1 | SUBROUTINE pbl_parameters(ngrid,nlay,ps,pplay,pz0, |
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2 | & pg,zzlay,zzlev,pu,pv,wstar_in,hfmax,zmax,pts,ph,z_out,n_out, |
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3 | & T_out,u_out,ustar,tstar,L_mo,vhf,vvv) |
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4 | IMPLICIT NONE |
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5 | !======================================================================= |
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6 | ! |
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7 | ! Anlysis of the PBL from input temperature, wind field and thermals outputs. |
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8 | ! |
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9 | ! ------- |
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10 | ! |
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11 | ! Author: Arnaud Colaitis 09/01/12 |
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12 | ! ------- |
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13 | ! |
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14 | ! Arguments: |
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15 | ! ---------- |
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16 | ! |
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17 | ! inputs: |
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18 | ! ------ |
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19 | ! ngrid size of the horizontal grid |
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20 | ! nlay size of the vertical grid |
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21 | ! pz0(ngrid) surface roughness length |
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22 | ! pg gravity (m s -2) |
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23 | ! zzlay(ngrid,nlay) height of mid-layers |
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24 | ! zzlev(ngrid,nlay+1) height of layers interfaces |
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25 | ! pu(ngrid,nlay) u component of the wind |
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26 | ! pv(ngrid,nlay) v component of the wind |
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27 | ! wstar_in(ngrid) free convection velocity in thermals |
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28 | ! hfmax(ngrid) maximum vertical turbulent heat flux in thermals |
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29 | ! zmax(ngrid) height reached by the thermals (pbl height) |
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30 | ! pts(ngrid) surface temperature |
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31 | ! ph(ngrid,nlay) potential temperature T*(p/ps)^kappa |
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32 | ! z_out(n_out) heights of interpolation |
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33 | ! n_out number of points for interpolation |
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34 | ! |
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35 | ! outputs: |
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36 | ! ------ |
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37 | ! |
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38 | ! Teta_out(ngrid,n_out) interpolated teta |
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39 | ! u_out(ngrid,n_out) interpolated u |
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40 | ! ustar(ngrid) friction velocity |
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41 | ! tstar(ngrid) friction temperature |
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42 | ! wstar(ngrid) free convection velocity |
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43 | ! L_mo(ngrid) monin_obukhov length |
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44 | ! |
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45 | ! |
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46 | !======================================================================= |
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47 | ! |
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48 | !----------------------------------------------------------------------- |
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49 | ! Declarations: |
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50 | ! ------------- |
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51 | |
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52 | #include "comcstfi.h" |
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53 | #include "callkeys.h" |
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54 | |
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55 | ! Arguments: |
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56 | ! ---------- |
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57 | |
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58 | INTEGER, INTENT(IN) :: ngrid,nlay,n_out |
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59 | REAL, INTENT(IN) :: pz0(ngrid),ps(ngrid),pplay(ngrid,nlay) |
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60 | REAL, INTENT(IN) :: pg,zzlay(ngrid,nlay),zzlev(ngrid,nlay) |
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61 | REAL, INTENT(IN) :: pu(ngrid,nlay),pv(ngrid,nlay) |
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62 | REAL, INTENT(IN) :: wstar_in(ngrid),hfmax(ngrid),zmax(ngrid) |
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63 | REAL, INTENT(IN) :: pts(ngrid),ph(ngrid,nlay) |
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64 | REAL, INTENT(IN) :: z_out(n_out) |
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65 | |
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66 | ! Outputs: |
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67 | ! -------- |
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68 | |
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69 | REAL, INTENT(OUT) :: T_out(ngrid,n_out),u_out(ngrid,n_out) |
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70 | REAL Teta_out(ngrid,n_out) |
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71 | REAL, INTENT(OUT) :: ustar(ngrid), tstar(ngrid) |
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72 | REAL wstar(ngrid) |
