| 1 | MODULE calltherm_interface_mod |
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| 2 | |
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| 3 | IMPLICIT NONE |
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| 4 | |
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| 5 | CONTAINS |
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| 6 | !======================================================================= |
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| 7 | ! CALLTHERM_INTERFACE |
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| 8 | !======================================================================= |
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| 9 | ! Main interface to the Martian thermal plume model |
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| 10 | ! This interface handles sub-timesteps for this model |
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| 11 | ! A call to this interface must be inserted in the main 'physics' routine |
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| 12 | ! NB: for information: |
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| 13 | ! In the Mars LMD-GCM, the thermal plume model is called after |
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| 14 | ! the vertical turbulent mixing scheme (Mellor and Yamada) |
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| 15 | ! and the surface layer scheme (Richardson-based surface layer + subgrid gustiness) |
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| 16 | ! Other routines called before the thermals model are |
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| 17 | ! radiative transfer and (orographic) gravity wave drag. |
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| 18 | ! ----------------------------------------------------------------------- |
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| 19 | ! Author : A. Colaitis 2011-01-05 (with updates 2011-2013) |
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| 20 | ! after C. Rio and F. Hourdin |
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| 21 | ! Institution : Laboratoire de Meteorologie Dynamique (LMD) Paris, France |
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| 22 | ! ----------------------------------------------------------------------- |
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| 23 | ! Corresponding author : A. Spiga aymeric.spiga_AT_upmc.fr |
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| 24 | ! ----------------------------------------------------------------------- |
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| 25 | ! ASSOCIATED FILES |
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| 26 | ! --> thermcell_main_mars.F90 |
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| 27 | ! --> thermcell_dqup.F90 |
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| 28 | ! --> comtherm_h.F90 |
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| 29 | ! ----------------------------------------------------------------------- |
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| 30 | ! Reference paper: |
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| 31 | ! A. Colaïtis, A. Spiga, F. Hourdin, C. Rio, F. Forget, and E. Millour. |
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| 32 | ! A thermal plume model for the Martian convective boundary layer. |
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| 33 | ! Journal of Geophysical Research (Planets), 118:1468-1487, July 2013. |
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| 34 | ! http://dx.doi.org/10.1002/jgre.20104 |
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| 35 | ! http://arxiv.org/abs/1306.6215 |
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| 36 | ! ----------------------------------------------------------------------- |
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| 37 | ! Reference paper for terrestrial plume model: |
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| 38 | ! C. Rio and F. Hourdin. |
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| 39 | ! A thermal plume model for the convective boundary layer : Representation of cumulus clouds. |
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| 40 | ! Journal of the Atmospheric Sciences, 65:407-425, 2008. |
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| 41 | ! ----------------------------------------------------------------------- |
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| 42 | |
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| 43 | SUBROUTINE calltherm_interface (ngrid,nlayer,nq, igcm_co2, & |
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| 44 | & zzlev,zzlay, & |
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| 45 | & ptimestep,pu,pv,pt,pq,pdu,pdv,pdt,pdq,q2, & |
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| 46 | & pplay,pplev,pphi,zpopsk, & |
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| 47 | & pdu_th,pdv_th,pdt_th,pdq_th,lmax,zmaxth,pbl_dtke, & |
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| 48 | & pdhdif,hfmax,wstar,sensibFlux) |
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| 49 | |
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| 50 | use comtherm_h |
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| 51 | use tracer_mod, only: nqmx,noms |
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| 52 | |
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| 53 | ! SHARED VARIABLES. This needs adaptations in another climate model. |
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| 54 | ! contains physical constant values such as |
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| 55 | ! "g" : gravitational acceleration (m.s-2) |
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| 56 | ! "r" : recuced gas constant (J.K-1.mol-1) |
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| 57 | ! "cpp" : specific heat of the atmosphere (J.kg-1.K-1) |
