<p><b>xylar@lanl.gov</b> 2010-11-16 15:06:26 -0700 (Tue, 16 Nov 2010)</p><p>BRANCH COMMIT<br>
<br>
copied core_sw to the core_land_ice (for future modification)<br>
</p><hr noshade><pre><font color="gray">Added: branches/land_ice/mpas/namelist.input.land_ice
===================================================================
--- branches/land_ice/mpas/namelist.input.land_ice         (rev 0)
+++ branches/land_ice/mpas/namelist.input.land_ice        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,28 @@
+&sw_model
+ config_test_case = 5
+ config_time_integration = 'RK4'
+ config_dt = 172.8
+ config_ntimesteps = 7500
+ config_output_interval = 500
+ config_stats_interval = 0
+ config_h_mom_eddy_visc2 = 0.0
+ config_h_mom_eddy_visc4 = 0.0
+ config_h_tracer_eddy_diff2 = 0.0
+ config_h_tracer_eddy_diff4 = 0.0
+ config_thickness_adv_order = 2
+ config_tracer_adv_order = 2
+ config_positive_definite = .false.
+ config_monotonic = .false.
+/
+
+&io
+ config_input_name = 'grid.nc'
+ config_output_name = 'output.nc'
+ config_restart_name = 'restart.nc'
+/
+
+&restart
+ config_restart_interval = 3000
+ config_do_restart = .false.
+ config_restart_time = 1036800.0
+/
Added: branches/land_ice/mpas/src/core_land_ice/Makefile
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/Makefile         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/Makefile        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,30 @@
+.SUFFIXES: .F .o
+
+OBJS =         module_mpas_core.o \
+ module_test_cases.o \
+        module_advection.o \
+        module_time_integration.o \
+        module_global_diagnostics.o
+
+all: core_sw
+
+core_sw: $(OBJS)
+        ar -ru libdycore.a $(OBJS)
+
+module_test_cases.o:
+
+module_advection.o:
+
+module_time_integration.o:
+
+module_global_diagnostics.o:
+
+module_mpas_core.o: module_global_diagnostics.o module_test_cases.o module_time_integration.o module_advection.o
+
+clean:
+        $(RM) *.o *.mod *.f90 libdycore.a
+
+.F.o:
+        $(RM) $@ $*.mod
+        $(CPP) $(CPPFLAGS) $(CPPINCLUDES) $< > $*.f90
+        $(FC) $(FFLAGS) -c $*.f90 $(FCINCLUDES) -I../framework -I../operators
Added: branches/land_ice/mpas/src/core_land_ice/Registry
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/Registry         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/Registry        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,147 @@
+#
+# namelist type namelist_record name default_value
+#
+namelist integer sw_model config_test_case 5
+namelist character sw_model config_time_integration RK4
+namelist real sw_model config_dt 172.8
+namelist integer sw_model config_ntimesteps 7500
+namelist integer sw_model config_output_interval 500
+namelist integer sw_model config_stats_interval 100
+namelist real sw_model config_h_mom_eddy_visc2 0.0
+namelist real sw_model config_h_mom_eddy_visc4 0.0
+namelist real sw_model config_h_tracer_eddy_diff2 0.0
+namelist real sw_model config_h_tracer_eddy_diff4 0.0
+namelist integer sw_model config_thickness_adv_order 2
+namelist integer sw_model config_tracer_adv_order 2
+namelist logical sw_model config_positive_definite false
+namelist logical sw_model config_monotonic false
+namelist real sw_model config_apvm_upwinding 0.5
+namelist character io config_input_name grid.nc
+namelist character io config_output_name output.nc
+namelist character io config_restart_name restart.nc
+namelist integer restart config_restart_interval 0
+namelist logical restart config_do_restart false
+namelist real restart config_restart_time 172800.0
+
+#
+# dim type name_in_file name_in_code
+#
+dim nCells nCells
+dim nEdges nEdges
+dim maxEdges maxEdges
+dim maxEdges2 maxEdges2
+dim nVertices nVertices
+dim TWO 2
+dim R3 3
+dim FIFTEEN 15
+dim TWENTYONE 21
+dim vertexDegree vertexDegree
+dim nVertLevels nVertLevels
+dim nTracers nTracers
+
+#
+# var persistence type name_in_file ( dims ) time_levs iro- name_in_code struct super-array array_class
+#
+var persistent real xtime ( Time ) 2 ro xtime state - -
+
+var persistent real latCell ( nCells ) 0 iro latCell mesh - -
+var persistent real lonCell ( nCells ) 0 iro lonCell mesh - -
+var persistent real xCell ( nCells ) 0 iro xCell mesh - -
+var persistent real yCell ( nCells ) 0 iro yCell mesh - -
+var persistent real zCell ( nCells ) 0 iro zCell mesh - -
+var persistent integer indexToCellID ( nCells ) 0 iro indexToCellID mesh - -
+
+var persistent real latEdge ( nEdges ) 0 iro latEdge mesh - -
+var persistent real lonEdge ( nEdges ) 0 iro lonEdge mesh - -
+var persistent real xEdge ( nEdges ) 0 iro xEdge mesh - -
+var persistent real yEdge ( nEdges ) 0 iro yEdge mesh - -
+var persistent real zEdge ( nEdges ) 0 iro zEdge mesh - -
+var persistent integer indexToEdgeID ( nEdges ) 0 iro indexToEdgeID mesh - -
+
+var persistent real latVertex ( nVertices ) 0 iro latVertex mesh - -
+var persistent real lonVertex ( nVertices ) 0 iro lonVertex mesh - -
+var persistent real xVertex ( nVertices ) 0 iro xVertex mesh - -
+var persistent real yVertex ( nVertices ) 0 iro yVertex mesh - -
+var persistent real zVertex ( nVertices ) 0 iro zVertex mesh - -
+var persistent integer indexToVertexID ( nVertices ) 0 iro indexToVertexID mesh - -
+
+var persistent integer cellsOnEdge ( TWO nEdges ) 0 iro cellsOnEdge mesh - -
+var persistent integer nEdgesOnCell ( nCells ) 0 iro nEdgesOnCell mesh - -
+var persistent integer nEdgesOnEdge ( nEdges ) 0 iro nEdgesOnEdge mesh - -
+var persistent integer edgesOnCell ( maxEdges nCells ) 0 iro edgesOnCell mesh - -
+var persistent integer edgesOnEdge ( maxEdges2 nEdges ) 0 iro edgesOnEdge mesh - -
+
+var persistent real weightsOnEdge ( maxEdges2 nEdges ) 0 iro weightsOnEdge mesh - -
+var persistent real dvEdge ( nEdges ) 0 iro dvEdge mesh - -
+var persistent real dcEdge ( nEdges ) 0 iro dcEdge mesh - -
+var persistent real angleEdge ( nEdges ) 0 iro angleEdge mesh - -
+var persistent real areaCell ( nCells ) 0 iro areaCell mesh - -
+var persistent real areaTriangle ( nVertices ) 0 iro areaTriangle mesh - -
+
+var persistent real edgeNormalVectors ( R3 nEdges ) 0 o edgeNormalVectors mesh - -
+var persistent real localVerticalUnitVectors ( R3 nCells ) 0 o localVerticalUnitVectors mesh - -
+var persistent real cellTangentPlane ( R3 TWO nEdges ) 0 o cellTangentPlane mesh - -
+
+var persistent integer cellsOnCell ( maxEdges nCells ) 0 iro cellsOnCell mesh - -
+var persistent integer verticesOnCell ( maxEdges nCells ) 0 iro verticesOnCell mesh - -
+var persistent integer verticesOnEdge ( TWO nEdges ) 0 iro verticesOnEdge mesh - -
+var persistent integer edgesOnVertex ( vertexDegree nVertices ) 0 iro edgesOnVertex mesh - -
+var persistent integer cellsOnVertex ( vertexDegree nVertices ) 0 iro cellsOnVertex mesh - -
