and scaleheight |
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| 137 | |
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| 138 | integer disvert_type ! type of vertical discretization: |
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| 139 | ! 1: Earth (default for planet_type==earth), |
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| 140 | ! automatic generation |
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| 141 | ! 2: Planets (default for planet_type!=earth), |
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| 142 | ! using 'z2sig.def' (or 'esasig.def) file |
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| 143 | |
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| 144 | logical pressure_exner |
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| 145 | ! compute pressure inside layers using Exner function, else use mean |
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| 146 | ! of pressure values at interfaces |
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| 147 | |
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| 148 | !----------------------------------------------------------------------- |
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| 149 | |
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| 150 | C Arguments : |
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| 151 | C ----------- |
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| 152 | C dtx : frequence fictive d'appel du transport |
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| 153 | C pbaru, pbarv : flux de masse en x et y en Pa.m2.s-1 |
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| 154 | |
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| 155 | INTEGER ntra |
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| 156 | PARAMETER (ntra = 1) |
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| 157 | |
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| 158 | C ATTENTION partout ou on trouve ntra, insertion de boucle |
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| 159 | C possible dans l'avenir. |
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| 160 | |
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| 161 | REAL dtx |
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| 162 | REAL pbaru ( iip1,jjp1,llm ) |
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| 163 | |
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| 164 | C moments: SM total mass in each grid box |
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| 165 | C S0 mass of tracer in each grid box |
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| 166 | C Si 1rst order moment in i direction |
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| 167 | C |
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| 168 | REAL SM(iip1,jjp1,llm),S0(iip1,jjp1,llm,ntra) |
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| 169 | REAL sx(iip1,jjp1,llm,ntra) |
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| 170 | $ ,sy(iip1,jjp1,llm,ntra) |
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| 171 | REAL sz(iip1,jjp1,llm,ntra) |
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| 172 | |
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| 173 | C Local : |
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| 174 | C ------- |
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| 175 | |
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| 176 | C mass fluxes across the boundaries (UGRI,VGRI,WGRI) |
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| 177 | C mass fluxes in kg |
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| 178 | C declaration : |
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| 179 | |
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| 180 | REAL UGRI(iip1,jjp1,llm) |
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| 181 | |
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| 182 | C Rem : VGRI et WGRI ne sont pas utilises dans |
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| 183 | C cette subroutine ( advection en x uniquement ) |
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| 184 | C |
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| 185 | C Ti are the moments for the current latitude and level |
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| 186 | C |
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| 187 | REAL TM(iim) |
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| 188 | REAL T0(iim,ntra),TX(iim,ntra) |
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| 189 | REAL TY(iim,ntra),TZ(iim,ntra) |
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| 190 | REAL TEMPTM ! just a temporary variable |
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| 191 | C |
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| 192 | C the moments F are similarly defined and used as temporary |
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| 193 | C storage for portions of the grid boxes in transit |
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| 194 | C |
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| 195 | REAL FM(iim) |
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| 196 | REAL F0(iim,ntra),FX(iim,ntra) |