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| 58 | USE comcstfi_h, only: r, g, cpp |
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| 59 | |
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| 60 | use thermcell_main_mars_mod, only: thermcell_main_mars |
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| 61 | |
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| 62 | use thermcell_dqup_mod, only: thermcell_dqup |
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| 63 | |
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| 64 | implicit none |
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| 65 | |
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| 66 | !-------------------------------------------------------- |
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| 67 | ! Input Variables |
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| 68 | !-------------------------------------------------------- |
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| 69 | |
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| 70 | INTEGER, INTENT(IN) :: ngrid ! number of horizontal grid points |
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| 71 | INTEGER, INTENT(IN) :: nlayer ! number of vertical grid points |
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| 72 | INTEGER, INTENT(IN) :: nq ! number of tracer species |
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| 73 | REAL, INTENT(IN) :: ptimestep !timestep (s) |
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| 74 | REAL, INTENT(IN) :: pplev(ngrid,nlayer+1) !intermediate pressure levels (Pa) |
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| 75 | REAL, INTENT(IN) :: pplay(ngrid,nlayer) !Pressure at the middle of the layers (Pa) |
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| 76 | REAL, INTENT(IN) :: pphi(ngrid,nlayer) !Geopotential at the middle of the layers (m2s-2) |
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| 77 | REAL, INTENT(IN) :: pu(ngrid,nlayer),pv(ngrid,nlayer) !u,v components of the wind (ms-1) |
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| 78 | REAL, INTENT(IN) :: pt(ngrid,nlayer),pq(ngrid,nlayer,nq)!temperature (K) and tracer concentration (kg/kg) |
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| 79 | REAL, INTENT(IN) :: zzlay(ngrid,nlayer) ! altitude at the middle of the layers |
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| 80 | REAL, INTENT(IN) :: zzlev(ngrid,nlayer+1) ! altitude at layer boundaries |
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| 81 | INTEGER, INTENT(IN) :: igcm_co2 ! index of the CO2 tracer in mixing ratio array |
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| 82 | ! --> 0 if no tracer is CO2 (or no tracer at all) |
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| 83 | ! --> this prepares special treatment for polar night mixing |
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| 84 | ! (see thermcell_main_mars) |
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| 85 | REAL, INTENT(IN) :: pdu(ngrid,nlayer),pdv(ngrid,nlayer) ! wind velocity change from routines called |
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| 86 | ! before thermals du/dt (m/s/s) |
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| 87 | REAL, INTENT(IN) :: pdq(ngrid,nlayer,nq) ! tracer concentration change from routines called |
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| 88 | ! before thermals dq/dt (kg/kg/s) |
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| 89 | REAL, INTENT(IN) :: pdt(ngrid,nlayer) ! temperature change from routines called before thermals dT/dt (K/s) |
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| 90 | REAL, INTENT(IN) :: q2(ngrid,nlayer+1) ! turbulent kinetic energy |
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| 91 | REAL, INTENT(IN) :: zpopsk(ngrid,nlayer) ! ratio of pressure at middle of layer to surface pressure, |
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| 92 | ! to the power r/cp, i.e. zpopsk=(pplay(ig,l)/pplev(ig,1))**rcp |
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| 93 | REAL, INTENT(IN) :: pdhdif(ngrid,nlayer) ! potential temperature change from turbulent diffusion scheme dT/dt (K/s) |
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| 94 | REAL, INTENT(IN) :: sensibFlux(ngrid) ! sensible heat flux computed from surface layer scheme |
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| 95 | |
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| 96 | !-------------------------------------------------------- |
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| 97 | ! Output Variables |
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| 98 | !-------------------------------------------------------- |
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| 99 | |
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| 100 | REAL, INTENT(OUT) :: pdu_th(ngrid,nlayer) ! wind velocity change from thermals du/dt (m/s/s) |
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| 101 | REAL, INTENT(OUT) :: pdv_th(ngrid,nlayer) ! wind velocity change from thermals dv/dt (m/s/s) |
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| 102 | REAL, INTENT(OUT) :: pdt_th(ngrid,nlayer) ! temperature change from thermals dT/dt (K/s) |
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| 103 | REAL, INTENT(OUT) :: pdq_th(ngrid,nlayer,nq) ! tracer change from thermals dq/dt (kg/kg/s) |
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| 104 | INTEGER, INTENT(OUT) :: lmax(ngrid) ! layer number reacher by thermals in grid point |
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| 105 | REAL, INTENT(OUT) :: zmaxth(ngrid) ! equivalent to lmax, but in (m), interpolated |
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| 106 | REAL, INTENT(OUT) :: pbl_dtke(ngrid,nlayer+1) ! turbulent kinetic energy change from thermals dtke/dt |