+var persistent real kiteAreasOnVertex ( vertexDegree nVertices ) 0 iro kiteAreasOnVertex mesh - -
+var persistent real fEdge ( nEdges ) 0 iro fEdge mesh - -
+var persistent real fVertex ( nVertices ) 0 iro fVertex mesh - -
+var persistent real fCell ( nCells ) 0 iro fCell mesh - -
+var persistent real h_s ( nCells ) 0 iro h_s mesh - -
+
+# Space needed for advection
+var persistent real deriv_two ( FIFTEEN TWO nEdges ) 0 o deriv_two mesh - -
+var persistent integer advCells ( TWENTYONE nCells ) 0 - advCells mesh - -
+
+# !! NOTE: the following arrays are needed to allow the use
+# !! of the module_advection.F w/o alteration
+# Space needed for deformation calculation weights
+var persistent real defc_a ( maxEdges nCells ) 0 - defc_a mesh - -
+var persistent real defc_b ( maxEdges nCells ) 0 - defc_b mesh - -
+var persistent real kdiff ( nVertLevels nCells Time ) 0 - kdiff mesh - -
+
+# Arrays required for reconstruction of velocity field
+var persistent real coeffs_reconstruct ( R3 maxEdges nCells ) 0 - coeffs_reconstruct mesh - -
+
+# Boundary conditions: read from input, saved in restart and written to output
+var persistent integer boundaryEdge ( nVertLevels nEdges ) 0 iro boundaryEdge mesh - -
+var persistent integer boundaryVertex ( nVertLevels nVertices ) 0 iro boundaryVertex mesh - -
+var persistent integer boundaryCell ( nVertLevels nCells ) 0 iro boundaryCell mesh - -
+
+# Prognostic variables: read from input, saved in restart, and written to output
+var persistent real u ( nVertLevels nEdges Time ) 2 iro u state - -
+var persistent real h ( nVertLevels nCells Time ) 2 iro h state - -
+var persistent real tracers ( nTracers nVertLevels nCells Time ) 2 iro tracers state - -
+
+# Tendency variables
+var persistent real tend_u ( nVertLevels nEdges Time ) 1 - u tend - -
+var persistent real tend_h ( nVertLevels nCells Time ) 1 - h tend - -
+var persistent real tend_tracers ( nTracers nVertLevels nCells Time ) 1 - tracers tend - -
+
+# Diagnostic fields: only written to output
+var persistent real v ( nVertLevels nEdges Time ) 2 o v state - -
+var persistent real divergence ( nVertLevels nCells Time ) 2 o divergence state - -
+var persistent real vorticity ( nVertLevels nVertices Time ) 2 o vorticity state - -
+var persistent real vorticity_cell ( nVertLevels nCells Time ) 2 o vorticity_cell state - -
+var persistent real pv_edge ( nVertLevels nEdges Time ) 2 o pv_edge state - -
+var persistent real h_edge ( nVertLevels nEdges Time ) 2 o h_edge state - -
+var persistent real ke ( nVertLevels nCells Time ) 2 o ke state - -
+var persistent real pv_vertex ( nVertLevels nVertices Time ) 2 o pv_vertex state - -
+var persistent real pv_cell ( nVertLevels nCells Time ) 2 o pv_cell state - -
+var persistent real uReconstructX ( nVertLevels nCells Time ) 2 o uReconstructX state - -
+var persistent real uReconstructY ( nVertLevels nCells Time ) 2 o uReconstructY state - -
+var persistent real uReconstructZ ( nVertLevels nCells Time ) 2 o uReconstructZ state - -
+var persistent real uReconstructZonal ( nVertLevels nCells Time ) 2 o uReconstructZonal state - -
+var persistent real uReconstructMeridional ( nVertLevels nCells Time ) 2 o uReconstructMeridional state - -
+
+# Other diagnostic variables: neither read nor written to any files
+var persistent real vh ( nVertLevels nEdges Time ) 2 - vh state - -
+var persistent real circulation ( nVertLevels nVertices Time ) 2 - circulation state - -
+var persistent real gradPVt ( nVertLevels nEdges Time ) 2 - gradPVt state - -
+var persistent real gradPVn ( nVertLevels nEdges Time ) 2 - gradPVn state - -
+var persistent real        h_vertex ( nVertLevels nVertices Time ) 2 - h_vertex state - -
+
Added: branches/land_ice/mpas/src/core_land_ice/module_advection.F
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/module_advection.F         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/module_advection.F        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,933 @@
+module advection
+
+ use grid_types
+ use configure
+ use constants
+
+
+ contains
+
+
+ subroutine initialize_advection_rk( grid )
+
+!
+! compute the cell coefficients for the polynomial fit.
+! this is performed during setup for model integration.
+! WCS, 31 August 2009
+!
+ implicit none
+
+ type (mesh_type), intent(in) :: grid
+
+ real (kind=RKIND), dimension(:,:,:), pointer :: deriv_two
+ integer, dimension(:,:), pointer :: advCells
+
+! local variables
+
+ real (kind=RKIND), dimension(2, grid % nEdges) :: thetae
+ real (kind=RKIND), dimension(grid % nEdges) :: xe, ye
+ real (kind=RKIND), dimension(grid % nCells) :: theta_abs
+
+ real (kind=RKIND), dimension(25) :: xc, yc, zc ! cell center coordinates
+ real (kind=RKIND), dimension(25) :: thetav, thetat, dl_sphere
+ real (kind=RKIND) :: xm, ym, zm, dl, xec, yec, zec
+ real (kind=RKIND) :: thetae_tmp, xe_tmp, ye_tmp
+ real (kind=RKIND) :: xv1, xv2, yv1, yv2, zv1, zv2
+ integer :: i, j, k, ip1, ip2, m, n, ip1a, ii
+ integer :: iCell, iEdge
+ real (kind=RKIND) :: pii
+ real (kind=RKIND) :: x0, y0, x1, y1, x2, y2, x3, y3, x4, y4, x5, y5
+ real (kind=RKIND) :: pdx1, pdx2, pdx3, pdy1, pdy2, pdy3, dx1, dx2, dy1, dy2
+ real (kind=RKIND) :: angv1, angv2, dl1, dl2
+ real (kind=RKIND), dimension(25) :: dxe, dye, x2v, y2v, xp, yp
+
+ real (kind=RKIND) :: amatrix(25,25), bmatrix(25,25), wmatrix(25,25)
+ real (kind=RKIND) :: length_scale
+ integer :: ma,na, cell_add, mw, nn
+ integer, dimension(25) :: cell_list
+
+
+ integer :: cell1, cell2
+ integer, parameter :: polynomial_order = 2
+! logical, parameter :: debug = .true.
+ logical, parameter :: debug = .false.
+! logical, parameter :: least_squares = .false.
+ logical, parameter :: least_squares = .true.
+ logical :: add_the_cell, do_the_cell
+
+ logical, parameter :: reset_poly = .true.
+
+ real (kind=RKIND) :: rcell, cos2t, costsint, sin2t
+ real (kind=RKIND), dimension(grid%maxEdges) :: angle_2d
+
+!---
+
+ pii = 2.*asin(1.0)
+
+ advCells => grid % advCells % array
+ deriv_two => grid % deriv_two % array
+ deriv_two(:,:,:) = 0.
+
+ do iCell = 1, grid % nCells ! is this correct? - we need first halo cell also...
+
+ cell_list(1) = iCell
+ do i=2, grid % nEdgesOnCell % array(iCell)+1
+ cell_list(i) = grid % CellsOnCell % array(i-1,iCell)
+ end do
+ n = grid % nEdgesOnCell % array(iCell) + 1
+
+ if ( polynomial_order > 2 ) then
+ do i=2,grid % nEdgesOnCell % array(iCell) + 1
+ do j=1,grid % nEdgesOnCell % array ( cell_list(i) )
+ cell_add = grid % CellsOnCell % array (j,cell_list(i))
+ add_the_cell = .true.
+ do k=1,n
+ if ( cell_add == cell_list(k) ) add_the_cell = .false.
+ end do
+ if (add_the_cell) then
+ n = n+1
+ cell_list(n) = cell_add
+ end if
+ end do
+ end do
+ end if
+
+ advCells(1,iCell) = n
+
+! check to see if we are reaching outside the halo
+
+ do_the_cell = .true.