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73 | REAL, INTENT(OUT) :: L_mo(ngrid) |
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74 | |
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75 | ! Local: |
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76 | ! ------ |
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77 | |
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78 | INTEGER ig,k,n |
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79 | REAL karman,nu |
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80 | DATA karman,nu/.41,0.001/ |
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81 | SAVE karman,nu |
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82 | |
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83 | ! Local(2): |
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84 | ! --------- |
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85 | |
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86 | REAL zout |
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87 | REAL rib(ngrid) ! Bulk Richardson number |
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88 | REAL fm(ngrid) ! stability function for momentum |
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89 | REAL fh(ngrid) ! stability function for heat |
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90 | REAL z1z0,z1z0t ! ratios z1/z0 and z1/z0T |
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91 | ! phim = 1+betam*zeta or (1-bm*zeta)**am |
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92 | ! phih = alphah + betah*zeta or alphah(1.-bh*zeta)**ah |
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93 | REAL betam, betah, alphah, bm, bh, lambda |
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94 | ! ah and am are assumed to be -0.25 and -0.5 respectively |
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95 | REAL cdn(ngrid),chn(ngrid) ! neutral momentum and heat drag coefficient |
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96 | REAL pz0t ! initial thermal roughness length. (local) |
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97 | REAL ric ! critical richardson number |
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98 | REAL reynolds(ngrid) ! reynolds number for UBL |
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99 | REAL prandtl(ngrid) ! prandtl number for UBL |
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100 | REAL pz0tcomp(ngrid) ! computed z0t |
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101 | REAL ite |
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102 | REAL residual,zcd0,z1 |
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103 | REAL pcdv(ngrid),pcdh(ngrid) |
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104 | REAL zu2(ngrid) ! Large-scale wind at first layer |
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105 | REAL pbl_teta(ngrid) ! mixed-layer potential temperature |
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106 | INTEGER pbl_height_index(ngrid) ! index of nearest vertical grid point for zmax |
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107 | REAL dteta(ngrid,nlay),x(ngrid) ! potential temperature gradient and z/zi |
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108 | REAL dvhf(ngrid),dvvv(ngrid) ! dimensionless vertical heat flux and |
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109 | ! dimensionless vertical velocity variance |
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110 | REAL vhf(ngrid),vvv(ngrid) ! vertical heat flux and vertical velocity variance |
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111 | INTEGER ii(1) |
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112 | ! temporary |
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113 | INTEGER dimout |
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114 | |
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115 | !------------------------------------------------------------------------ |
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116 | !------------------------------------------------------------------------ |
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117 | ! PART I : RICHARDSON/REYNOLDS/THERMAL_ROUGHNESS/STABILITY_COEFFICIENTS |
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118 | !------------------------------------------------------------------------ |
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119 | !------------------------------------------------------------------------ |
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120 | |
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121 | DO n=1,n_out |
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122 | |
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123 | c Initialisation : |
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124 | |
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125 | L_mo(:)=0. |
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126 | ustar(:)=0. |
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127 | tstar(:)=0. |
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128 | zout=z_out(n) |
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129 | reynolds(:)=0. |
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130 | pz0t = 0. |
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131 | pz0tcomp(:) = 0.1*pz0(:) |
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132 | rib(:)=0. |
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133 | pcdv(:)=0. |
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134 | pcdh(:)=0. |
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135 | |
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136 | ! this formulation assumes alphah=1., implying betah=betam |
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137 | ! We use Dyer et al. parameters, as they cover a broad range of Richardson numbers : |
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138 | |
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139 | bm=16. !UBL |
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140 | bh=16. !UBL |
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141 | alphah=1. |
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142 | betam=5. !SBL |
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143 | betah=5. !SBL |