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| 107 | REAL, INTENT(OUT) :: wstar(ngrid) ! free convection velocity (m/s) |
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| 108 | |
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| 109 | !-------------------------------------------------------- |
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| 110 | ! Thermals local variables |
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| 111 | !-------------------------------------------------------- |
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| 112 | REAL zu(ngrid,nlayer), zv(ngrid,nlayer) |
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| 113 | REAL zt(ngrid,nlayer) |
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| 114 | REAL d_t_ajs(ngrid,nlayer) |
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| 115 | REAL d_u_ajs(ngrid,nlayer), d_q_ajs(ngrid,nlayer,nq) |
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| 116 | REAL d_v_ajs(ngrid,nlayer) |
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| 117 | REAL fm_therm(ngrid,nlayer+1), entr_therm(ngrid,nlayer) |
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| 118 | REAL detr_therm(ngrid,nlayer),detrmod(ngrid,nlayer) |
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| 119 | REAL zw2(ngrid,nlayer+1) |
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| 120 | REAL fraca(ngrid,nlayer+1),zfraca(ngrid,nlayer+1) |
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| 121 | REAL q_therm(ngrid,nlayer), pq_therm(ngrid,nlayer,nq) |
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| 122 | REAL q2_therm(ngrid,nlayer), dq2_therm(ngrid,nlayer) |
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| 123 | REAL lmax_real(ngrid) |
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| 124 | REAL masse(ngrid,nlayer) |
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| 125 | |
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| 126 | INTEGER l,ig,iq,ii(1),k |
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| 127 | CHARACTER (LEN=20) modname |
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| 128 | |
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| 129 | !-------------------------------------------------------- |
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| 130 | ! Local variables for sub-timestep |
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| 131 | !-------------------------------------------------------- |
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| 132 | |
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| 133 | REAL d_t_the(ngrid,nlayer), d_q_the(ngrid,nlayer,nq) |
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| 134 | INTEGER isplit |
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| 135 | REAL fact |
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| 136 | REAL zfm_therm(ngrid,nlayer+1),zdt |
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| 137 | REAL zentr_therm(ngrid,nlayer),zdetr_therm(ngrid,nlayer) |
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| 138 | REAL zheatFlux(ngrid,nlayer) |
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| 139 | REAL zheatFlux_down(ngrid,nlayer) |
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| 140 | REAL zbuoyancyOut(ngrid,nlayer) |
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| 141 | REAL zbuoyancyEst(ngrid,nlayer) |
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| 142 | REAL zzw2(ngrid,nlayer+1) |
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| 143 | REAL zmax(ngrid) |
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| 144 | INTEGER ndt,limz |
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| 145 | |
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| 146 | !-------------------------------------------------------- |
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| 147 | ! Diagnostics |
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| 148 | !-------------------------------------------------------- |
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| 149 | |
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| 150 | REAL heatFlux(ngrid,nlayer) |
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| 151 | REAL heatFlux_down(ngrid,nlayer) |
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| 152 | REAL buoyancyOut(ngrid,nlayer) |
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| 153 | REAL buoyancyEst(ngrid,nlayer) |
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| 154 | REAL hfmax(ngrid),wmax(ngrid) |
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| 155 | REAL pbl_teta(ngrid),dteta(ngrid,nlayer) |
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| 156 | REAL rpdhd(ngrid,nlayer) |
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| 157 | REAL wtdif(ngrid,nlayer),rho(ngrid,nlayer) |
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| 158 | REAL wtth(ngrid,nlayer) |
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| 159 | |
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| 160 | ! ********************************************************************** |
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| 161 | ! Initializations |
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| 162 | ! ********************************************************************** |
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| 163 | |
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| 164 | lmax(:)=0 |
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| 165 | pdu_th(:,:)=0. |
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| 166 | pdv_th(:,:)=0. |
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| 167 | pdt_th(:,:)=0. |
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| 168 | entr_therm(:,:)=0. |
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| 169 | detr_therm(:,:)=0. |
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| 170 | q2_therm(:,:)=0. |