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| 197 | REAL FY(iim,ntra),FZ(iim,ntra) |
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| 198 | C |
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| 199 | C work arrays |
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| 200 | C |
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| 201 | REAL ALF(iim),ALF1(iim),ALFQ(iim),ALF1Q(iim) |
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| 202 | C |
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| 203 | REAL SMNEW(iim),UEXT(iim) |
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| 204 | C |
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| 205 | REAL sqi,sqf |
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| 206 | |
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| 207 | LOGICAL LIMIT |
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| 208 | INTEGER NUM(jjp1),LONK,NUMK |
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| 209 | INTEGER lon,lati,latf,niv |
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| 210 | INTEGER i,i2,i3,j,jv,l,k,itrac |
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| 211 | |
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| 212 | lon = iim |
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| 213 | niv = llm |
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| 214 | |
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| 215 | C *** Test de passage d'arguments ****** |
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| 216 | |
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| 217 | |
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| 218 | C ------------------------------------- |
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| 219 | DO 300 j = 1,jjp1 |
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| 220 | NUM(j) = 1 |
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| 221 | 300 CONTINUE |
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| 222 | sqi = 0. |
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| 223 | sqf = 0. |
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| 224 | |
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| 225 | DO l = 1,llm |
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| 226 | DO j = 1,jjp1 |
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| 227 | DO i = 1,iim |
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| 228 | cIM 240305 sqi = sqi + S0(i,j,l,9) |
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| 229 | sqi = sqi + S0(i,j,l,ntra) |
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| 230 | ENDDO |
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| 231 | ENDDO |
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| 232 | ENDDO |
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| 233 | PRINT*,'-------- DIAG DANS ADVX - ENTREE ---------' |
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| 234 | PRINT*,'sqi=',sqi |
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| 235 | |
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| 236 | |
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| 237 | C Interface : adaptation nouveau modele |
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| 238 | C ------------------------------------- |
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| 239 | C |
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| 240 | C --------------------------------------------------------- |
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| 241 | C Conversion des flux de masses en kg/s |
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| 242 | C pbaru est en N/s d'ou : |
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| 243 | C ugri est en kg/s |
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| 244 | |
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| 245 | DO 500 l = 1,llm |
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| 246 | DO 500 j = 1,jjm+1 |
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| 247 | DO 500 i = 1,iip1 |
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| 248 | C ugri (i,j,llm+1-l) = pbaru (i,j,l) * ( dsig(l) / g ) |
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| 249 | ugri (i,j,llm+1-l) = pbaru (i,j,l) |
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| 250 | 500 CONTINUE |
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| 251 | |
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| 252 | |
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| 253 | C --------------------------------------------------------- |
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| 254 | C --------------------------------------------------------- |
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| 255 | C --------------------------------------------------------- |
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| 256 | |
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| 257 | C start here |
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| 258 | C |
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| 259 | C boucle principale sur les niveaux et les latitudes |
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| 260 | C |
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| 261 | DO 1 L=1,NIV |