+ do i=1,n
+ if (cell_list(i) > grid % nCells) do_the_cell = .false.
+ end do
+
+
+ if ( .not. do_the_cell ) cycle
+
+
+! compute poynomial fit for this cell if all needed neighbors exist
+ if ( grid % on_a_sphere ) then
+
+ do i=1,n
+ advCells(i+1,iCell) = cell_list(i)
+ xc(i) = grid % xCell % array(advCells(i+1,iCell))/a
+ yc(i) = grid % yCell % array(advCells(i+1,iCell))/a
+ zc(i) = grid % zCell % array(advCells(i+1,iCell))/a
+ end do
+
+ theta_abs(iCell) = pii/2. - sphere_angle( xc(1), yc(1), zc(1), &
+ xc(2), yc(2), zc(2), &
+ 0., 0., 1. )
+
+! angles from cell center to neighbor centers (thetav)
+
+ do i=1,n-1
+
+ ip2 = i+2
+ if (ip2 > n) ip2 = 2
+
+ thetav(i) = sphere_angle( xc(1), yc(1), zc(1), &
+ xc(i+1), yc(i+1), zc(i+1), &
+ xc(ip2), yc(ip2), zc(ip2) )
+
+ dl_sphere(i) = a*arc_length( xc(1), yc(1), zc(1), &
+ xc(i+1), yc(i+1), zc(i+1) )
+ end do
+
+ length_scale = 1.
+ do i=1,n-1
+ dl_sphere(i) = dl_sphere(i)/length_scale
+ end do
+
+! thetat(1) = 0. ! this defines the x direction, cell center 1 ->
+ thetat(1) = theta_abs(iCell) ! this defines the x direction, longitude line
+ do i=2,n-1
+ thetat(i) = thetat(i-1) + thetav(i-1)
+ end do
+
+ do i=1,n-1
+ xp(i) = cos(thetat(i)) * dl_sphere(i)
+ yp(i) = sin(thetat(i)) * dl_sphere(i)
+ end do
+
+ else ! On an x-y plane
+
+ do i=1,n-1
+
+ angle_2d(i) = grid%angleEdge%array(grid % EdgesOnCell % array(i,iCell))
+ iEdge = grid % EdgesOnCell % array(i,iCell)
+ if ( iCell .ne. grid % CellsOnEdge % array(1,iEdge)) &
+ angle_2d(i) = angle_2d(i) - pii
+
+! xp(i) = grid % xCell % array(cell_list(i)) - grid % xCell % array(iCell)
+! yp(i) = grid % yCell % array(cell_list(i)) - grid % yCell % array(iCell)
+
+ xp(i) = grid % dcEdge % array(grid % EdgesOnCell % array(i,iCell)) * cos(angle_2d(i))
+ yp(i) = grid % dcEdge % array(grid % EdgesOnCell % array(i,iCell)) * sin(angle_2d(i))
+
+ end do
+
+ end if
+
+
+ ma = n-1
+ mw = grid % nEdgesOnCell % array (iCell)
+
+ bmatrix = 0.
+ amatrix = 0.
+ wmatrix = 0.
+
+ if (polynomial_order == 2) then
+ na = 6
+ ma = ma+1
+
+ amatrix(1,1) = 1.
+ wmatrix(1,1) = 1.
+ do i=2,ma
+ amatrix(i,1) = 1.
+ amatrix(i,2) = xp(i-1)
+ amatrix(i,3) = yp(i-1)
+ amatrix(i,4) = xp(i-1)**2
+ amatrix(i,5) = xp(i-1) * yp(i-1)
+ amatrix(i,6) = yp(i-1)**2
+
+ wmatrix(i,i) = 1.
+ end do
+
+ else if (polynomial_order == 3) then
+ na = 10
+ ma = ma+1
+
+ amatrix(1,1) = 1.
+ wmatrix(1,1) = 1.
+ do i=2,ma
+ amatrix(i,1) = 1.
+ amatrix(i,2) = xp(i-1)
+ amatrix(i,3) = yp(i-1)
+
+ amatrix(i,4) = xp(i-1)**2
+ amatrix(i,5) = xp(i-1) * yp(i-1)
+ amatrix(i,6) = yp(i-1)**2
+
+ amatrix(i,7) = xp(i-1)**3
+ amatrix(i,8) = yp(i-1) * (xp(i-1)**2)
+ amatrix(i,9) = xp(i-1) * (yp(i-1)**2)
+ amatrix(i,10) = yp(i-1)**3
+
+ wmatrix(i,i) = 1.
+
+ end do
+
+ else
+ na = 15
+ ma = ma+1
+
+ amatrix(1,1) = 1.
+ wmatrix(1,1) = 1.
+ do i=2,ma
+ amatrix(i,1) = 1.
+ amatrix(i,2) = xp(i-1)
+ amatrix(i,3) = yp(i-1)
+
+ amatrix(i,4) = xp(i-1)**2
+ amatrix(i,5) = xp(i-1) * yp(i-1)
+ amatrix(i,6) = yp(i-1)**2
+
+ amatrix(i,7) = xp(i-1)**3
+ amatrix(i,8) = yp(i-1) * (xp(i-1)**2)
+ amatrix(i,9) = xp(i-1) * (yp(i-1)**2)
+ amatrix(i,10) = yp(i-1)**3
+
+ amatrix(i,11) = xp(i-1)**4
+ amatrix(i,12) = yp(i-1) * (xp(i-1)**3)
+ amatrix(i,13) = (xp(i-1)**2)*(yp(i-1)**2)
+ amatrix(i,14) = xp(i-1) * (yp(i-1)**3)
+ amatrix(i,15) = yp(i-1)**4
+
+ wmatrix(i,i) = 1.
+
+ end do
+
+ do i=1,mw
+ wmatrix(i,i) = 1.
+ end do
+
+ end if
+
+ call poly_fit_2( amatrix, bmatrix, wmatrix, ma, na, 25 )
+
+ do i=1,grid % nEdgesOnCell % array (iCell)
+ ip1 = i+1
+ if (ip1 > n-1) ip1 = 1
+
+ iEdge = grid % EdgesOnCell % array (i,iCell)
+ xv1 = grid % xVertex % array(grid % verticesOnEdge % array (1,iedge))/a
+ yv1 = grid % yVertex % array(grid % verticesOnEdge % array (1,iedge))/a
+ zv1 = grid % zVertex % array(grid % verticesOnEdge % array (1,iedge))/a
+ xv2 = grid % xVertex % array(grid % verticesOnEdge % array (2,iedge))/a
+ yv2 = grid % yVertex % array(grid % verticesOnEdge % array (2,iedge))/a
+ zv2 = grid % zVertex % array(grid % verticesOnEdge % array (2,iedge))/a
+
+ if ( grid % on_a_sphere ) then
+ call arc_bisect( xv1, yv1, zv1, &
+ xv2, yv2, zv2, &
+ xec, yec, zec )
+
+ thetae_tmp = sphere_angle( xc(1), yc(1), zc(1), &
+ xc(i+1), yc(i+1), zc(i+1), &
+ xec, yec, zec )
+ thetae_tmp = thetae_tmp + thetat(i)
+ if (iCell == grid % cellsOnEdge % array(1,iEdge)) then
+ thetae(1,grid % EdgesOnCell % array (i,iCell)) = thetae_tmp
+ else
+ thetae(2,grid % EdgesOnCell % array (i,iCell)) = thetae_tmp
+ end if
+! else
+!