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| 171 | dq2_therm(:,:)=0. |
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| 172 | pbl_dtke(:,:)=0. |
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| 173 | fm_therm(:,:)=0. |
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| 174 | zw2(:,:)=0. |
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| 175 | fraca(:,:)=0. |
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| 176 | zfraca(:,:)=0. |
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| 177 | pdq_th(:,:,:)=0. |
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| 178 | d_t_ajs(:,:)=0. |
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| 179 | d_u_ajs(:,:)=0. |
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| 180 | d_v_ajs(:,:)=0. |
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| 181 | d_q_ajs(:,:,:)=0. |
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| 182 | heatFlux(:,:)=0. |
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| 183 | heatFlux_down(:,:)=0. |
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| 184 | buoyancyOut(:,:)=0. |
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| 185 | buoyancyEst(:,:)=0. |
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| 186 | zmaxth(:)=0. |
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| 187 | lmax_real(:)=0. |
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| 188 | |
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| 189 | |
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| 190 | ! ********************************************************************** |
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| 191 | ! Preparing inputs for the thermals: increment tendancies |
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| 192 | ! from other subroutines called before the thermals model |
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| 193 | ! ********************************************************************** |
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| 194 | |
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| 195 | zu(:,:)=pu(:,:)+pdu(:,:)*ptimestep ! u-component of wind velocity |
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| 196 | zv(:,:)=pv(:,:)+pdv(:,:)*ptimestep ! v-component of wind velocity |
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| 197 | zt(:,:)=pt(:,:)+pdt(:,:)*ptimestep ! temperature |
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| 198 | |
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| 199 | pq_therm(:,:,:)=0. ! tracer concentration |
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| 200 | |
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| 201 | if(qtransport_thermals) then |
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| 202 | pq_therm(:,:,:)=pq(:,:,:)+pdq(:,:,:)*ptimestep ! tracer concentration |
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| 203 | endif |
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| 204 | |
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| 205 | |
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| 206 | IF(dtke_thermals) THEN |
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| 207 | DO l=1,nlayer |
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| 208 | q2_therm(:,l)=0.5*(q2(:,l)+q2(:,l+1)) |
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| 209 | ENDDO |
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| 210 | ENDIF |
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| 211 | |
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| 212 | ! ********************************************************************** |
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| 213 | ! --> CALLTHERM |
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| 214 | ! SUB-TIMESTEP LOOP |
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| 215 | ! ********************************************************************** |
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| 216 | |
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| 217 | zdt=ptimestep/REAL(nsplit_thermals) !subtimestep |
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| 218 | |
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| 219 | DO isplit=1,nsplit_thermals !temporal loop on the subtimestep |
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| 220 | |
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| 221 | ! Initialization of intermediary variables |
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| 222 | |
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| 223 | zzw2(:,:)=0. |
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| 224 | zmax(:)=0. |
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| 225 | lmax(:)=0 |
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| 226 | |
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| 227 | if (nq .ne. 0 .and. igcm_co2 .ne. 0) then !initialize co2 tracer tendancy |
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| 228 | d_q_the(:,:,igcm_co2)=0. |
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| 229 | endif |
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| 230 | |
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| 231 | ! CALL to main thermal routine |
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| 232 | CALL thermcell_main_mars(ngrid,nlayer,nq & |
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| 233 | & ,igcm_co2 & |
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| 234 | & ,zdt & |
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| 235 | & ,pplay,pplev,pphi,zzlev,zzlay & |
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| 236 | & ,zu,zv,zt,pq_therm,q2_therm & |
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| 237 | & ,d_t_the,d_q_the & |
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| 238 | & ,zfm_therm,zentr_therm,zdetr_therm,lmax,zmax,limz & |
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| 239 | & ,zzw2,fraca,zpopsk & |