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| 262 | DO 1 K=lati,latf |
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| 263 | C |
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| 264 | C initialisation |
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| 265 | C |
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| 266 | C program assumes periodic boundaries in X |
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| 267 | C |
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| 268 | DO 10 I=2,LON |
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| 269 | SMNEW(I)=SM(I,K,L)+(UGRI(I-1,K,L)-UGRI(I,K,L))*DTX |
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| 270 | 10 CONTINUE |
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| 271 | SMNEW(1)=SM(1,K,L)+(UGRI(LON,K,L)-UGRI(1,K,L))*DTX |
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| 272 | C |
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| 273 | C modifications for extended polar zones |
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| 274 | C |
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| 275 | NUMK=NUM(K) |
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| 276 | LONK=LON/NUMK |
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| 277 | C |
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| 278 | IF(NUMK.GT.1) THEN |
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| 279 | C |
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| 280 | DO 111 I=1,LON |
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| 281 | TM(I)=0. |
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| 282 | 111 CONTINUE |
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| 283 | DO 112 JV=1,NTRA |
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| 284 | DO 1120 I=1,LON |
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| 285 | T0(I,JV)=0. |
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| 286 | TX(I,JV)=0. |
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| 287 | TY(I,JV)=0. |
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| 288 | TZ(I,JV)=0. |
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| 289 | 1120 CONTINUE |
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| 290 | 112 CONTINUE |
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| 291 | C |
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| 292 | DO 11 I2=1,NUMK |
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| 293 | C |
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| 294 | DO 113 I=1,LONK |
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| 295 | I3=(I-1)*NUMK+I2 |
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| 296 | TM(I)=TM(I)+SM(I3,K,L) |
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| 297 | ALF(I)=SM(I3,K,L)/TM(I) |
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| 298 | ALF1(I)=1.-ALF(I) |
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| 299 | 113 CONTINUE |
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| 300 | C |
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| 301 | DO JV=1,NTRA |
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| 302 | DO I=1,LONK |
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| 303 | I3=(I-1)*NUMK+I2 |
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| 304 | TEMPTM=-ALF(I)*T0(I,JV)+ALF1(I) |
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| 305 | $ *S0(I3,K,L,JV) |
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| 306 | T0(I,JV)=T0(I,JV)+S0(I3,K,L,JV) |
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| 307 | TX(I,JV)=ALF(I) *sx(I3,K,L,JV)+ |
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| 308 | $ ALF1(I)*TX(I,JV) +3.*TEMPTM |
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| 309 | TY(I,JV)=TY(I,JV)+sy(I3,K,L,JV) |
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| 310 | TZ(I,JV)=TZ(I,JV)+sz(I3,K,L,JV) |
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| 311 | ENDDO |
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| 312 | ENDDO |
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| 313 | C |
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| 314 | 11 CONTINUE |
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| 315 | C |
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| 316 | ELSE |
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| 317 | C |
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| 318 | DO 115 I=1,LON |
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| 319 | TM(I)=SM(I,K,L) |
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| 320 | 115 CONTINUE |
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| 321 | DO 116 JV=1,NTRA |
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| 322 | DO 1160 I=1,LON |
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| 323 | T0(I,JV)=S0(I,K,L,JV) |
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| 324 | TX(I,JV)=sx(I,K,L,JV) |
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| 325 | TY(I,JV)=sy(I,K,L,JV) |
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| 326 | TZ(I,JV)=sz(I,K,L,JV) |
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| 327 | 1160 CONTINUE |
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| 328 | 116 CONTINUE |
