source: LMDZ6/trunk/libf/phylmd/climb_wind_mod.f90 @ 5291

Last change on this file since 5291 was 5285, checked in by abarral, 9 months ago

As discussed internally, remove generic ONLY: ... for new _mod_h modules
  • Property copyright set to
    Name of program: LMDZ
    Creation date: 1984
    Version: LMDZ5
    License: CeCILL version 2
    Holder: Laboratoire de m\'et\'eorologie dynamique, CNRS, UMR 8539
    See the license file in the root directory
  • Property svn:eol-style set to native
  • Property svn:keywords set to Author Date Id Revision
File size: 13.1 KB
Line 
1!
2MODULE climb_wind_mod
3!
4! Module to solve the verctical diffusion of the wind components "u" and "v".
5!
6  USE dimphy
7
8  IMPLICIT NONE
9
10  SAVE
11  PRIVATE
12 
13  REAL, DIMENSION(:),   ALLOCATABLE  :: alf1, alf2
14  !$OMP THREADPRIVATE(alf1,alf2)
15  REAL, DIMENSION(:,:), ALLOCATABLE  :: Kcoefm
16  !$OMP THREADPRIVATE(Kcoefm)
17  REAL, DIMENSION(:,:), ALLOCATABLE  :: Ccoef_U, Dcoef_U
18  !$OMP THREADPRIVATE(Ccoef_U, Dcoef_U)
19  REAL, DIMENSION(:,:), ALLOCATABLE  :: Ccoef_V, Dcoef_V
20  !$OMP THREADPRIVATE(Ccoef_V, Dcoef_V)
21  REAL, DIMENSION(:), ALLOCATABLE   :: Acoef_U, Bcoef_U
22  !$OMP THREADPRIVATE(Acoef_U, Bcoef_U)
23  REAL, DIMENSION(:), ALLOCATABLE   :: Acoef_V, Bcoef_V
24  !$OMP THREADPRIVATE(Acoef_V, Bcoef_V)
25  LOGICAL                            :: firstcall=.TRUE.
26  !$OMP THREADPRIVATE(firstcall)
27
28 
29  PUBLIC :: climb_wind_down, climb_wind_up
30
31CONTAINS
32!
33!****************************************************************************************
34!
35  SUBROUTINE climb_wind_init
36
37    INTEGER             :: ierr
38    CHARACTER(len = 20) :: modname = 'climb_wind_init'   
39
40!****************************************************************************************
41! Allocation of global module variables
42!
43!****************************************************************************************
44
45    ALLOCATE(alf1(klon), stat=ierr)
46    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocate alf1',1)
47
48    ALLOCATE(alf2(klon), stat=ierr)
49    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocate alf2',1)
50
51    ALLOCATE(Kcoefm(klon,klev), stat=ierr)
52    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocate Kcoefm',1)
53
54    ALLOCATE(Ccoef_U(klon,klev), stat=ierr)
55    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocate Ccoef_U',1)
56
57    ALLOCATE(Dcoef_U(klon,klev), stat=ierr)
58    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocation Dcoef_U',1)
59
60    ALLOCATE(Ccoef_V(klon,klev), stat=ierr)
61    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocation Ccoef_V',1)
62
63    ALLOCATE(Dcoef_V(klon,klev), stat=ierr)
64    IF (ierr /= 0) CALL abort_physic(modname,'Pb in allocation Dcoef_V',1)
65
66    ALLOCATE(Acoef_U(klon), Bcoef_U(klon), Acoef_V(klon), Bcoef_V(klon), STAT=ierr)
67    IF ( ierr /= 0 )  PRINT*,' pb in allloc Acoef_U and Bcoef_U, ierr=', ierr
68
69    firstcall=.FALSE.
70
71  END SUBROUTINE climb_wind_init
72!
73!****************************************************************************************
74!
75  SUBROUTINE climb_wind_down(knon, dtime, coef_in, pplay, paprs, temp, delp, u_old, v_old, &
76!!! nrlmd le 02/05/2011
77       Ccoef_U_out, Ccoef_V_out, Dcoef_U_out, Dcoef_V_out, &
78       Kcoef_m_out, alf_1_out, alf_2_out, &
79!!!
80       Acoef_U_out, Acoef_V_out, Bcoef_U_out, Bcoef_V_out)
81!
82! This routine calculates for the wind components u and v,
83! recursivly the coefficients C and D in equation
84! X(k) = C(k) + D(k)*X(k-1), X=[u,v], k=[1,klev] is the vertical layer.
85!