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| 240 | & ,zheatFlux,zheatFlux_down & |
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| 241 | & ,zbuoyancyOut,zbuoyancyEst) |
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| 242 | |
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| 243 | fact=1./REAL(nsplit_thermals) |
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| 244 | |
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| 245 | ! Update thermals tendancies |
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| 246 | d_t_the(:,:)=d_t_the(:,:)*ptimestep*fact !temperature |
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| 247 | if (igcm_co2 .ne. 0) then |
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| 248 | d_q_the(:,:,igcm_co2)=d_q_the(:,:,igcm_co2)*ptimestep*fact !co2 mass mixing ratio |
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| 249 | endif |
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| 250 | zmaxth(:)=zmaxth(:)+zmax(:)*fact !thermals height |
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| 251 | lmax_real(:)=lmax_real(:)+float(lmax(:))*fact !thermals height index |
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| 252 | fm_therm(:,:)=fm_therm(:,:) & !upward mass flux |
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| 253 | & +zfm_therm(:,:)*fact |
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| 254 | entr_therm(:,:)=entr_therm(:,:) & !entrainment mass flux |
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| 255 | & +zentr_therm(:,:)*fact |
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| 256 | detr_therm(:,:)=detr_therm(:,:) & !detrainment mass flux |
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| 257 | & +zdetr_therm(:,:)*fact |
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| 258 | zfraca(:,:)=zfraca(:,:) + fraca(:,:)*fact !updraft fractional coverage |
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| 259 | heatFlux(:,:)=heatFlux(:,:) & !upward heat flux |
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| 260 | & +zheatFlux(:,:)*fact |
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| 261 | heatFlux_down(:,:)=heatFlux_down(:,:) & !downward heat flux |
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| 262 | & +zheatFlux_down(:,:)*fact |
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| 263 | buoyancyOut(:,:)=buoyancyOut(:,:) & !plume final buoyancy |
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| 264 | & +zbuoyancyOut(:,:)*fact |
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| 265 | buoyancyEst(:,:)=buoyancyEst(:,:) & !plume estimated buoyancy used for vertical velocity computation |
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| 266 | & +zbuoyancyEst(:,:)*fact |
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| 267 | zw2(:,:)=zw2(:,:) + zzw2(:,:)*fact !vertical velocity |
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| 268 | |
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| 269 | ! Save tendancies |
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| 270 | d_t_ajs(:,:)=d_t_ajs(:,:)+d_t_the(:,:) !temperature tendancy (delta T) |
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| 271 | if (igcm_co2 .ne. 0) then |
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| 272 | d_q_ajs(:,:,igcm_co2)=d_q_ajs(:,:,igcm_co2)+d_q_the(:,:,igcm_co2) !tracer tendancy (delta q) |
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| 273 | endif |
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| 274 | |
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| 275 | ! Increment temperature and co2 concentration for next pass in subtimestep loop |
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| 276 | zt(:,:) = zt(:,:) + d_t_the(:,:) !temperature |
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| 277 | if (igcm_co2 .ne. 0) then |
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| 278 | pq_therm(:,:,igcm_co2) = & |
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| 279 | & pq_therm(:,:,igcm_co2) + d_q_the(:,:,igcm_co2) !co2 tracer |
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| 280 | endif |
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| 281 | |
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| 282 | |
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| 283 | ENDDO ! isplit |
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| 284 | !**************************************************************** |
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| 285 | |
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| 286 | ! Now that we have computed total entrainment and detrainment, we can |
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| 287 | ! advect u, v, and q in thermals. (potential temperature and co2 MMR |
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| 288 | ! have already been advected in thermcell_main because they are coupled |
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| 289 | ! to the determination of the thermals caracteristics). This is done |
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| 290 | ! separatly because u,v, and q are not used in thermcell_main for |
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| 291 | ! any thermals-related computation : they are purely passive. |
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| 292 | |
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| 293 | ! mass of cells |
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| 294 | do l=1,nlayer |
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| 295 | masse(:,l)=(pplev(:,l)-pplev(:,l+1))/g |
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| 296 | enddo |
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| 297 | |
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| 298 | ! recompute detrainment mass flux from entrainment and upward mass flux |
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| 299 | ! this ensure mass flux conservation |