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144 | lambda=(sqrt(bh/bm))/alphah |
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145 | ric=betah/(betam**2) |
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146 | DO ig=1,ngrid |
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147 | ite=0. |
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148 | residual=abs(pz0tcomp(ig)-pz0t) |
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149 | ! zu2(ig)=MAX(pu(ig,1)*pu(ig,1)+pv(ig,1)*pv(ig,1) |
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150 | ! & ,(0.3*wstar_in(ig))**2) |
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151 | zu2(ig)=pu(ig,1)*pu(ig,1)+pv(ig,1)*pv(ig,1)+ |
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152 | & + (log(1.+0.7*wstar_in(ig) + 2.3*wstar_in(ig)**2))**2 |
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153 | |
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154 | DO WHILE((residual .gt. 0.01*pz0(ig)) .and. (ite .lt. 10.)) |
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155 | |
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156 | pz0t=pz0tcomp(ig) |
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157 | IF (zu2(ig) .ne. 0.) THEN |
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158 | ! Richardson number formulation proposed by D.E. England et al. (1995) |
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159 | rib(ig) = (pg/pts(ig)) |
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160 | & *sqrt(zzlay(ig,1)*pz0(ig)) |
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161 | & *(((log(zzlay(ig,1)/pz0(ig)))**2)/(log(zzlay(ig,1)/pz0t))) |
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162 | & *(ph(ig,1)-pts(ig))/zu2(ig) |
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163 | ELSE |
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164 | print*,'warning, infinite Richardson at surface' |
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165 | print*,pu(ig,1),pv(ig,1) |
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166 | rib(ig) = ric |
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167 | ENDIF |
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168 | |
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169 | z1z0=zzlay(ig,1)/pz0(ig) |
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170 | z1z0t=zzlay(ig,1)/pz0t |
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171 | |
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172 | cdn(ig)=karman/log(z1z0) |
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173 | cdn(ig)=cdn(ig)*cdn(ig) |
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174 | chn(ig)=cdn(ig)*log(z1z0)/log(z1z0t) |
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175 | |
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176 | ! STABLE BOUNDARY LAYER : |
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177 | IF (rib(ig) .gt. 0.) THEN |
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178 | ! From D.E. England et al. (95) |
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179 | prandtl(ig)=1. |
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180 | if(rib(ig) .lt. ric) then |
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181 | ! Assuming alphah=1. and bh=bm for stable conditions : |
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182 | fm(ig)=((ric-rib(ig))/ric)**2 |
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183 | fh(ig)=((ric-rib(ig))/ric)**2 |
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184 | else |
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185 | ! For Ri>Ric, we consider Ri->Infinity => no turbulent mixing at surface |
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186 | fm(ig)=0. |
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187 | fh(ig)=0. |
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188 | endif |
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189 | ! UNSTABLE BOUNDARY LAYER : |
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190 | ELSE |
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191 | ! From D.E. England et al. (95) |
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192 | fm(ig)=sqrt(1.-lambda*bm*rib(ig)) |
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193 | fh(ig)=(1./alphah)*((1.-lambda*bh*rib(ig))**0.5)* |
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194 | & (1.-lambda*bm*rib(ig))**0.25 |
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195 | prandtl(ig)=alphah*((1.-lambda*bm*rib(ig))**0.25)/ |
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196 | & ((1.-lambda*bh*rib(ig))**0.5) |
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197 | ENDIF |
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198 | |
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199 | reynolds(ig)=karman*sqrt(fm(ig)) |
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200 | & *sqrt(zu2(ig)) |
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201 | & *pz0(ig)/(log(z1z0)*nu) |
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202 | pz0tcomp(ig)=pz0(ig)*exp(-karman*7.3* |
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203 | & (reynolds(ig)**0.25)*(prandtl(ig)**0.5)) |
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204 | residual = abs(pz0t-pz0tcomp(ig)) |
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205 | ite = ite+1 |
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206 | |
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207 | ENDDO ! of while |
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208 | pz0t=0. |
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209 | |
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210 | ! Drag computation: |
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211 | |
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212 | pcdv(ig)=cdn(ig)*fm(ig) |
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213 | pcdh(ig)=chn(ig)*fh(ig) |
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214 | |
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215 | ENDDO ! of ngrid |
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216 | |
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217 | !------------------------------------------------------------------------ |
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218 | !------------------------------------------------------------------------ |