86!
87USE yomcst_mod_h
88! Input arguments
89!****************************************************************************************
90    INTEGER, INTENT(IN)                      :: knon
91    REAL, INTENT(IN)                         :: dtime
92    REAL, DIMENSION(klon,klev), INTENT(IN)   :: coef_in
93    REAL, DIMENSION(klon,klev), INTENT(IN)   :: pplay ! pres au milieu de couche (Pa)
94    REAL, DIMENSION(klon,klev+1), INTENT(IN) :: paprs ! pression a inter-couche (Pa)
95    REAL, DIMENSION(klon,klev), INTENT(IN)   :: temp  ! temperature
96    REAL, DIMENSION(klon,klev), INTENT(IN)   :: delp
97    REAL, DIMENSION(klon,klev), INTENT(IN)   :: u_old
98    REAL, DIMENSION(klon,klev), INTENT(IN)   :: v_old
99
100! Output arguments
101!****************************************************************************************
102    REAL, DIMENSION(klon), INTENT(OUT)       :: Acoef_U_out
103    REAL, DIMENSION(klon), INTENT(OUT)       :: Acoef_V_out
104    REAL, DIMENSION(klon), INTENT(OUT)       :: Bcoef_U_out
105    REAL, DIMENSION(klon), INTENT(OUT)       :: Bcoef_V_out
106
107!!! nrlmd le 02/05/2011
108    REAL, DIMENSION(klon,klev), INTENT(OUT)  :: Ccoef_U_out
109    REAL, DIMENSION(klon,klev), INTENT(OUT)  :: Ccoef_V_out
110    REAL, DIMENSION(klon,klev), INTENT(OUT)  :: Dcoef_U_out
111    REAL, DIMENSION(klon,klev), INTENT(OUT)  :: Dcoef_V_out
112    REAL, DIMENSION(klon,klev), INTENT(OUT)  :: Kcoef_m_out
113    REAL, DIMENSION(klon), INTENT(OUT)       :: alf_1_out
114    REAL, DIMENSION(klon), INTENT(OUT)       :: alf_2_out
115!!!
116
117! Local variables
118!****************************************************************************************
119    REAL, DIMENSION(klon)                    :: u1lay, v1lay
120    INTEGER                                  :: k, i
121
122! Include
123!****************************************************************************************
124    INCLUDE "compbl.h"
125
126!****************************************************************************************
127! Initialize module
128    IF (firstcall) CALL climb_wind_init
129
130!****************************************************************************************
131! Calculate the coefficients C and D in : u(k) = C(k) + D(k)*u(k-1)
132!
133!****************************************************************************************
134! - Define alpha (alf1 and alf2)
135    alf1(:) = 1.0
136    alf2(:) = 1.0 - alf1(:)
137
138! - Calculate the coefficients K
139    Kcoefm(:,:) = 0.0
140    DO k = 2, klev
141       DO i=1,knon
142          Kcoefm(i,k) = coef_in(i,k)*RG*RG*dtime/(pplay(i,k-1)-pplay(i,k)) &
143               *(paprs(i,k)*2/(temp(i,k)+temp(i,k-1))/RD)**2
144       END DO
145    END DO
146
147! - Calculate the coefficients C and D, component "u"
148    CALL calc_coef(knon, Kcoefm(:,:), delp(:,:), &
149         u_old(:,:), alf1(:), alf2(:),  &
150         Ccoef_U(:,:), Dcoef_U(:,:), Acoef_U(:), Bcoef_U(:))
151
152! - Calculate the coefficients C and D, component "v"
153    CALL calc_coef(knon, Kcoefm(:,:), delp(:,:), &
154         v_old(:,:), alf1(:), alf2(:),  &
155         Ccoef_V(:,:), Dcoef_V(:,:), Acoef_V(:), Bcoef_V(:))
156
157!****************************************************************************************
158! 6)
159! Return the first layer in output variables
160!
161!****************************************************************************************
162    Acoef_U_out = Acoef_U
163    Bcoef_U_out = Bcoef_U
164    Acoef_V_out = Acoef_V
165    Bcoef_V_out = Bcoef_V
166
167!****************************************************************************************
168! 7)
169! If Pbl is split, return also the other layers in output variables
170!