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| 300 | detrmod(:,:)=0. |
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| 301 | do l=1,limz |
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| 302 | do ig=1,ngrid |
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| 303 | detrmod(ig,l)=fm_therm(ig,l)-fm_therm(ig,l+1) & |
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| 304 | & +entr_therm(ig,l) |
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| 305 | if (detrmod(ig,l).lt.0.) then |
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| 306 | entr_therm(ig,l)=entr_therm(ig,l)-detrmod(ig,l) |
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| 307 | detrmod(ig,l)=0. |
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| 308 | endif |
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| 309 | enddo |
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| 310 | enddo |
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| 311 | |
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| 312 | ! u component of wind velocity advection in thermals |
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| 313 | ! result is a derivative (d_u_ajs in m/s/s) |
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| 314 | ndt=10 |
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| 315 | call thermcell_dqup(ngrid,nlayer,ptimestep & |
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| 316 | & ,fm_therm,entr_therm,detrmod, & |
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| 317 | & masse,zu,d_u_ajs,ndt,limz) |
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| 318 | |
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| 319 | ! v component of wind velocity advection in thermals |
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| 320 | ! result is a derivative (d_v_ajs in m/s/s) |
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| 321 | call thermcell_dqup(ngrid,nlayer,ptimestep & |
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| 322 | & ,fm_therm,entr_therm,detrmod, & |
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| 323 | & masse,zv,d_v_ajs,ndt,limz) |
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| 324 | |
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| 325 | ! non co2 tracers advection in thermals |
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| 326 | ! result is a derivative (d_q_ajs in kg/kg/s) |
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| 327 | |
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| 328 | if (nq .ne. 0.) then |
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| 329 | DO iq=1,nq |
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| 330 | if (iq .ne. igcm_co2) then |
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| 331 | call thermcell_dqup(ngrid,nlayer,ptimestep & |
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| 332 | & ,fm_therm,entr_therm,detrmod, & |
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| 333 | & masse,pq_therm(:,:,iq),d_q_ajs(:,:,iq),ndt,limz) |
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| 334 | endif |
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| 335 | ENDDO |
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| 336 | endif |
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| 337 | |
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| 338 | ! tke advection in thermals |
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| 339 | ! result is a tendancy (d_u_ajs in J) |
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| 340 | if (dtke_thermals) then |
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| 341 | call thermcell_dqup(ngrid,nlayer,ptimestep & |
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| 342 | & ,fm_therm,entr_therm,detrmod, & |
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| 343 | & masse,q2_therm,dq2_therm,ndt,limz) |
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| 344 | endif |
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| 345 | |
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| 346 | ! compute wmax for diagnostics |
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| 347 | DO ig=1,ngrid |
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| 348 | wmax(ig)=MAXVAL(zw2(ig,:)) |
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| 349 | ENDDO |
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| 350 | |
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| 351 | ! ********************************************************************** |
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| 352 | ! ********************************************************************** |
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| 353 | ! ********************************************************************** |
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| 354 | ! CALLTHERM END |
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| 355 | ! ********************************************************************** |
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| 356 | ! ********************************************************************** |
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| 357 | ! ********************************************************************** |
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| 358 | |
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| 359 | |
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| 360 | ! ********************************************************************** |
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| 361 | ! Preparing outputs |
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| 362 | ! ********************************************************************** |
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| 363 | |
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| 364 | do l=1,limz |