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219 | ! PART II : USTAR/TSTAR/U_OUT/TETA_OUT COMPUTATIONS |
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220 | !------------------------------------------------------------------------ |
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221 | !------------------------------------------------------------------------ |
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222 | |
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223 | |
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224 | ! u* theta* computation |
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225 | ! and Monin Obukhov length: |
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226 | |
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227 | DO ig=1,ngrid |
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228 | IF (rib(ig) .ge. ric) THEN |
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229 | ustar(ig)=0. |
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230 | tstar(ig)=0. |
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231 | L_mo(ig)=0. |
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232 | ELSE |
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233 | ustar(ig)=sqrt(pcdv(ig)) |
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234 | & *sqrt(pu(ig,1)*pu(ig,1)+pv(ig,1)*pv(ig,1)) |
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235 | tstar(ig)=-pcdh(ig)*(pts(ig)-ph(ig,1)) |
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236 | & /sqrt(pcdv(ig)) |
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237 | L_mo(ig)=pts(ig)*(ustar(ig)**2)/(pg*karman*tstar(ig)) !as defined here, L is positive for SBL, negative for UBL |
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238 | ENDIF |
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239 | ENDDO |
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240 | |
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241 | ! Monin Obukhov length: |
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242 | |
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243 | ! DO ig=1,ngrid |
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244 | ! IF (rib(ig) .ge. ric) THEN |
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245 | ! L_mo(ig)=0. |
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246 | ! ELSE |
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247 | ! L_mo(ig)=pts(ig)*(ustar(ig)**2)/(pg*karman*tstar(ig)) !as defined here, L is positive for SBL, negative for UBL |
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248 | ! ENDIF |
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249 | ! ENDDO |
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250 | |
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251 | ! Interpolation: |
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252 | |
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253 | DO ig=1,ngrid |
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254 | IF(zout .lt. pz0tcomp(ig)) THEN |
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255 | u_out(ig,n)=0. |
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256 | Teta_out(ig,n)=pts(ig) |
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257 | ELSEIF (L_mo(ig) .gt. 0.) THEN |
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258 | ! u_out(ig,n)=(ustar(ig)/karman)*log(zout/pz0(ig)) + |
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259 | ! & 5.*(ustar(ig)/(karman*L_mo(ig)))*(zout-pz0(ig)) |
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260 | ! Teta_out(ig,n)=pts(ig)+(tstar(ig)/(prandtl(ig)*karman)) |
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261 | ! & *log(zout/pz0tcomp(ig)) + |
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262 | ! & 5.*(tstar(ig)/(prandtl(ig)*karman*L_mo(ig))) |
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263 | ! & *(zout-pz0tcomp(ig)) |
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264 | IF ((zout/L_mo(ig).lt.ric).and.(pz0(ig).lt.ric)) THEN |
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265 | ! & ((zout/L_mo(ig).gt.ric).and.(pz0(ig).gt.ric)) ) THEN |
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266 | |
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267 | u_out(ig,n)=(ustar(ig)/karman)*( |
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268 | & log((ric-pz0(ig)/L_mo(ig))/(ric-zout/L_mo(ig))) |
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269 | & +log(zout/pz0(ig)) |
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270 | & ) |
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271 | ELSEIF ((zout/L_mo(ig).gt.ric).and.(pz0(ig).gt.ric)) THEN |
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272 | |
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273 | u_out(ig,n)=(ustar(ig)/karman)*( |
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274 | & log((zout-ric*L_mo(ig))/(pz0(ig)-ric*L_mo(ig))) |
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275 | & +log(pz0(ig)/zout) |
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276 | & ) |
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277 | |
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278 | ELSEIF ((zout/L_mo(ig).gt.ric).and.(pz0(ig).lt.ric)) THEN |
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279 | !integral of the stability function does not converge |
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280 | |
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281 | |
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282 | u_out(ig,n)=sqrt(pu(ig,1)**2 + pv(ig,1)**2) |
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283 | |
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284 | |
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285 | ENDIF |
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286 | IF((zout/L_mo(ig).lt.ric).and.(pz0tcomp(ig).lt.ric)) THEN |
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287 | ! & ((zout/L_mo(ig).gt.ric).and.(pz0tcomp(ig).gt.ric)) ) THEN |
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288 | |
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289 | Teta_out(ig,n)=pts(ig)+(tstar(ig)/(prandtl(ig)*karman))*( |
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290 | & log((ric-pz0tcomp(ig)/L_mo(ig))/(ric-zout/L_mo(ig))) |