+! xe(grid % EdgesOnCell % array (i,iCell)) = 0.5 * (xv1 + xv2)
+! ye(grid % EdgesOnCell % array (i,iCell)) = 0.5 * (yv1 + yv2)
+
+ end if
+
+ end do
+
+! fill second derivative stencil for rk advection
+
+ do i=1, grid % nEdgesOnCell % array (iCell)
+ iEdge = grid % EdgesOnCell % array (i,iCell)
+
+
+ if ( grid % on_a_sphere ) then
+ if (iCell == grid % cellsOnEdge % array(1,iEdge)) then
+
+ cos2t = cos(thetae(1,grid % EdgesOnCell % array (i,iCell)))
+ sin2t = sin(thetae(1,grid % EdgesOnCell % array (i,iCell)))
+ costsint = cos2t*sin2t
+ cos2t = cos2t**2
+ sin2t = sin2t**2
+
+ do j=1,n
+ deriv_two(j,1,iEdge) = 2.*cos2t*bmatrix(4,j) &
+ + 2.*costsint*bmatrix(5,j) &
+ + 2.*sin2t*bmatrix(6,j)
+ end do
+ else
+
+ cos2t = cos(thetae(2,grid % EdgesOnCell % array (i,iCell)))
+ sin2t = sin(thetae(2,grid % EdgesOnCell % array (i,iCell)))
+ costsint = cos2t*sin2t
+ cos2t = cos2t**2
+ sin2t = sin2t**2
+
+ do j=1,n
+ deriv_two(j,2,iEdge) = 2.*cos2t*bmatrix(4,j) &
+ + 2.*costsint*bmatrix(5,j) &
+ + 2.*sin2t*bmatrix(6,j)
+ end do
+ end if
+
+ else
+
+ cos2t = cos(angle_2d(i))
+ sin2t = sin(angle_2d(i))
+ costsint = cos2t*sin2t
+ cos2t = cos2t**2
+ sin2t = sin2t**2
+
+! do j=1,n
+!
+! deriv_two(j,1,iEdge) = 2.*xe(iEdge)*xe(iEdge)*bmatrix(4,j) &
+! + 2.*xe(iEdge)*ye(iEdge)*bmatrix(5,j) &
+! + 2.*ye(iEdge)*ye(iEdge)*bmatrix(6,j)
+! end do
+
+ if (iCell == grid % cellsOnEdge % array(1,iEdge)) then
+ do j=1,n
+ deriv_two(j,1,iEdge) = 2.*cos2t*bmatrix(4,j) &
+ + 2.*costsint*bmatrix(5,j) &
+ + 2.*sin2t*bmatrix(6,j)
+ end do
+ else
+ do j=1,n
+ deriv_two(j,2,iEdge) = 2.*cos2t*bmatrix(4,j) &
+ + 2.*costsint*bmatrix(5,j) &
+ + 2.*sin2t*bmatrix(6,j)
+ end do
+ end if
+
+ end if
+ end do
+
+ end do ! end of loop over cells
+
+ if (debug) stop
+
+
+! write(0,*) ' check for deriv2 coefficients, iEdge 4 '
+!
+! iEdge = 4
+! j = 1
+! iCell = grid % cellsOnEdge % array(1,iEdge)
+! write(0,*) ' j, icell, coef ',j,iCell,deriv_two(j,1,iEdge)
+! do j=2,7
+! write(0,*) ' j, icell, coef ',j,grid % CellsOnCell % array(j-1,iCell),deriv_two(j,1,iEdge)
+! end do
+!
+! j = 1
+! iCell = grid % cellsOnEdge % array(2,iEdge)
+! write(0,*) ' j, icell, coef ',j,iCell,deriv_two(j,2,iEdge)
+! do j=2,7
+! write(0,*) ' j, icell, coef ',j,grid % CellsOnCell % array(j-1,iCell),deriv_two(j,2,iEdge)
+! end do
+! stop
+
+ end subroutine initialize_advection_rk
+
+
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! FUNCTION SPHERE_ANGLE
+ !
+ ! Computes the angle between arcs AB and AC, given points A, B, and C
+ ! Equation numbers w.r.t. http://mathworld.wolfram.com/SphericalTrigonometry.html
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ real function sphere_angle(ax, ay, az, bx, by, bz, cx, cy, cz)
+
+ implicit none
+
+ real (kind=RKIND), intent(in) :: ax, ay, az, bx, by, bz, cx, cy, cz
+
+ real (kind=RKIND) :: a, b, c ! Side lengths of spherical triangle ABC
+
+ real (kind=RKIND) :: ABx, ABy, ABz ! The components of the vector AB
+ real (kind=RKIND) :: mAB ! The magnitude of AB
+ real (kind=RKIND) :: ACx, ACy, ACz ! The components of the vector AC
+ real (kind=RKIND) :: mAC ! The magnitude of AC
+
+ real (kind=RKIND) :: Dx ! The i-components of the cross product AB x AC
+ real (kind=RKIND) :: Dy ! The j-components of the cross product AB x AC
+ real (kind=RKIND) :: Dz ! The k-components of the cross product AB x AC
+
+ real (kind=RKIND) :: s ! Semiperimeter of the triangle
+ real (kind=RKIND) :: sin_angle
+
+ a = acos(max(min(bx*cx + by*cy + bz*cz,1.0),-1.0)) ! Eqn. (3)
+ b = acos(max(min(ax*cx + ay*cy + az*cz,1.0),-1.0)) ! Eqn. (2)
+ c = acos(max(min(ax*bx + ay*by + az*bz,1.0),-1.0)) ! Eqn. (1)
+
+ ABx = bx - ax
+ ABy = by - ay
+ ABz = bz - az
+
+ ACx = cx - ax
+ ACy = cy - ay
+ ACz = cz - az
+
+ Dx = (ABy * ACz) - (ABz * ACy)
+ Dy = -((ABx * ACz) - (ABz * ACx))
+ Dz = (ABx * ACy) - (ABy * ACx)
+
+ s = 0.5*(a + b + c)
+! sin_angle = sqrt((sin(s-b)*sin(s-c))/(sin(b)*sin(c))) ! Eqn. (28)
+ sin_angle = sqrt(min(1.,max(0.,(sin(s-b)*sin(s-c))/(sin(b)*sin(c))))) ! Eqn. (28)
+
+ if ((Dx*ax + Dy*ay + Dz*az) >= 0.0) then
+ sphere_angle = 2.0 * asin(max(min(sin_angle,1.0),-1.0))
+ else
+ sphere_angle = -2.0 * asin(max(min(sin_angle,1.0),-1.0))
+ end if
+
+ end function sphere_angle
+
+
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! FUNCTION PLANE_ANGLE
+ !
+ ! Computes the angle between vectors AB and AC, given points A, B, and C, and
+ ! a vector (u,v,w) normal to the plane.
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ real function plane_angle(ax, ay, az, bx, by, bz, cx, cy, cz, u, v, w)
+
+ implicit none
+
+ real (kind=RKIND), intent(in) :: ax, ay, az, bx, by, bz, cx, cy, cz, u, v, w
+
+ real (kind=RKIND) :: ABx, ABy, ABz ! The components of the vector AB
+ real (kind=RKIND) :: mAB ! The magnitude of AB
+ real (kind=RKIND) :: ACx, ACy, ACz ! The components of the vector AC
+ real (kind=RKIND) :: mAC ! The magnitude of AC
+
+ real (kind=RKIND) :: Dx ! The i-components of the cross product AB x AC
+ real (kind=RKIND) :: Dy ! The j-components of the cross product AB x AC
+ real (kind=RKIND) :: Dz ! The k-components of the cross product AB x AC
+
+ real (kind=RKIND) :: cos_angle
+
+ ABx = bx - ax
+ ABy = by - ay
+ ABz = bz - az
+ mAB = sqrt(ABx**2.0 + ABy**2.0 + ABz**2.0)
+
+ ACx = cx - ax
+ ACy = cy - ay
+ ACz = cz - az
+ mAC = sqrt(ACx**2.0 + ACy**2.0 + ACz**2.0)
+
+
+ Dx = (ABy * ACz) - (ABz * ACy)
+ Dy = -((ABx * ACz) - (ABz * ACx))
+ Dz = (ABx * ACy) - (ABy * ACx)
+
+ cos_angle = (ABx*ACx + ABy*ACy + ABz*ACz) / (mAB * mAC)
+
+ if ((Dx*u + Dy*v + Dz*w) >= 0.0) then
+ plane_angle = acos(max(min(cos_angle,1.0),-1.0))
+ else
+ plane_angle = -acos(max(min(cos_angle,1.0),-1.0))
+ end if
+
+ end function plane_angle
+
+
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! FUNCTION ARC_LENGTH
+ !