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| 365 | pdu_th(:,l)=d_u_ajs(:,l) |
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| 366 | pdv_th(:,l)=d_v_ajs(:,l) |
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| 367 | enddo |
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| 368 | |
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| 369 | ! if tracers are transported in thermals, update output variables, else these are 0. |
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| 370 | if(qtransport_thermals) then |
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| 371 | do iq=1,nq |
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| 372 | if (iq .ne. igcm_co2) then |
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| 373 | do l=1,limz |
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| 374 | pdq_th(:,l,iq)=d_q_ajs(:,l,iq) !non-co2 tracers d_q_ajs are dq/dt (kg/kg/s) |
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| 375 | enddo |
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| 376 | else |
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| 377 | do l=1,limz |
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| 378 | pdq_th(:,l,iq)=d_q_ajs(:,l,iq)/ptimestep !co2 tracer d_q_ajs is dq (kg/kg) |
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| 379 | enddo |
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| 380 | endif |
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| 381 | enddo |
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| 382 | endif |
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| 383 | |
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| 384 | ! if tke is transported in thermals, update output variable, else this is 0. |
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| 385 | IF(dtke_thermals) THEN |
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| 386 | DO l=2,nlayer |
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| 387 | pbl_dtke(:,l)=0.5*(dq2_therm(:,l-1)+dq2_therm(:,l)) |
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| 388 | ENDDO |
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| 389 | |
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| 390 | pbl_dtke(:,1)=0.5*dq2_therm(:,1) |
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| 391 | pbl_dtke(:,nlayer+1)=0. |
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| 392 | ENDIF |
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| 393 | |
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| 394 | ! update output variable for temperature. d_t_ajs is delta T in (K), pdt_th is dT/dt in (K/s) |
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| 395 | do l=1,limz |
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| 396 | pdt_th(:,l)=d_t_ajs(:,l)/ptimestep |
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| 397 | enddo |
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| 398 | |
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| 399 | |
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| 400 | ! ********************************************************************** |
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| 401 | ! SURFACE LAYER INTERFACE |
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| 402 | ! Compute the free convection velocity w* scale for surface layer gustiness |
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| 403 | ! speed parameterization. The computed value of w* will be used at the next |
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| 404 | ! timestep to modify surface-atmosphere exchange fluxes, because the surface |
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| 405 | ! layer scheme and diffusion are called BEFORE the thermals. (outside of these |
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| 406 | ! routines) |
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| 407 | ! ********************************************************************** |
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| 408 | |
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| 409 | ! Potential temperature gradient |
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| 410 | |
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| 411 | dteta(:,nlayer)=0. |
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| 412 | DO l=1,nlayer-1 |
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| 413 | DO ig=1, ngrid |
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| 414 | dteta(ig,l) = ((zt(ig,l+1)-zt(ig,l))/zpopsk(ig,l)) & |
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| 415 | & /(zzlay(ig,l+1)-zzlay(ig,l)) |
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| 416 | ENDDO |
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| 417 | ENDDO |
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| 418 | |
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| 419 | ! Computation of the PBL mixed layer temperature |
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| 420 | |
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| 421 | DO ig=1, ngrid |
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| 422 | ii=MINLOC(abs(dteta(ig,1:lmax(ig)))) |
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| 423 | pbl_teta(ig) = zt(ig,ii(1))/zpopsk(ig,ii(1)) |
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| 424 | ENDDO |
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| 425 | |
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| 426 | ! In order to have an accurate w*, we must add the heat flux from the |
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| 427 | ! diffusion scheme to the computation of the maximum heat flux hfmax |
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| 428 | ! Here pdhdif is the potential temperature change from the diffusion |
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| 429 | ! scheme (Mellor and Yamada, see paper section 6, paragraph 57) |