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291 | & +log(zout/pz0tcomp(ig)) |
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292 | & ) |
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293 | ELSEIF ((zout/L_mo(ig).gt.ric).and.(pz0tcomp(ig).gt.ric)) THEN |
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294 | |
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295 | Teta_out(ig,n)=pts(ig)+(tstar(ig)/(prandtl(ig)*karman))*( |
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296 | & log((zout-ric*L_mo(ig))/(pz0tcomp(ig)-ric*L_mo(ig))) |
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297 | & +log(pz0tcomp(ig)/zout) |
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298 | & ) |
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299 | |
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300 | ELSEIF ((zout/L_mo(ig).gt.ric).and.(pz0tcomp(ig).lt.ric)) THEN |
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301 | !integral of the stability function does not converge |
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302 | |
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303 | Teta_out(ig,n)=ph(ig,1) |
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304 | |
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305 | ENDIF |
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306 | |
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307 | ELSEIF (L_mo(ig) .lt. 0.) THEN |
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308 | |
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309 | IF(L_mo(ig) .gt. -1000.) THEN |
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310 | |
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311 | u_out(ig,n)=(ustar(ig)/karman)*( |
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312 | & 2.*atan((1.-16.*zout/L_mo(ig))**0.25) |
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313 | & -2.*atan((1.-16.*pz0(ig)/L_mo(ig))**0.25) |
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314 | & -2.*log(1.+(1.-16.*zout/L_mo(ig))**0.25) |
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315 | & +2.*log(1.+(1.-16.*pz0(ig)/L_mo(ig))**0.25) |
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316 | & - log(1.+sqrt(1.-16.*zout/L_mo(ig))) |
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317 | & + log(1.+sqrt(1.-16.*pz0(ig)/L_mo(ig))) |
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318 | & + log(zout/pz0(ig)) |
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319 | & ) |
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320 | |
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321 | Teta_out(ig,n)=MAX(pts(ig)+(tstar(ig)/(prandtl(ig)*karman))*( |
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322 | & 2.*log(1.+sqrt(1.-16.*pz0tcomp(ig)/L_mo(ig))) |
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323 | & -2.*log(1.+sqrt(1.-16.*zout/L_mo(ig))) |
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324 | & + log(zout/pz0tcomp(ig)) |
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325 | & ),ph(ig,1)) |
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326 | |
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327 | ELSE |
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328 | |
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329 | ! We have to treat the case where L is very large and negative, |
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330 | ! corresponding to a very nearly stable atmosphere (but not quite !) |
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331 | ! i.e. teta* <0 and almost zero. We choose the cutoff |
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332 | ! corresponding to L_mo < -1000 and use a 3rd order taylor expansion. The difference |
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333 | ! between the two expression for z/L = -1/1000 is -1.54324*10^-9 |
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334 | ! (we do that to avoid using r*4 precision, otherwise, we get -inf values) |
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335 | |
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336 | u_out(ig,n)=(ustar(ig)/karman)*( |
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337 | & (4./L_mo(ig))*(zout-pz0(ig)) |
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338 | & + (20./(L_mo(ig))**2)*(zout**2-pz0(ig)**2) |
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339 | & + (160./(L_mo(ig))**3)*(zout**3-pz0(ig)**3) |
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340 | & + log(zout/pz0(ig)) |
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341 | & ) |
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342 | |
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343 | Teta_out(ig,n)=MAX(pts(ig)+(tstar(ig)/(prandtl(ig)*karman))*( |
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344 | & (8./L_mo(ig))*(zout-pz0tcomp(ig)) |
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345 | & + (48./(L_mo(ig))**2)*(zout**2-pz0tcomp(ig)**2) |
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346 | & + (1280./(3.*(L_mo(ig))**3))*(zout**3-pz0tcomp(ig)**3) |
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347 | & + log(zout/pz0tcomp(ig)) |
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348 | & ),ph(ig,1)) |
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349 | |
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350 | ENDIF |
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351 | ELSE |
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352 | u_out(ig,n)=sqrt(pu(ig,1)**2 + pv(ig,1)**2) |
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353 | Teta_out(ig,n)=ph(ig,1) |
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354 | ENDIF |
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355 | IF(zout .lt. pz0(ig)) THEN |
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356 | u_out(ig,n)=0. |
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357 | ENDIF |
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358 | |
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359 | ! Final check |
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360 | IF (L_mo(ig) .gt. 0) THEN |
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361 | IF (Teta_out(ig,n) .gt. ph(ig,1)) THEN |