171!****************************************************************************************
172!!! jyg le 07/02/2012
173!!jyg       IF (mod(iflag_pbl_split,2) .eq.1) THEN
174       IF (mod(iflag_pbl_split,10) .ge.1) THEN
175!!! nrlmd le 02/05/2011
176    DO k= 1, klev
177      DO i= 1, klon
178        Ccoef_U_out(i,k) = Ccoef_U(i,k)
179        Ccoef_V_out(i,k) = Ccoef_V(i,k)
180        Dcoef_U_out(i,k) = Dcoef_U(i,k)
181        Dcoef_V_out(i,k) = Dcoef_V(i,k)
182        Kcoef_m_out(i,k) = Kcoefm(i,k)
183      ENDDO
184    ENDDO
185    DO i= 1, klon
186      alf_1_out(i)   = alf1(i)
187      alf_2_out(i)   = alf2(i)
188    ENDDO
189!!!     
190       ENDIF  ! (mod(iflag_pbl_split,2) .ge.1)
191!!!
192
193  END SUBROUTINE climb_wind_down
194!
195!****************************************************************************************
196!
197  SUBROUTINE calc_coef(knon, Kcoef, delp, X, alfa1, alfa2, Ccoef, Dcoef, Acoef, Bcoef)
198!
199! Find the coefficients C and D in fonction of alfa, K and delp
200USE yomcst_mod_h
201! Input arguments
202!****************************************************************************************
203    INTEGER, INTENT(IN)                      :: knon
204    REAL, DIMENSION(klon,klev), INTENT(IN)   :: Kcoef, delp
205    REAL, DIMENSION(klon,klev), INTENT(IN)   :: X
206    REAL, DIMENSION(klon), INTENT(IN)        :: alfa1, alfa2
207
208! Output arguments
209!****************************************************************************************
210    REAL, DIMENSION(klon), INTENT(OUT)       :: Acoef, Bcoef
211    REAL, DIMENSION(klon,klev), INTENT(OUT)  :: Ccoef, Dcoef
212 
213! local variables
214!****************************************************************************************
215    INTEGER                                  :: k, i
216    REAL                                     :: buf
217    !****************************************************************************************
218!
219
220! Calculate coefficients C and D at top level, k=klev
221!
222    Ccoef(:,:) = 0.0
223    Dcoef(:,:) = 0.0
224
225    DO i = 1, knon
226       buf = delp(i,klev) + Kcoef(i,klev)
227
228       Ccoef(i,klev) = X(i,klev)*delp(i,klev)/buf
229       Dcoef(i,klev) = Kcoef(i,klev)/buf
230    END DO
231   
232!
233! Calculate coefficients C and D at top level (klev-1) <= k <= 2
234!
235    DO k=(klev-1),2,-1
236       DO i = 1, knon
237          buf = delp(i,k) + Kcoef(i,k) + Kcoef(i,k+1)*(1.-Dcoef(i,k+1))
238         
239          Ccoef(i,k) = (X(i,k)*delp(i,k) + Kcoef(i,k+1)*Ccoef(i,k+1))/buf
240          Dcoef(i,k) = Kcoef(i,k)/buf
241       END DO
242    END DO
243
244!
245! Calculate coeffiecent A and B at surface
246!
247    DO i = 1, knon
248       buf = delp(i,1) + Kcoef(i,2)*(1-Dcoef(i,2))
249       Acoef(i) = (X(i,1)*delp(i,1) + Kcoef(i,2)*Ccoef(i,2))/buf
250       Bcoef(i) = -RG/buf
251    END DO
252
253  END SUBROUTINE calc_coef
254!
255!****************************************************************************************
256!
257
258  SUBROUTINE climb_wind_up(knon, dtime, u_old, v_old, flx_u1, flx_v1,  &
259!!! nrlmd le 02/05/2011
260       Acoef_U_in, Acoef_V_in, Bcoef_U_in, Bcoef_V_in, &
261       Ccoef_U_in, Ccoef_V_in, Dcoef_U_in, Dcoef_V_in, &
262       Kcoef_m_in, &
263!!!
264       flx_u_new, flx_v_new, d_u_new, d_v_new)
265!
266! Diffuse the wind components from the surface layer and up to the top layer.
267! Coefficents A, B, C and D are known from before. Start values for the diffusion are the
268! momentum fluxes at surface.
269!
270! u(k=1) = A + B*flx*dtime
271! u(k)   = C(k) + D(k)*u(k-1)  [2 <= k <= klev]
272!