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| 329 | C |
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| 330 | ENDIF |
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| 331 | C |
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| 332 | DO 117 I=1,LONK |
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| 333 | UEXT(I)=UGRI(I*NUMK,K,L) |
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| 334 | 117 CONTINUE |
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| 335 | C |
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| 336 | C place limits on appropriate moments before transport |
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| 337 | C (if flux-limiting is to be applied) |
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| 338 | C |
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| 339 | IF(.NOT.LIMIT) GO TO 13 |
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| 340 | C |
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| 341 | DO 12 JV=1,NTRA |
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| 342 | DO 120 I=1,LONK |
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| 343 | TX(I,JV)=SIGN(AMIN1(AMAX1(T0(I,JV),0.),ABS(TX(I,JV))),TX(I,JV)) |
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| 344 | 120 CONTINUE |
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| 345 | 12 CONTINUE |
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| 346 | C |
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| 347 | 13 CONTINUE |
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| 348 | C |
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| 349 | C calculate flux and moments between adjacent boxes |
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| 350 | C 1- create temporary moments/masses for partial boxes in transit |
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| 351 | C 2- reajusts moments remaining in the box |
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| 352 | C |
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| 353 | C flux from IP to I if U(I).lt.0 |
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| 354 | C |
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| 355 | DO 140 I=1,LONK-1 |
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| 356 | IF(UEXT(I).LT.0.) THEN |
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| 357 | FM(I)=-UEXT(I)*DTX |
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| 358 | ALF(I)=FM(I)/TM(I+1) |
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| 359 | TM(I+1)=TM(I+1)-FM(I) |
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| 360 | ENDIF |
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| 361 | 140 CONTINUE |
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| 362 | C |
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| 363 | I=LONK |
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| 364 | IF(UEXT(I).LT.0.) THEN |
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| 365 | FM(I)=-UEXT(I)*DTX |
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| 366 | ALF(I)=FM(I)/TM(1) |
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| 367 | TM(1)=TM(1)-FM(I) |
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| 368 | ENDIF |
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| 369 | C |
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| 370 | C flux from I to IP if U(I).gt.0 |
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| 371 | C |
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| 372 | DO 141 I=1,LONK |
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| 373 | IF(UEXT(I).GE.0.) THEN |
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| 374 | FM(I)=UEXT(I)*DTX |
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| 375 | ALF(I)=FM(I)/TM(I) |
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| 376 | TM(I)=TM(I)-FM(I) |
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| 377 | ENDIF |
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| 378 | 141 CONTINUE |
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| 379 | C |
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| 380 | DO 142 I=1,LONK |
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| 381 | ALFQ(I)=ALF(I)*ALF(I) |
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| 382 | ALF1(I)=1.-ALF(I) |
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| 383 | ALF1Q(I)=ALF1(I)*ALF1(I) |
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| 384 | 142 CONTINUE |
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| 385 | C |
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| 386 | DO 150 JV=1,NTRA |
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| 387 | DO 1500 I=1,LONK-1 |
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| 388 | C |
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| 389 | IF(UEXT(I).LT.0.) THEN |
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| 390 | C |
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| 391 | F0(I,JV)=ALF (I)* ( T0(I+1,JV)-ALF1(I)*TX(I+1,JV) ) |
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| 392 | FX(I,JV)=ALFQ(I)*TX(I+1,JV) |
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| 393 | FY(I,JV)=ALF (I)*TY(I+1,JV) |
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| 394 | FZ(I,JV)=ALF (I)*TZ(I+1,JV) |