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362 | Teta_out(ig,n)=ph(ig,1) |
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363 | ELSEIF (Teta_out(ig,n) .lt. pts(ig)) THEN |
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364 | Teta_out(ig,n)=pts(ig) |
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365 | ENDIF |
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366 | ELSEIF (L_mo(ig) .lt. 0) THEN |
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367 | IF (Teta_out(ig,n) .lt. ph(ig,1)) THEN |
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368 | Teta_out(ig,n)=ph(ig,1) |
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369 | ELSEIF (Teta_out(ig,n) .gt. pts(ig)) THEN |
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370 | Teta_out(ig,n)=pts(ig) |
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371 | ENDIF |
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372 | ENDIF |
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373 | |
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374 | IF (u_out(ig,n) .gt. sqrt(pu(ig,1)**2 + pv(ig,1)**2)) THEN |
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375 | u_out(ig,n)=sqrt(pu(ig,1)**2 + pv(ig,1)**2) |
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376 | ENDIF |
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377 | |
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378 | ENDDO |
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379 | |
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380 | ! when using convective adjustment without thermals, a vertical potential temperature |
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381 | ! profile is assumed up to the thermal roughness length. Hence, theoretically, theta |
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382 | ! interpolated at any height in the surface layer is theta at the first level. |
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383 | |
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384 | IF ((.not.calltherm).and.(calladj)) THEN |
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385 | Teta_out(:,n)=ph(:,1) |
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386 | u_out(:,n)=(sqrt(cdn(:))*sqrt(pu(:,1)*pu(:,1)+pv(:,1)*pv(:,1)) |
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387 | & /karman)*log(zout/pz0(:)) |
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388 | ENDIF |
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389 | T_out(:,n) = Teta_out(:,n)*(exp( |
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390 | & (zout/zzlay(:,1))*(log(pplay(:,1)/ps)) |
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391 | & ) |
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392 | & )**rcp |
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393 | |
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394 | ENDDO !of n=1,n_out |
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395 | |
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396 | !------------------------------------------------------------------------ |
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397 | !------------------------------------------------------------------------ |
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398 | ! PART III : WSTAR COMPUTATION |
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399 | !------------------------------------------------------------------------ |
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400 | !------------------------------------------------------------------------ |
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401 | |
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402 | ! Detection of the mixed-layer potential temperature |
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403 | ! ------------ |
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404 | |
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405 | ! Nearest index for the pbl height |
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406 | |
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407 | IF (calltherm) THEN |
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408 | |
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409 | pbl_height_index(:)=1 |
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410 | |
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411 | DO k=1,nlay-1 |
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412 | DO ig=1, ngrid |
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413 | IF (abs(zmax(ig)-zzlay(ig,k)) .lt. |
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414 | & abs(zmax(ig)-zzlay(ig,pbl_height_index(ig)))) THEN |
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415 | pbl_height_index(ig)=k |
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416 | ENDIF |
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417 | ENDDO |
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418 | ENDDO |
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419 | |
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420 | ! Potential temperature gradient |
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421 | |
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422 | dteta(:,nlay)=0. |
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423 | DO k=1,nlay-1 |
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424 | DO ig=1, ngrid |
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425 | dteta(ig,k) = (ph(ig,k+1)-ph(ig,k))/(zzlay(ig,k+1)-zzlay(ig,k)) |
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426 | ENDDO |
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427 | ENDDO |
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428 | |
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429 | ! Computation of the pbl mixed layer temperature |
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430 | |
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431 | DO ig=1, ngrid |
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432 | ii=MINLOC(abs(dteta(ig,1:pbl_height_index(ig)))) |
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433 | pbl_teta(ig) = ph(ig,ii(1)) |
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434 | ENDDO |
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435 | |
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436 | ! Recompute wstar |
