Changeset 5144 for LMDZ6/branches/Amaury_dev/libf/phylmd/aeropt.F90

Timestamp:

Jul 29, 2024, 11:01:04 PM (3 months ago)

Author:

abarral

Message:

Put YOMCST.h into modules

File:

• LMDZ6/branches/Amaury_dev/libf/phylmd/aeropt.F90 (modified) (7 diffs)

LMDZ6/branches/Amaury_dev/libf/phylmd/aeropt.F90

@@ -1 @@
-
 ! $Id$
 
 SUBROUTINE aeropt(pplay, paprs, t_seri, msulfate, rhcl, tau_ae, piz_ae, &
-    cg_ae, ai)
+        cg_ae, ai)
 
   USE dimphy
   USE lmdz_abort_physic, ONLY: abort_physic
+  USE lmdz_yomcst
+
   IMPLICIT NONE
-
-
-
-  include "YOMCST.h"
 
   ! Arguments:
 
-  REAL, INTENT (IN) :: paprs(klon, klev+1)
+  REAL, INTENT (IN) :: paprs(klon, klev + 1)
   REAL, INTENT (IN) :: pplay(klon, klev), t_seri(klon, klev)
   REAL, INTENT (IN) :: msulfate(klon, klev) ! masse sulfate ug SO4/m3  [ug/m^3]
@@ -28 +25 @@
   INTEGER i, k, inu
   INTEGER rh_num, nbre_rh
-  PARAMETER (nbre_rh=12)
+  PARAMETER (nbre_rh = 12)
   REAL rh_tab(nbre_rh)
   REAL rh_max, delta, rh
-  PARAMETER (rh_max=95.)
+  PARAMETER (rh_max = 95.)
   DATA rh_tab/0., 10., 20., 30., 40., 50., 60., 70., 80., 85., 90., 95./
   REAL zrho, zdz
@@ -39 +36 @@
   REAL alphasulfate
 
-  CHARACTER (LEN=20) :: modname = 'aeropt'
-  CHARACTER (LEN=80) :: abort_message
+  CHARACTER (LEN = 20) :: modname = 'aeropt'
+  CHARACTER (LEN = 80) :: abort_message
 
 
@@ -48 +45 @@
   REAL cg_aer(nbre_rh, 2)
   DATA alpha_aer/.500130E+01, .500130E+01, .500130E+01, .500130E+01, &
-    .500130E+01, .616710E+01, .826850E+01, .107687E+02, .136976E+02, &
-    .162972E+02, .211690E+02, .354833E+02, .139460E+01, .139460E+01, &
-    .139460E+01, .139460E+01, .139460E+01, .173910E+01, .244380E+01, &
-    .332320E+01, .440120E+01, .539570E+01, .734580E+01, .136038E+02/
+          .500130E+01, .616710E+01, .826850E+01, .107687E+02, .136976E+02, &
+          .162972E+02, .211690E+02, .354833E+02, .139460E+01, .139460E+01, &
+          .139460E+01, .139460E+01, .139460E+01, .173910E+01, .244380E+01, &
+          .332320E+01, .440120E+01, .539570E+01, .734580E+01, .136038E+02/
   DATA cg_aer/.619800E+00, .619800E+00, .619800E+00, .619800E+00, &
-    .619800E+00, .662700E+00, .682100E+00, .698500E+00, .712500E+00, &
-    .721800E+00, .734600E+00, .755800E+00, .545600E+00, .545600E+00, &
-    .545600E+00, .545600E+00, .545600E+00, .583700E+00, .607100E+00, &
-    .627700E+00, .645800E+00, .658400E+00, .676500E+00, .708500E+00/
+          .619800E+00, .662700E+00, .682100E+00, .698500E+00, .712500E+00, &
+          .721800E+00, .734600E+00, .755800E+00, .545600E+00, .545600E+00, &
+          .545600E+00, .545600E+00, .545600E+00, .583700E+00, .607100E+00, &
+          .627700E+00, .645800E+00, .658400E+00, .676500E+00, .708500E+00/
   DATA alpha_aer_sulfate/4.910, 4.910, 4.910, 4.910, 6.547, 7.373, 8.373, &
-    9.788, 12.167, 14.256, 17.924, 28.433, 1.453, 1.453, 1.453, 1.453, 2.003, &
-    2.321, 2.711, 3.282, 4.287, 5.210, 6.914, 12.305, 4.308, 4.308, 4.308, &
-    4.308, 5.753, 6.521, 7.449, 8.772, 11.014, 12.999, 16.518, 26.772, 3.265, &
-    3.265, 3.265, 3.265, 4.388, 5.016, 5.775, 6.868, 8.745, 10.429, 13.457, &
-    22.538, 2.116, 2.116, 2.116, 2.116, 2.882, 3.330, 3.876, 4.670, 6.059, &
-    7.327, 9.650, 16.883/
+          9.788, 12.167, 14.256, 17.924, 28.433, 1.453, 1.453, 1.453, 1.453, 2.003, &
+          2.321, 2.711, 3.282, 4.287, 5.210, 6.914, 12.305, 4.308, 4.308, 4.308, &
+          4.308, 5.753, 6.521, 7.449, 8.772, 11.014, 12.999, 16.518, 26.772, 3.265, &
+          3.265, 3.265, 3.265, 4.388, 5.016, 5.775, 6.868, 8.745, 10.429, 13.457, &
+          22.538, 2.116, 2.116, 2.116, 2.116, 2.882, 3.330, 3.876, 4.670, 6.059, &
+          7.327, 9.650, 16.883/
 