+ ! Returns the length of the great circle arc from A=(ax, ay, az) to
+ ! B=(bx, by, bz). It is assumed that both A and B lie on the surface of the
+ ! same sphere centered at the origin.
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ real function arc_length(ax, ay, az, bx, by, bz)
+
+ implicit none
+
+ real (kind=RKIND), intent(in) :: ax, ay, az, bx, by, bz
+
+ real (kind=RKIND) :: r, c
+ real (kind=RKIND) :: cx, cy, cz
+
+ cx = bx - ax
+ cy = by - ay
+ cz = bz - az
+
+! r = ax*ax + ay*ay + az*az
+! c = cx*cx + cy*cy + cz*cz
+!
+! arc_length = sqrt(r) * acos(1.0 - c/(2.0*r))
+
+ r = sqrt(ax*ax + ay*ay + az*az)
+ c = sqrt(cx*cx + cy*cy + cz*cz)
+! arc_length = sqrt(r) * 2.0 * asin(c/(2.0*r))
+ arc_length = r * 2.0 * asin(c/(2.0*r))
+
+ end function arc_length
+
+
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! SUBROUTINE ARC_BISECT
+ !
+ ! Returns the point C=(cx, cy, cz) that bisects the great circle arc from
+ ! A=(ax, ay, az) to B=(bx, by, bz). It is assumed that A and B lie on the
+ ! surface of a sphere centered at the origin.
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ subroutine arc_bisect(ax, ay, az, bx, by, bz, cx, cy, cz)
+
+ implicit none
+
+ real (kind=RKIND), intent(in) :: ax, ay, az, bx, by, bz
+ real (kind=RKIND), intent(out) :: cx, cy, cz
+
+ real (kind=RKIND) :: r ! Radius of the sphere
+ real (kind=RKIND) :: d
+
+ r = sqrt(ax*ax + ay*ay + az*az)
+
+ cx = 0.5*(ax + bx)
+ cy = 0.5*(ay + by)
+ cz = 0.5*(az + bz)
+
+ if (cx == 0. .and. cy == 0. .and. cz == 0.) then
+ write(0,*) 'Error: arc_bisect: A and B are diametrically opposite'
+ else
+ d = sqrt(cx*cx + cy*cy + cz*cz)
+ cx = r * cx / d
+ cy = r * cy / d
+ cz = r * cz / d
+ end if
+
+ end subroutine arc_bisect
+
+
+ subroutine poly_fit_2(a_in,b_out,weights_in,m,n,ne)
+
+ implicit none
+
+ integer, intent(in) :: m,n,ne
+ real (kind=RKIND), dimension(ne,ne), intent(in) :: a_in, weights_in
+ real (kind=RKIND), dimension(ne,ne), intent(out) :: b_out
+
+ ! local storage
+
+ real (kind=RKIND), dimension(m,n) :: a
+ real (kind=RKIND), dimension(n,m) :: b
+ real (kind=RKIND), dimension(m,m) :: w,wt,h
+ real (kind=RKIND), dimension(n,m) :: at, ath
+ real (kind=RKIND), dimension(n,n) :: ata, ata_inv, atha, atha_inv
+ integer, dimension(n) :: indx
+ integer :: i,j
+
+ if ( (ne<n) .or. (ne<m) ) then
+ write(6,*) ' error in poly_fit_2 inversion ',m,n,ne
+ stop
+ end if
+
+! a(1:m,1:n) = a_in(1:n,1:m)
+ a(1:m,1:n) = a_in(1:m,1:n)
+ w(1:m,1:m) = weights_in(1:m,1:m)
+ b_out(:,:) = 0.
+
+ wt = transpose(w)
+ h = matmul(wt,w)
+ at = transpose(a)
+ ath = matmul(at,h)
+ atha = matmul(ath,a)
+
+ ata = matmul(at,a)
+
+! if (m == n) then
+! call migs(a,n,b,indx)
+! else
+
+ call migs(atha,n,atha_inv,indx)
+
+ b = matmul(atha_inv,ath)
+
+! call migs(ata,n,ata_inv,indx)
+! b = matmul(ata_inv,at)
+! end if
+ b_out(1:n,1:m) = b(1:n,1:m)
+
+! do i=1,n
+! write(6,*) ' i, indx ',i,indx(i)
+! end do
+!
+! write(6,*) ' '
+
+ end subroutine poly_fit_2
+
+
+! Updated 10/24/2001.
+!
+!!!!!!!!!!!!!!!!!!!!!!!!!!! Program 4.4 !!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+!
+!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+! !
+! Please Note: !
+! !
+! (1) This computer program is written by Tao Pang in conjunction with !
+! his book, "An Introduction to Computational Physics," published !
+! by Cambridge University Press in 1997. !
+! !
+! (2) No warranties, express or implied, are made for this program. !
+! !
+!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+!
+SUBROUTINE MIGS (A,N,X,INDX)
+!
+! Subroutine to invert matrix A(N,N) with the inverse stored
+! in X(N,N) in the output. Copyright (c) Tao Pang 2001.
+!
+ IMPLICIT NONE
+ INTEGER, INTENT (IN) :: N
+ INTEGER :: I,J,K
+ INTEGER, INTENT (OUT), DIMENSION (N) :: INDX
+ REAL (kind=RKIND), INTENT (INOUT), DIMENSION (N,N):: A
+ REAL (kind=RKIND), INTENT (OUT), DIMENSION (N,N):: X
+ REAL (kind=RKIND), DIMENSION (N,N) :: B
+!
+ DO I = 1, N
+ DO J = 1, N
+ B(I,J) = 0.0
+ END DO
+ END DO
+ DO I = 1, N
+ B(I,I) = 1.0
+ END DO
+!
+ CALL ELGS (A,N,INDX)
+!
+ DO I = 1, N-1
+ DO J = I+1, N
+ DO K = 1, N
+ B(INDX(J),K) = B(INDX(J),K)-A(INDX(J),I)*B(INDX(I),K)
+ END DO
+ END DO
+ END DO
+!
+ DO I = 1, N
+ X(N,I) = B(INDX(N),I)/A(INDX(N),N)
+ DO J = N-1, 1, -1
+ X(J,I) = B(INDX(J),I)
+ DO K = J+1, N
+ X(J,I) = X(J,I)-A(INDX(J),K)*X(K,I)
+ END DO
+ X(J,I) = X(J,I)/A(INDX(J),J)
+ END DO
+ END DO
+END SUBROUTINE MIGS
+
+
+SUBROUTINE ELGS (A,N,INDX)
+!
+! Subroutine to perform the partial-pivoting Gaussian elimination.
+! A(N,N) is the original matrix in the input and transformed matrix
+! plus the pivoting element ratios below the diagonal in the output.
+! INDX(N) records the pivoting order. Copyright (c) Tao Pang 2001.
+!
+ IMPLICIT NONE
+ INTEGER, INTENT (IN) :: N
+ INTEGER :: I,J,K,ITMP
+ INTEGER, INTENT (OUT), DIMENSION (N) :: INDX
+ REAL (kind=RKIND) :: C1,PI,PI1,PJ
+ REAL (kind=RKIND), INTENT (INOUT), DIMENSION (N,N) :: A
+ REAL (kind=RKIND), DIMENSION (N) :: C
+!
+! Initialize the index
+!
+ DO I = 1, N
+ INDX(I) = I
+ END DO
+!
+! Find the rescaling factors, one from each row
+!
+ DO I = 1, N
+ C1= 0.0
+ DO J = 1, N
+ C1 = MAX(C1,ABS(A(I,J)))
+ END DO
+ C(I) = C1
+ END DO
+!
+! Search the pivoting (largest) element from each column
+!
+ DO J = 1, N-1
+ PI1 = 0.0
+ DO I = J, N
+ PI = ABS(A(INDX(I),J))/C(INDX(I))
+ IF (PI.GT.PI1) THEN
+ PI1 = PI
+ K = I
+ ENDIF
+ END DO
+!
+! Interchange the rows via INDX(N) to record pivoting order
+!