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437 | ! We follow Spiga et. al 2010 (QJRMS) |
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438 | ! ------------ |
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439 | |
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440 | DO ig=1, ngrid |
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441 | IF (zmax(ig) .gt. 0.) THEN |
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442 | wstar(ig)=(pg*zmax(ig)*hfmax(ig)/pbl_teta(ig))**(1./3.) |
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443 | ELSE |
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444 | wstar(ig)=0. |
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445 | ENDIF |
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446 | ENDDO |
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447 | |
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448 | !------------------------------------------------------------------------ |
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449 | !------------------------------------------------------------------------ |
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450 | ! PART IV : VERTICAL_VELOCITY_VARIANCE/VERTICAL_TURBULENT_FLUX PROFILES |
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451 | !------------------------------------------------------------------------ |
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452 | !------------------------------------------------------------------------ |
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453 | |
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454 | ! We follow Spiga et. al 2010 (QJRMS) |
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455 | ! ------------ |
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456 | |
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457 | DO ig=1, ngrid |
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458 | IF (zmax(ig) .gt. 0.) THEN |
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459 | x(ig) = zout/zmax(ig) |
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460 | ELSE |
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461 | x(ig) = 999. |
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462 | ENDIF |
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463 | ENDDO |
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464 | |
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465 | DO ig=1, ngrid |
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466 | ! dimensionless vertical heat flux |
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467 | IF (x(ig) .le. 0.3) THEN |
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468 | dvhf(ig) = ((-3.85/log(x(ig)))+0.07*log(x(ig))) |
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469 | & *exp(-4.61*x(ig)) |
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470 | ELSEIF (x(ig) .le. 1.) THEN |
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471 | dvhf(ig) = -1.52*x(ig) + 1.24 |
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472 | ELSE |
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473 | dvhf(ig) = 0. |
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474 | ENDIF |
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475 | ! dimensionless vertical velocity variance |
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476 | IF (x(ig) .le. 1.) THEN |
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477 | dvvv(ig) = 2.05*(x(ig)**(2./3.))*(1.-0.64*x(ig))**2 |
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478 | ELSE |
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479 | dvvv(ig) = 0. |
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480 | ENDIF |
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481 | ENDDO |
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482 | |
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483 | vhf(:) = dvhf(:)*hfmax(:) |
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484 | vvv(:) = dvvv(:)*(wstar(:))**2 |
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485 | |
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486 | ENDIF ! of if calltherm |
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487 | |
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488 | call WRITEDIAGFI(ngrid,'rib_pbl', |
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489 | & 'Richardson in pbl parameter','m/s',2,rib) |
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490 | call WRITEDIAGFI(ngrid,'cdn_pbl', |
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491 | & 'neutral momentum coef','m/s',2,cdn) |
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492 | call WRITEDIAGFI(ngrid,'fm_pbl', |
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493 | & 'momentum stab function','m/s',2,fm) |
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494 | call WRITEDIAGFI(ngrid,'uv', |
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495 | & 'wind norm first layer','m/s',2,sqrt(zu2)) |
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496 | call WRITEDIAGFI(ngrid,'uvtrue', |
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497 | & 'wind norm first layer','m/s',2,sqrt(pu(:,1)**2+pv(:,1)**2)) |
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498 | call WRITEDIAGFI(ngrid,'chn_pbl', |
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499 | & 'neutral momentum coef','m/s',2,chn) |
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500 | call WRITEDIAGFI(ngrid,'fh_pbl', |
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501 | & 'momentum stab function','m/s',2,fh) |
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502 | call WRITEDIAGFI(ngrid,'B_pbl', |
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503 | & 'flottabilité','m/',2,(ph(:,1)-pts(:))/pts(:)) |
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504 | call WRITEDIAGFI(ngrid,'zot_pbl', |
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505 | & 'flottabilité','ms',2,pz0tcomp) |
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506 | call WRITEDIAGFI(ngrid,'zz1','flottabilité','m',2,zzlay(:,1)) |
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507 | |
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508 | RETURN |
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509 | END |
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