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| 395 | C |
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| 396 | T0(I+1,JV)=T0(I+1,JV)-F0(I,JV) |
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| 397 | TX(I+1,JV)=ALF1Q(I)*TX(I+1,JV) |
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| 398 | TY(I+1,JV)=TY(I+1,JV)-FY(I,JV) |
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| 399 | TZ(I+1,JV)=TZ(I+1,JV)-FZ(I,JV) |
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| 400 | C |
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| 401 | ENDIF |
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| 402 | C |
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| 403 | 1500 CONTINUE |
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| 404 | 150 CONTINUE |
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| 405 | C |
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| 406 | I=LONK |
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| 407 | IF(UEXT(I).LT.0.) THEN |
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| 408 | C |
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| 409 | DO 151 JV=1,NTRA |
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| 410 | C |
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| 411 | F0 (I,JV)=ALF (I)* ( T0(1,JV)-ALF1(I)*TX(1,JV) ) |
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| 412 | FX (I,JV)=ALFQ(I)*TX(1,JV) |
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| 413 | FY (I,JV)=ALF (I)*TY(1,JV) |
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| 414 | FZ (I,JV)=ALF (I)*TZ(1,JV) |
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| 415 | C |
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| 416 | T0(1,JV)=T0(1,JV)-F0(I,JV) |
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| 417 | TX(1,JV)=ALF1Q(I)*TX(1,JV) |
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| 418 | TY(1,JV)=TY(1,JV)-FY(I,JV) |
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| 419 | TZ(1,JV)=TZ(1,JV)-FZ(I,JV) |
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| 420 | C |
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| 421 | 151 CONTINUE |
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| 422 | C |
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| 423 | ENDIF |
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| 424 | C |
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| 425 | DO 152 JV=1,NTRA |
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| 426 | DO 1520 I=1,LONK |
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| 427 | C |
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| 428 | IF(UEXT(I).GE.0.) THEN |
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| 429 | C |
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| 430 | F0(I,JV)=ALF (I)* ( T0(I,JV)+ALF1(I)*TX(I,JV) ) |
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| 431 | FX(I,JV)=ALFQ(I)*TX(I,JV) |
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| 432 | FY(I,JV)=ALF (I)*TY(I,JV) |
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| 433 | FZ(I,JV)=ALF (I)*TZ(I,JV) |
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| 434 | C |
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| 435 | T0(I,JV)=T0(I,JV)-F0(I,JV) |
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| 436 | TX(I,JV)=ALF1Q(I)*TX(I,JV) |
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| 437 | TY(I,JV)=TY(I,JV)-FY(I,JV) |
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| 438 | TZ(I,JV)=TZ(I,JV)-FZ(I,JV) |
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| 439 | C |
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| 440 | ENDIF |
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| 441 | C |
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| 442 | 1520 CONTINUE |
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| 443 | 152 CONTINUE |
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| 444 | C |
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| 445 | C puts the temporary moments Fi into appropriate neighboring boxes |
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| 446 | C |
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| 447 | DO 160 I=1,LONK |
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| 448 | IF(UEXT(I).LT.0.) THEN |
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| 449 | TM(I)=TM(I)+FM(I) |
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| 450 | ALF(I)=FM(I)/TM(I) |
|---|
| 451 | ENDIF |
|---|
| 452 | 160 CONTINUE |
|---|
| 453 | C |
|---|
| 454 | DO 161 I=1,LONK-1 |
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| 455 | IF(UEXT(I).GE.0.) THEN |
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| 456 | TM(I+1)=TM(I+1)+FM(I) |
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| 457 | ALF(I)=FM(I)/TM(I+1) |
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| 458 | ENDIF |
|---|
| 459 | 161 CONTINUE |
|---|
| 460 | C |
|---|
| 461 | I=LONK |
|---|
| 462 | IF(UEXT(I).GE.0.) THEN |
|---|
| 463 | TM(1)=TM(1)+FM(I) |
|---|
| 464 | ALF(I)=FM(I)/TM(1) |
|---|
| 465 | ENDIF |
|---|
| 466 | C |
|---|
| 467 | DO 162 I=1,LONK |
|---|
| 468 | ALF1(I)=1.-ALF(I) |
|---|
| 469 | 162 CONTINUE |
|---|
| 470 | C |
|---|
| 471 | DO 170 JV=1,NTRA |