+ ITMP = INDX(J)
+ INDX(J) = INDX(K)
+ INDX(K) = ITMP
+ DO I = J+1, N
+ PJ = A(INDX(I),J)/A(INDX(J),J)
+!
+! Record pivoting ratios below the diagonal
+!
+ A(INDX(I),J) = PJ
+!
+! Modify other elements accordingly
+!
+ DO K = J+1, N
+ A(INDX(I),K) = A(INDX(I),K)-PJ*A(INDX(J),K)
+ END DO
+ END DO
+ END DO
+!
+END SUBROUTINE ELGS
+
+!-------------------------------------------------------------
+
+ subroutine initialize_deformation_weights( grid )
+
+!
+! compute the cell coefficients for the deformation calculations
+! WCS, 13 July 2010
+!
+ implicit none
+
+ type (mesh_type), intent(in) :: grid
+
+ real (kind=RKIND), dimension(:,:), pointer :: defc_a, defc_b
+ integer, dimension(:,:), pointer :: cellsOnEdge, edgesOnCell
+
+! local variables
+
+ real (kind=RKIND), dimension(2, grid % nEdges) :: thetae
+ real (kind=RKIND), dimension(grid % nEdges) :: xe, ye
+ real (kind=RKIND), dimension(grid % nCells) :: theta_abs
+
+ real (kind=RKIND), dimension(25) :: xc, yc, zc ! cell center coordinates
+ real (kind=RKIND), dimension(25) :: thetav, thetat, dl_sphere
+ real (kind=RKIND) :: xm, ym, zm, dl, xec, yec, zec
+ real (kind=RKIND) :: thetae_tmp, xe_tmp, ye_tmp
+ real (kind=RKIND) :: xv1, xv2, yv1, yv2, zv1, zv2
+ integer :: i, j, k, ip1, ip2, m, n, ip1a, ii
+ integer :: iCell, iEdge
+ real (kind=RKIND) :: pii
+ real (kind=RKIND) :: x0, y0, x1, y1, x2, y2, x3, y3, x4, y4, x5, y5
+ real (kind=RKIND) :: pdx1, pdx2, pdx3, pdy1, pdy2, pdy3, dx1, dx2, dy1, dy2
+ real (kind=RKIND) :: angv1, angv2, dl1, dl2
+ real (kind=RKIND), dimension(25) :: dxe, dye, x2v, y2v, xp, yp, xpt, ypt
+
+ real (kind=RKIND) :: length_scale
+ integer :: ma,na, cell_add, mw, nn
+ integer, dimension(25) :: cell_list
+
+ integer :: cell1, cell2, iv
+ logical :: do_the_cell
+ real (kind=RKIND) :: area_cell, sint2, cost2, sint_cost, sumw1, sumw2, xptt, area_cellt
+
+ logical, parameter :: debug = .false.
+
+ if (debug) write(0,*) ' in def weight calc '
+
+ defc_a => grid % defc_a % array
+ defc_b => grid % defc_b % array
+ cellsOnEdge => grid % cellsOnEdge % array
+ edgesOnCell => grid % edgesOnCell % array
+
+ defc_a(:,:) = 0.
+ defc_b(:,:) = 0.
+
+ pii = 2.*asin(1.0)
+
+ if (debug) write(0,*) ' beginning cell loop '
+
+ do iCell = 1, grid % nCells
+
+ if (debug) write(0,*) ' cell loop ', iCell
+
+ cell_list(1) = iCell
+ do i=2, grid % nEdgesOnCell % array(iCell)+1
+ cell_list(i) = grid % CellsOnCell % array(i-1,iCell)
+ end do
+ n = grid % nEdgesOnCell % array(iCell) + 1
+
+! check to see if we are reaching outside the halo
+
+ if (debug) write(0,*) ' points ', n
+
+ do_the_cell = .true.
+ do i=1,n
+ if (cell_list(i) > grid % nCells) do_the_cell = .false.
+ end do
+
+
+ if (.not. do_the_cell) cycle
+
+
+! compute poynomial fit for this cell if all needed neighbors exist
+ if (grid % on_a_sphere) then
+
+ xc(1) = grid % xCell % array(iCell)/a
+ yc(1) = grid % yCell % array(iCell)/a
+ zc(1) = grid % zCell % array(iCell)/a
+
+
+ do i=2,n
+ iv = grid % verticesOnCell % array(i-1,iCell)
+ xc(i) = grid % xVertex % array(iv)/a
+ yc(i) = grid % yVertex % array(iv)/a
+ zc(i) = grid % zVertex % array(iv)/a
+ end do
+
+ theta_abs(iCell) = pii/2. - sphere_angle( xc(1), yc(1), zc(1), &
+ xc(2), yc(2), zc(2), &
+ 0., 0., 1. )
+
+! angles from cell center to neighbor centers (thetav)
+
+ do i=1,n-1
+
+ ip2 = i+2
+ if (ip2 > n) ip2 = 2
+
+ thetav(i) = sphere_angle( xc(1), yc(1), zc(1), &
+ xc(i+1), yc(i+1), zc(i+1), &
+ xc(ip2), yc(ip2), zc(ip2) )
+
+ dl_sphere(i) = a*arc_length( xc(1), yc(1), zc(1), &
+ xc(i+1), yc(i+1), zc(i+1) )
+ end do
+
+ length_scale = 1.
+ do i=1,n-1
+ dl_sphere(i) = dl_sphere(i)/length_scale
+ end do
+
+ thetat(1) = 0. ! this defines the x direction, cell center 1 ->
+! thetat(1) = theta_abs(iCell) ! this defines the x direction, longitude line
+ do i=2,n-1
+ thetat(i) = thetat(i-1) + thetav(i-1)
+ end do
+
+ do i=1,n-1
+ xp(i) = cos(thetat(i)) * dl_sphere(i)
+ yp(i) = sin(thetat(i)) * dl_sphere(i)
+ end do
+
+ else ! On an x-y plane
+
+ xp(1) = grid % xCell % array(iCell)
+ yp(1) = grid % yCell % array(iCell)
+
+
+ do i=2,n
+ iv = grid % verticesOnCell % array(i-1,iCell)
+ xp(i) = grid % xVertex % array(iv)
+ yp(i) = grid % yVertex % array(iv)
+ end do
+
+ end if
+
+! thetat(1) = 0.
+ thetat(1) = theta_abs(iCell)
+ do i=2,n-1
+ ip1 = i+1
+ if (ip1 == n) ip1 = 1
+ thetat(i) = plane_angle( 0.,0.,0., &
+ xp(i)-xp(i-1), yp(i)-yp(i-1), 0., &
+ xp(ip1)-xp(i), yp(ip1)-yp(i), 0., &
+ 0., 0., 1.)
+ thetat(i) = thetat(i) + thetat(i-1)
+ end do
+
+ area_cell = 0.
+ area_cellt = 0.
+ do i=1,n-1
+ ip1 = i+1
+ if (ip1 == n) ip1 = 1
+ dl = sqrt((xp(ip1)-xp(i))**2 + (yp(ip1)-yp(i))**2)
+ area_cell = area_cell + 0.25*(xp(i)+xp(ip1))*(yp(ip1)-yp(i)) - 0.25*(yp(i)+yp(ip1))*(xp(ip1)-xp(i))
+ area_cellt = area_cellt + (0.25*(xp(i)+xp(ip1))*cos(thetat(i)) + 0.25*(yp(i)+yp(ip1))*sin(thetat(i)))*dl
+ end do
+ if (debug) write(0,*) ' area_cell, area_cellt ',area_cell, area_cellt,area_cell-area_cellt
+
+ do i=1,n-1
+ ip1 = i+1
+ if (ip1 == n) ip1 = 1
+ dl = sqrt((xp(ip1)-xp(i))**2 + (yp(ip1)-yp(i))**2)
+ sint2 = (sin(thetat(i)))**2
+ cost2 = (cos(thetat(i)))**2
+ sint_cost = sin(thetat(i))*cos(thetat(i))
+ defc_a(i,iCell) = dl*(cost2 - sint2)/area_cell
+ defc_b(i,iCell) = dl*2.*sint_cost/area_cell
+ if (cellsOnEdge(1,EdgesOnCell(i,iCell)) /= iCell) then
+ defc_a(i,iCell) = - defc_a(i,iCell)
+ defc_b(i,iCell) = - defc_b(i,iCell)
+ end if
+
+ end do
+
+ end do
+
+ if (debug) write(0,*) ' exiting def weight calc '
+
+ end subroutine initialize_deformation_weights
+
+end module advection
Added: branches/land_ice/mpas/src/core_land_ice/module_global_diagnostics.F
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/module_global_diagnostics.F         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/module_global_diagnostics.F        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,384 @@
+module global_diagnostics
+
+ use grid_types
+ use configure
+ use constants
+ use dmpar
+
+ implicit none
+ save
+ public
+
+ contains
+
+ subroutine computeGlobalDiagnostics(dminfo, state, grid, timeIndex, dt)
+
+ ! Note: this routine assumes that there is only one block per processor. No looping
+ ! is preformed over blocks.