273!****************************************************************************************
274USE yomcst_mod_h
275! Input arguments
276!****************************************************************************************
277    INTEGER, INTENT(IN)                     :: knon
278    REAL, INTENT(IN)                        :: dtime
279    REAL, DIMENSION(klon,klev), INTENT(IN)  :: u_old
280    REAL, DIMENSION(klon,klev), INTENT(IN)  :: v_old
281    REAL, DIMENSION(klon), INTENT(IN)       :: flx_u1, flx_v1 ! momentum flux
282
283!!! nrlmd le 02/05/2011
284    REAL, DIMENSION(klon), INTENT(IN)       :: Acoef_U_in,Acoef_V_in, Bcoef_U_in, Bcoef_V_in
285    REAL, DIMENSION(klon,klev), INTENT(IN)  :: Ccoef_U_in, Ccoef_V_in, Dcoef_U_in, Dcoef_V_in
286    REAL, DIMENSION(klon,klev), INTENT(IN)  :: Kcoef_m_in
287!!!
288
289! Output arguments
290!****************************************************************************************
291    REAL, DIMENSION(klon,klev), INTENT(OUT) :: flx_u_new, flx_v_new
292    REAL, DIMENSION(klon,klev), INTENT(OUT) :: d_u_new, d_v_new
293
294! Local variables
295!****************************************************************************************
296    REAL, DIMENSION(klon,klev)              :: u_new, v_new
297    INTEGER                                 :: k, i
298
299! Include
300!****************************************************************************************
301    INCLUDE "compbl.h"
302   
303!
304!****************************************************************************************
305
306!!! jyg le 07/02/2012
307!!jyg       IF (mod(iflag_pbl_split,2) .eq.1) THEN
308       IF (mod(iflag_pbl_split,10) .ge.1) THEN
309!!! nrlmd le 02/05/2011
310    DO i = 1, knon
311      Acoef_U(i)=Acoef_U_in(i)
312      Acoef_V(i)=Acoef_V_in(i)
313      Bcoef_U(i)=Bcoef_U_in(i)
314      Bcoef_V(i)=Bcoef_V_in(i)
315    ENDDO
316    DO k = 1, klev
317      DO i = 1, knon
318        Ccoef_U(i,k)=Ccoef_U_in(i,k)
319        Ccoef_V(i,k)=Ccoef_V_in(i,k)
320        Dcoef_U(i,k)=Dcoef_U_in(i,k)
321        Dcoef_V(i,k)=Dcoef_V_in(i,k)
322        Kcoefm(i,k)=Kcoef_m_in(i,k)
323      ENDDO
324    ENDDO
325!!!
326       ENDIF  ! (mod(iflag_pbl_split,2) .ge.1)
327!!!
328
329! Niveau 1
330    DO i = 1, knon
331       u_new(i,1) = Acoef_U(i) + Bcoef_U(i)*flx_u1(i)*dtime
332       v_new(i,1) = Acoef_V(i) + Bcoef_V(i)*flx_v1(i)*dtime
333    END DO
334
335! Niveau 2 jusqu'au sommet klev
336    DO k = 2, klev
337       DO i=1, knon
338          u_new(i,k) = Ccoef_U(i,k) + Dcoef_U(i,k) * u_new(i,k-1)
339          v_new(i,k) = Ccoef_V(i,k) + Dcoef_V(i,k) * v_new(i,k-1)
340       END DO
341    END DO
342
343!****************************************************************************************
344! Calcul flux
345!
346!== flux_u/v est le flux de moment angulaire (positif vers bas)
347!== dont l'unite est: (kg m/s)/(m**2 s)
348!
349!****************************************************************************************
350!
351    flx_u_new(:,:) = 0.0
352    flx_v_new(:,:) = 0.0
353
354    flx_u_new(1:knon,1)=flx_u1(1:knon)
355    flx_v_new(1:knon,1)=flx_v1(1:knon)
356
357! Niveau 2->klev
358    DO k = 2, klev
359       DO i = 1, knon
360          flx_u_new(i,k) = Kcoefm(i,k)/RG/dtime * &
361               (u_new(i,k)-u_new(i,k-1))
362         
363          flx_v_new(i,k) = Kcoefm(i,k)/RG/dtime * &
364               (v_new(i,k)-v_new(i,k-1))
365       END DO
366    END DO
367
368!****************************************************************************************
369! Calcul tendances
370!
371!****************************************************************************************
372    d_u_new(:,:) = 0.0
373    d_v_new(:,:) = 0.0
374    DO k = 1, klev
375       DO i = 1, knon
376          d_u_new(i,k) = u_new(i,k) - u_old(i,k)
377          d_v_new(i,k) = v_new(i,k) - v_old(i,k)
378       END DO
379    END DO
380
381  END SUBROUTINE climb_wind_up
382!
383!****************************************************************************************
384!
385END MODULE climb_wind_mod
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