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| 472 | DO 1700 I=1,LONK |
|---|
| 473 | C |
|---|
| 474 | IF(UEXT(I).LT.0.) THEN |
|---|
| 475 | C |
|---|
| 476 | TEMPTM=-ALF(I)*T0(I,JV)+ALF1(I)*F0(I,JV) |
|---|
| 477 | T0(I,JV)=T0(I,JV)+F0(I,JV) |
|---|
| 478 | TX(I,JV)=ALF(I)*FX(I,JV)+ALF1(I)*TX(I,JV)+3.*TEMPTM |
|---|
| 479 | TY(I,JV)=TY(I,JV)+FY(I,JV) |
|---|
| 480 | TZ(I,JV)=TZ(I,JV)+FZ(I,JV) |
|---|
| 481 | C |
|---|
| 482 | ENDIF |
|---|
| 483 | C |
|---|
| 484 | 1700 CONTINUE |
|---|
| 485 | 170 CONTINUE |
|---|
| 486 | C |
|---|
| 487 | DO 171 JV=1,NTRA |
|---|
| 488 | DO 1710 I=1,LONK-1 |
|---|
| 489 | C |
|---|
| 490 | IF(UEXT(I).GE.0.) THEN |
|---|
| 491 | C |
|---|
| 492 | TEMPTM=ALF(I)*T0(I+1,JV)-ALF1(I)*F0(I,JV) |
|---|
| 493 | T0(I+1,JV)=T0(I+1,JV)+F0(I,JV) |
|---|
| 494 | TX(I+1,JV)=ALF(I)*FX(I,JV)+ALF1(I)*TX(I+1,JV)+3.*TEMPTM |
|---|
| 495 | TY(I+1,JV)=TY(I+1,JV)+FY(I,JV) |
|---|
| 496 | TZ(I+1,JV)=TZ(I+1,JV)+FZ(I,JV) |
|---|
| 497 | C |
|---|
| 498 | ENDIF |
|---|
| 499 | C |
|---|
| 500 | 1710 CONTINUE |
|---|
| 501 | 171 CONTINUE |
|---|
| 502 | C |
|---|
| 503 | I=LONK |
|---|
| 504 | IF(UEXT(I).GE.0.) THEN |
|---|
| 505 | DO 172 JV=1,NTRA |
|---|
| 506 | TEMPTM=ALF(I)*T0(1,JV)-ALF1(I)*F0(I,JV) |
|---|
| 507 | T0(1,JV)=T0(1,JV)+F0(I,JV) |
|---|
| 508 | TX(1,JV)=ALF(I)*FX(I,JV)+ALF1(I)*TX(1,JV)+3.*TEMPTM |
|---|
| 509 | TY(1,JV)=TY(1,JV)+FY(I,JV) |
|---|
| 510 | TZ(1,JV)=TZ(1,JV)+FZ(I,JV) |
|---|
| 511 | 172 CONTINUE |
|---|
| 512 | ENDIF |
|---|
| 513 | C |
|---|
| 514 | C retour aux mailles d'origine (passage des Tij aux Sij) |
|---|
| 515 | C |
|---|
| 516 | IF(NUMK.GT.1) THEN |
|---|
| 517 | C |
|---|
| 518 | DO 180 I2=1,NUMK |
|---|
| 519 | C |
|---|
| 520 | DO 180 I=1,LONK |
|---|
| 521 | C |
|---|
| 522 | I3=I2+(I-1)*NUMK |
|---|
| 523 | SM(I3,K,L)=SMNEW(I3) |
|---|
| 524 | ALF(I)=SMNEW(I3)/TM(I) |
|---|
| 525 | TM(I)=TM(I)-SMNEW(I3) |
|---|
| 526 | C |
|---|
| 527 | ALFQ(I)=ALF(I)*ALF(I) |
|---|
| 528 | ALF1(I)=1.-ALF(I) |
|---|
| 529 | ALF1Q(I)=ALF1(I)*ALF1(I) |
|---|
| 530 | C |
|---|
| 531 | 180 CONTINUE |
|---|
| 532 | C |
|---|
| 533 | DO JV=1,NTRA |
|---|
| 534 | DO I=1,LONK |
|---|
| 535 | C |
|---|
| 536 | I3=I2+(I-1)*NUMK |
|---|
| 537 | S0(I3,K,L,JV)=ALF (I) |
|---|
| 538 | $ * (T0(I,JV)-ALF1(I)*TX(I,JV)) |
|---|
| 539 | sx(I3,K,L,JV)=ALFQ(I)*TX(I,JV) |
|---|
| 540 | sy(I3,K,L,JV)=ALF (I)*TY(I,JV) |
|---|
| 541 | sz(I3,K,L,JV)=ALF (I)*TZ(I,JV) |
|---|
| 542 | C |
|---|
| 543 | C reajusts moments remaining in the box |
|---|
| 544 | C |
|---|
| 545 | T0(I,JV)=T0(I,JV)-S0(I3,K,L,JV) |
|---|
| 546 | TX(I,JV)=ALF1Q(I)*TX(I,JV) |
|---|
| 547 | TY(I,JV)=TY(I,JV)-sy(I3,K,L,JV) |
|---|
| 548 | TZ(I,JV)=TZ(I,JV)-sz(I3,K,L,JV) |
|---|
| 549 | ENDDO |
|---|
| 550 | ENDDO |
|---|
| 551 | C |
|---|
| 552 | C |
|---|
| 553 | ELSE |
|---|
| 554 | C |
|---|
| 555 | DO 190 I=1,LON |
|---|
| 556 | SM(I,K,L)=TM(I) |
|---|
| 557 | 190 CONTINUE |
|---|
| 558 | DO 191 JV=1,NTRA |
|---|
| 559 | DO 1910 I=1,LON |
|---|
| 560 | S0(I,K,L,JV)=T0(I,JV) |
|---|
| 561 | sx(I,K,L,JV)=TX(I,JV) |
|---|
| 562 | sy(I,K,L,JV)=TY(I,JV) |
|---|
| 563 | sz(I,K,L,JV)=TZ(I,JV) |
|---|
| 564 | 1910 CONTINUE |
|---|
| 565 | 191 CONTINUE |
|---|
| 566 | C |
|---|
| 567 | ENDIF |
|---|
| 568 | C |
|---|
| 569 | 1 CONTINUE |
|---|
| 570 | C |
|---|
| 571 | C ----------- AA Test en fin de ADVX ------ Controle des S* |
|---|
| 572 | c OK |
|---|
| 573 | c DO 9998 l = 1, llm |
|---|
| 574 | c DO 9998 j = 1, jjp1 |
|---|
| 575 | c DO 9998 i = 1, iip1 |
|---|
| 576 | c IF (S0(i,j,l,ntra).lt.0..and.LIMIT) THEN |
|---|
| 577 | c PRINT*, '-------------------' |
|---|
| 578 | c PRINT*, 'En fin de ADVX' |
|---|
| 579 | c PRINT*,'SM(',i,j,l,')=',SM(i,j,l) |
|---|
| 580 | c PRINT*,'S0(',i,j,l,')=',S0(i,j,l,ntra) |
|---|
| 581 | c print*, 'sx(',i,j,l,')=',sx(i,j,l,ntra) |
|---|
| 582 | c print*, 'sy(',i,j,l,')=',sy(i,j,l,ntra) |
|---|
| 583 | c print*, 'sz(',i,j,l,')=',sz(i,j,l,ntra) |
|---|
| 584 | c WRITE (*,*) 'On arrete !! - pbl en fin de ADVX1' |
|---|
| 585 | cc STOP |
|---|
| 586 | c ENDIF |
|---|
| 587 | c 9998 CONTINUE |
|---|
| 588 | c |
|---|
| 589 | C ---------- bouclage cyclique |
|---|
| 590 | DO itrac=1,ntra |
|---|
| 591 | DO l = 1,llm |
|---|
| 592 | DO j = lati,latf |
|---|
| 593 | SM(iip1,j,l) = SM(1,j,l) |
|---|
| 594 | S0(iip1,j,l,itrac) = S0(1,j,l,itrac) |
|---|
| 595 | sx(iip1,j,l,itrac) = sx(1,j,l,itrac) |
|---|
| 596 | sy(iip1,j,l,itrac) = sy(1,j,l,itrac) |
|---|
| 597 | sz(iip1,j,l,itrac) = sz(1,j,l,itrac) |
|---|
| 598 | END DO |
|---|
| 599 | END DO |
|---|
| 600 | ENDDO |
|---|
| 601 | |
|---|
| 602 | c ----------- qqtite totale de traceur dans tte l'atmosphere |
|---|
| 603 | DO l = 1, llm |
|---|
| 604 | DO j = 1, jjp1 |
|---|
| 605 | DO i = 1, iim |
|---|
| 606 | cIM 240405 sqf = sqf + S0(i,j,l,9) |
|---|
| 607 | sqf = sqf + S0(i,j,l,ntra) |
|---|
| 608 | END DO |
|---|
| 609 | END DO |
|---|
| 610 | END DO |
|---|
| 611 | c |
|---|
| 612 | PRINT*,'------ DIAG DANS ADVX - SORTIE -----' |
|---|
| 613 | PRINT*,'sqf=',sqf |
|---|
| 614 | c------------- |
|---|
| 615 | |
|---|
| 616 | RETURN |
|---|
| 617 | END |
|---|
| 618 | C_________________________________________________________________ |
|---|
| 619 | C_________________________________________________________________ |
|---|
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