+ ! dminfo is the domain info needed for global communication
+ ! state contains the state variables needed to compute global diagnostics
+ ! grid conains the meta data about the grid
+ ! timeIndex is the current time step counter
+ ! dt is the duration of each time step
+
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! INSTRUCTIONS !
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! To add a new Diagnostic as a Global Stat, follow these steps.
+ ! 1. Define the array to integrate, and the variable for the value above.
+ ! 2. Allocate the array with the correct dimensions.
+ ! 3. Fill the array with the data to be integrated.
+ ! eg. GlobalFluidThickness = Sum(h dA)/Sum(dA), See below for array filling
+ ! 4. Call Function to compute Global Stat that you want.
+ ! 5. Finish computing the global stat/integral
+ ! 6. Write out your global stat to the file
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (dm_info), intent(in) :: dminfo
+ type (state_type), intent(inout) :: state
+ type (mesh_type), intent(in) :: grid
+ integer, intent(in) :: timeIndex
+ real (kind=RKIND), intent(in) :: dt
+
+ integer :: nVertLevels, nCellsSolve, nEdgesSolve, nVerticesSolve, nCellsGlobal, nEdgesGlobal, nVerticesGlobal, iTracer
+ integer :: nCells
+
+ ! Step 1
+ ! 1. Define the array to integrate, and the variable for the value to be stored in after the integration
+ real (kind=RKIND), dimension(:), pointer :: areaCell, dcEdge, dvEdge, areaTriangle, h_s, fCell, fEdge
+ real (kind=RKIND), dimension(:,:), pointer :: h, u, v, h_edge, pv_edge, pv_vertex, pv_cell, h_vertex, weightsOnEdge
+
+ real (kind=RKIND), dimension(:,:,:), pointer :: tracers
+
+ real (kind=RKIND), dimension(:), allocatable :: volumeWeightedPotentialEnergyReservoir, averageThickness
+ real (kind=RKIND), dimension(:), allocatable :: potentialEnstrophyReservior, areaEdge, h_s_edge
+
+ real (kind=RKIND), dimension(:,:), allocatable :: cellVolume, cellArea, volumeWeightedPotentialVorticity
+ real (kind=RKIND), dimension(:,:), allocatable :: volumeWeightedPotentialEnstrophy, vertexVolume, volumeWeightedKineticEnergy
+ real (kind=RKIND), dimension(:,:), allocatable :: volumeWeightedPotentialEnergy, volumeWeightedPotentialEnergyTopography
+ real (kind=RKIND), dimension(:,:), allocatable :: keTend_CoriolisForce, keTend_PressureGradient
+ real (kind=RKIND), dimension(:,:), allocatable ::peTend_DivThickness, refAreaWeightedSurfaceHeight, refAreaWeightedSurfaceHeight_edge
+
+ real (kind=RKIND) :: sumCellVolume, sumCellArea, sumVertexVolume, sumrefAreaWeightedSurfaceHeight
+
+ real (kind=RKIND) :: globalFluidThickness, globalPotentialVorticity, globalPotentialEnstrophy, globalEnergy
+ real (kind=RKIND) :: globalCoriolisEnergyTendency, globalKEPETendency, globalPotentialEnstrophyReservoir
+ real (kind=RKIND) :: globalKineticEnergy, globalPotentialEnergy, globalPotentialEnergyReservoir
+ real (kind=RKIND) :: globalKineticEnergyTendency, globalPotentialEnergyTendency
+ real (kind=RKIND) :: global_temp, workpv, q
+ real (kind=RKIND) :: volumeCellGlobal, volumeEdgeGlobal, CFLNumberGlobal
+
+ integer :: elementIndex, variableIndex, nVariables, nSums, nMaxes, nMins
+ integer :: timeLevel, eoe, iLevel, iCell, iEdge, iVertex
+ integer :: fileID, iCell1, iCell2, j
+
+ integer, dimension(:,:), pointer :: cellsOnEdge, edgesOnCell, edgesOnEdge
+ integer, dimension(:), pointer :: nEdgesOnEdge
+
+ cellsOnEdge => grid % cellsOnEdge % array
+ edgesOnCell => grid % edgesOnCell % array
+
+ nVertLevels = grid % nVertLevels
+ nCellsSolve = grid % nCellsSolve
+ nEdgesSolve = grid % nEdgesSolve
+ nVerticesSolve = grid % nVerticesSolve
+ nCells = grid % nCells
+
+ h_s => grid % h_s % array
+ areaCell => grid % areaCell % array
+ dcEdge => grid % dcEdge % array
+ dvEdge => grid % dvEdge % array
+ areaTriangle => grid % areaTriangle % array
+ fCell => grid % fCell % array
+ fEdge => grid % fEdge % array
+ edgesOnEdge => grid % edgesOnEdge % array
+ nEdgesOnEdge => grid % nEdgesOnEdge % array
+
+ allocate(areaEdge(1:nEdgesSolve))
+ areaEdge = dcEdge(1:nEdgesSolve)*dvEdge(1:nEdgesSolve)
+ weightsOnEdge => grid % weightsOnEdge % array
+
+ h => state % h % array
+ u => state % u % array
+ v => state % v % array
+ tracers => state % tracers % array
+ h_edge => state % h_edge % array
+ h_vertex => state % h_vertex % array
+ pv_edge => state % pv_edge % array
+ pv_vertex => state % pv_vertex % array
+ pv_cell => state % pv_cell % array
+
+ ! Step 2
+ ! 2. Allocate the array with the correct dimensions.
+ allocate(cellVolume(nVertLevels,nCellsSolve))
+ allocate(cellArea(nVertLevels,nCellsSolve))
+ allocate(refAreaWeightedSurfaceHeight(nVertLevels,nCellsSolve))
+ allocate(refAreaWeightedSurfaceHeight_edge(nVertLevels,nEdgesSolve))
+ allocate(volumeWeightedPotentialVorticity(nVertLevels,nVerticesSolve))
+ allocate(volumeWeightedPotentialEnstrophy(nVertLevels,nVerticesSolve))
+ allocate(potentialEnstrophyReservior(nCellsSolve))
+ allocate(vertexVolume(nVertLevels,nVerticesSolve))
+ allocate(volumeWeightedKineticEnergy(nVertLevels,nEdgesSolve))
+ allocate(volumeWeightedPotentialEnergy(nVertLevels,nCellsSolve))
+ allocate(volumeWeightedPotentialEnergyTopography(nVertLevels,nCellsSolve))
+ allocate(volumeWeightedPotentialEnergyReservoir(nCellsSolve))
+ allocate(keTend_CoriolisForce(nVertLevels,nEdgesSolve))
+ allocate(keTend_PressureGradient(nVertLevels,nEdgesSolve))
+ allocate(peTend_DivThickness(nVertLevels,nCells))
+
+ allocate(averageThickness(nCellsSolve))
+
+ allocate(h_s_edge(nEdgesSOlve))
+
+
+ cellVolume = 0
+ refAreaWeightedSurfaceHeight = 0
+ refAreaWeightedSurfaceHeight_edge = 0
+ vertexVolume = 0
+ cellArea = 0
+ averageThickness = 0
+ volumeWeightedPotentialVorticity = 0
+ volumeWeightedPotentialEnstrophy = 0
+ volumeWeightedKineticEnergy = 0
+ volumeWeightedPotentialEnergy = 0
+ volumeWeightedPotentialEnergyTopography = 0
+ volumeWeightedPotentialEnergyReservoir = 0
+ keTend_PressureGradient = 0
+ peTend_DivThickness = 0
+ keTend_CoriolisForce = 0
+ h_s_edge = 0
+
+ ! Build Arrays for Global Integrals
+ ! Step 3
+ ! 3. Fill the array with the data to be integrated.