   DO i = 1, klon
@@ -72 +69 @@
   DO k = 1, klev
     DO i = 1, klon
-      IF (t_seri(i,k)==0) WRITE (*, *) 'aeropt T ', i, k, t_seri(i, k)
-      IF (pplay(i,k)==0) WRITE (*, *) 'aeropt p ', i, k, pplay(i, k)
-      zrho = pplay(i, k)/t_seri(i, k)/rd ! kg/m3
-      zdz = (paprs(i,k)-paprs(i,k+1))/zrho/rg ! m
-      rh = min(rhcl(i,k)*100., rh_max)
-      rh_num = int(rh/10.+1.)
+      IF (t_seri(i, k)==0) WRITE (*, *) 'aeropt T ', i, k, t_seri(i, k)
+      IF (pplay(i, k)==0) WRITE (*, *) 'aeropt p ', i, k, pplay(i, k)
+      zrho = pplay(i, k) / t_seri(i, k) / rd ! kg/m3
+      zdz = (paprs(i, k) - paprs(i, k + 1)) / zrho / rg ! m
+      rh = min(rhcl(i, k) * 100., rh_max)
+      rh_num = int(rh / 10. + 1.)
       IF (rh<0.) THEN
         abort_message = 'aeropt: RH < 0 not possible'
@@ -84 +81 @@
       IF (rh>85.) rh_num = 10
       IF (rh>90.) rh_num = 11
-      delta = (rh-rh_tab(rh_num))/(rh_tab(rh_num+1)-rh_tab(rh_num))
+      delta = (rh - rh_tab(rh_num)) / (rh_tab(rh_num + 1) - rh_tab(rh_num))
 
       inu = 1
-      tau_ae(i, k, inu) = alpha_aer(rh_num, inu) + delta*(alpha_aer(rh_num+1, &
-        inu)-alpha_aer(rh_num,inu))
-      tau_ae(i, k, inu) = tau_ae(i, k, inu)*msulfate(i, k)*zdz*1.E-6
+      tau_ae(i, k, inu) = alpha_aer(rh_num, inu) + delta * (alpha_aer(rh_num + 1, &
+              inu) - alpha_aer(rh_num, inu))
+      tau_ae(i, k, inu) = tau_ae(i, k, inu) * msulfate(i, k) * zdz * 1.E-6
       piz_ae(i, k, inu) = 1.0
-      cg_ae(i, k, inu) = cg_aer(rh_num, inu) + delta*(cg_aer(rh_num+1,inu)- &
-        cg_aer(rh_num,inu))
+      cg_ae(i, k, inu) = cg_aer(rh_num, inu) + delta * (cg_aer(rh_num + 1, inu) - &
+              cg_aer(rh_num, inu))
 
       inu = 2
-      tau_ae(i, k, inu) = alpha_aer(rh_num, inu) + delta*(alpha_aer(rh_num+1, &
-        inu)-alpha_aer(rh_num,inu))
-      tau_ae(i, k, inu) = tau_ae(i, k, inu)*msulfate(i, k)*zdz*1.E-6
+      tau_ae(i, k, inu) = alpha_aer(rh_num, inu) + delta * (alpha_aer(rh_num + 1, &
+              inu) - alpha_aer(rh_num, inu))
+      tau_ae(i, k, inu) = tau_ae(i, k, inu) * msulfate(i, k) * zdz * 1.E-6
       piz_ae(i, k, inu) = 1.0
-      cg_ae(i, k, inu) = cg_aer(rh_num, inu) + delta*(cg_aer(rh_num+1,inu)- &
-        cg_aer(rh_num,inu))
+      cg_ae(i, k, inu) = cg_aer(rh_num, inu) + delta * (cg_aer(rh_num + 1, inu) - &
+              cg_aer(rh_num, inu))
       ! jq
       ! jq for aerosol index
 
       alphasulfate = alpha_aer_sulfate(rh_num, 4) + &
-        delta*(alpha_aer_sulfate(rh_num+1,4)-alpha_aer_sulfate(rh_num,4)) !--m2/g
+              delta * (alpha_aer_sulfate(rh_num + 1, 4) - alpha_aer_sulfate(rh_num, 4)) !--m2/g
 
-      taue670(i) = taue670(i) + alphasulfate*msulfate(i, k)*zdz*1.E-6
+      taue670(i) = taue670(i) + alphasulfate * msulfate(i, k) * zdz * 1.E-6
 
       alphasulfate = alpha_aer_sulfate(rh_num, 5) + &
-        delta*(alpha_aer_sulfate(rh_num+1,5)-alpha_aer_sulfate(rh_num,5)) !--m2/g
+              delta * (alpha_aer_sulfate(rh_num + 1, 5) - alpha_aer_sulfate(rh_num, 5)) !--m2/g
 
-      taue865(i) = taue865(i) + alphasulfate*msulfate(i, k)*zdz*1.E-6
+      taue865(i) = taue865(i) + alphasulfate * msulfate(i, k) * zdz * 1.E-6
 
     END DO
@@ -118 +115 @@
 
   DO i = 1, klon
-    ai(i) = (-log(max(taue670(i),0.0001)/max(taue865(i), &
-      0.0001))/log(670./865.))*taue865(i)
+    ai(i) = (-log(max(taue670(i), 0.0001) / max(taue865(i), &
+            0.0001)) / log(670. / 865.)) * taue865(i)
   END DO
 
-
 END SUBROUTINE aeropt