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| 430 | |
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| 431 | ! compute rho as it is after the diffusion |
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| 432 | |
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| 433 | rho(:,:)=pplay(:,:) & |
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| 434 | & /(r*(pt(:,:)+pdhdif(:,:)*zpopsk(:,:)*ptimestep)) |
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| 435 | |
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| 436 | ! integrate -rho*pdhdif |
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| 437 | |
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| 438 | rpdhd(:,:)=0. |
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| 439 | |
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| 440 | DO ig=1,ngrid |
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| 441 | DO l=1,lmax(ig) |
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| 442 | rpdhd(ig,l)=0. |
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| 443 | DO k=1,l |
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| 444 | rpdhd(ig,l)=rpdhd(ig,l)-rho(ig,k)*pdhdif(ig,k)* & |
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| 445 | & (zzlev(ig,k+1)-zzlev(ig,k)) |
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| 446 | ENDDO |
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| 447 | rpdhd(ig,l)=rpdhd(ig,l)-sensibFlux(ig)/cpp |
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| 448 | ENDDO |
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| 449 | ENDDO |
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| 450 | |
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| 451 | ! compute w'theta' (vertical turbulent flux of temperature) from |
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| 452 | ! the diffusion scheme |
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| 453 | |
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| 454 | wtdif(:,:)=rpdhd(:,:)/rho(:,:) |
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| 455 | |
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| 456 | ! Now we compute the contribution of the thermals to w'theta': |
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| 457 | ! compute rho as it is after the thermals |
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| 458 | |
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| 459 | rho(:,:)=pplay(:,:)/(r*(zt(:,:))) |
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| 460 | |
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| 461 | ! integrate -rho*pdhdif |
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| 462 | |
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| 463 | DO ig=1,ngrid |
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| 464 | DO l=1,lmax(ig) |
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| 465 | rpdhd(ig,l)=0. |
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| 466 | DO k=1,l |
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| 467 | rpdhd(ig,l)=rpdhd(ig,l)-rho(ig,k)*(pdt_th(ig,k)/zpopsk(ig,k))* & |
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| 468 | & (zzlev(ig,k+1)-zzlev(ig,k)) |
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| 469 | ENDDO |
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| 470 | rpdhd(ig,l)=rpdhd(ig,l)+ & |
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| 471 | & rho(ig,1)*(heatFlux(ig,1)+heatFlux_down(ig,1)) |
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| 472 | ENDDO |
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| 473 | ENDDO |
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| 474 | rpdhd(:,nlayer)=0. |
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| 475 | |
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| 476 | ! compute w'teta' from thermals |
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| 477 | |
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| 478 | wtth(:,:)=rpdhd(:,:)/rho(:,:) |
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| 479 | |
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| 480 | ! Add vertical turbulent heat fluxes from the thermals and the diffusion scheme |
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| 481 | ! and compute the maximum |
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| 482 | |
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| 483 | DO ig=1,ngrid |
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| 484 | hfmax(ig)=MAXVAL(wtth(ig,:)+wtdif(ig,:)) |
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| 485 | ENDDO |
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| 486 | |
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| 487 | ! Finally we can compute the free convection velocity scale |
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| 488 | ! We follow Spiga et. al 2010 (QJRMS) |
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| 489 | ! ------------ |
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| 490 | |
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| 491 | DO ig=1, ngrid |
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| 492 | IF (zmax(ig) .gt. 0.) THEN |
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| 493 | wstar(ig)=(g*zmaxth(ig)*hfmax(ig)/pbl_teta(ig))**(1./3.) |
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| 494 | ELSE |
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| 495 | wstar(ig)=0. |
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| 496 | ENDIF |
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| 497 | ENDDO |
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| 498 | |
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| 499 | END SUBROUTINE calltherm_interface |
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| 500 | |
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| 501 | END MODULE calltherm_interface_mod |
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