+ ! eg. GlobalFluidThickness = Sum(h dA)/Sum(dA), See below for array filling
+ do iLevel = 1,nVertLevels
+ ! eg. GlobalFluidThickness top (Sum( h dA)) = Sum(cellVolume)
+ cellVolume(iLevel,:) = h(iLevel,1:nCellsSolve)*areaCell(1:nCellsSolve)
+ ! eg. GlobalFluidThickness bot (Sum(dA)) = Sum(cellArea)
+ cellArea(iLevel,:) = areaCell(1:nCellsSolve)
+ volumeWeightedPotentialVorticity(iLevel,:) = pv_vertex(iLevel,1:nVerticesSolve) &
+ *h_vertex(iLevel,1:nVerticesSolve)*areaTriangle(1:nVerticesSolve)
+ volumeWeightedPotentialEnstrophy(iLevel,:) = pv_vertex(iLevel,1:nVerticesSolve) &
+ *pv_vertex(iLevel,1:nVerticesSolve)*h_vertex(iLevel,1:nVerticesSolve)*areaTriangle(1:nVerticesSolve)
+ vertexVolume(iLevel,:) = h_vertex(iLevel,1:nVerticesSolve)*areaTriangle(1:nVerticesSolve)
+ volumeWeightedKineticEnergy(iLevel,:) = u(iLevel,1:nEdgesSolve)*u(iLevel,1:nEdgesSolve) &
+ *h_edge(iLevel,1:nEdgesSolve)*areaEdge(1:nEdgesSolve)*0.5
+ volumeWeightedPotentialEnergy(iLevel,:) = gravity*h(iLevel,1:nCellsSolve)*h(iLevel,1:nCellsSolve)*areaCell(1:nCellsSolve)*0.5
+ volumeWeightedPotentialEnergyTopography(iLevel,:) = gravity*h(iLevel,1:nCellsSolve)*h_s(1:nCellsSolve)*areaCell(1:nCellsSolve)
+ refAreaWeightedSurfaceHeight(iLevel,:) = areaCell(1:nCellsSolve)*(h(iLevel,1:nCellsSolve)+h_s(1:nCellsSolve))
+
+ do iEdge = 1,nEdgesSolve
+ q = 0.0
+ do j = 1,nEdgesOnEdge(iEdge)
+ eoe = edgesOnEdge(j,iEdge)
+ workpv = 0.5 * (pv_edge(iLevel,iEdge) + pv_edge(iLevel,eoe))
+ q = q + weightsOnEdge(j,iEdge) * u(iLevel,eoe) * workpv * h_edge(iLevel,eoe)
+ end do
+ keTend_CoriolisForce(iLevel,iEdge) = h_edge(iLevel,iEdge) * u(iLevel,iEdge) * q * areaEdge(iEdge)
+
+ iCell1 = cellsOnEdge(1,iEdge)
+ iCell2 = cellsOnEdge(2,iEdge)
+
+ refAreaWeightedSurfaceHeight_edge(iLevel,iEdge) = areaEdge(iEdge)*(h_edge(iLevel,iEdge) + 0.5*(h_s(iCell1) + h_s(iCell2)))
+
+ keTend_PressureGradient(iLevel,iEdge) = areaEdge(iEdge)*h_edge(iLevel,iEdge)*u(iLevel,iEdge) &
+ *gravity*(h(iLevel,iCell2)+h_s(iCell2) - h(iLevel,iCell1)-h_s(iCell1))/dcEdge(iEdge)
+ peTend_DivThickness(iLevel,iCell1) = peTend_DivThickness(iLevel,iCell1) &
+ + h_edge(iLevel,iEdge)*u(iLevel,iEdge)*dvEdge(iEdge)
+ peTend_DivThickness(iLevel,iCell2) = peTend_DivThickness(iLevel,iCell2) &
+ - h_edge(iLevel,iEdge)*u(iLevel,iEdge)*dvEdge(iEdge)
+ end do
+
+ peTend_DivThickness(iLevel,:) = peTend_DivThickness(iLevel,1:nCells)*gravity &
+ *(h(iLevel,1:nCells)+h_s(1:nCells))
+ end do
+
+ do iEdge = 1,nEdgesSolve
+ iCell1 = cellsOnEdge(1,iEdge)
+ iCell2 = cellsOnEdge(2,iEdge)
+
+ h_s_edge(iEdge) = 0.5*(h_s(iCell1) + h_s(iCell2))
+ end do
+
+ ! Step 4
+ ! 4. Call Function to compute Global Stat that you want.
+ ! Computing Kinetic and Potential Energy Tendency Terms
+ call computeGlobalSum(dminfo, nVertLevels, nEdgesSolve, keTend_PressureGradient, globalKineticEnergyTendency)
+ call computeGlobalSum(dminfo, nVertLevels, nCells, peTend_DivThickness, globalPotentialEnergyTendency)
+
+ ! Computing top and bottom of global mass integral
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, cellVolume, sumCellVolume)
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, cellArea, sumCellArea)
+
+ globalKineticEnergyTendency = globalKineticEnergyTendency / sumCellVolume
+ globalPotentialEnergyTendency = globalPotentialEnergyTendency / sumCellVolume
+
+ ! Step 5
+ ! 5. Finish computing the global stat/integral
+ globalFluidThickness = sumCellVolume/sumCellArea
+
+ ! Compute Average Sea Surface Height for Potential Energy and Enstrophy
+ ! Reservoir computations
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, refAreaWeightedSurfaceHeight, sumrefAreaWeightedSurfaceHeight)
+
+ averageThickness(:) = (sumrefAreaWeightedSurfaceHeight/sumCellArea)-h_s(1:nCellsSolve)
+
+ ! Compute Volume Weighted Averages of Potential Vorticity and Potential Enstrophy
+ call computeGlobalSum(dminfo, nVertLevels, nVerticesSolve, volumeWeightedPotentialVorticity, globalPotentialVorticity)
+ call computeGlobalSum(dminfo, nVertLevels, nVerticesSolve, volumeWeightedPotentialEnstrophy, globalPotentialEnstrophy)
+ call computeGlobalSum(dminfo, nVertLevels, nVerticesSolve, vertexVolume, sumVertexVolume)
+
+ globalPotentialVorticity = globalPotentialVorticity/sumVertexVolume
+ globalPotentialEnstrophy = globalPotentialEnstrophy/sumVertexVolume
+
+ ! Compte Potential Enstrophy Reservior
+ potentialEnstrophyReservior(:) = areaCell(:)*fCell(:)*fCell(:)/averageThickness
+ call computeGlobalSum(dminfo, 1, nCellsSolve, potentialEnstrophyReservior, globalPotentialEnstrophyReservoir)
+ globalPotentialEnstrophyReservoir = globalPotentialEnstrophyReservoir/sumCellVolume
+
+ globalPotentialEnstrophy = globalPotentialEnstrophy - globalPotentialEnstrophyReservoir
+
+ ! Compute Kinetic and Potential Energy terms to be combined into total energy
+ call computeGlobalSum(dminfo, nVertLevels, nEdgesSolve, volumeWeightedKineticEnergy, globalKineticEnergy)
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, volumeWeightedPotentialEnergy, globalPotentialEnergy)
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, volumeWeightedPotentialEnergyTopography, global_temp)
+
+ globalKineticEnergy = globalKineticEnergy/sumCellVolume
+ globalPotentialEnergy = (globalPotentialEnergy + global_temp)/sumCellVolume
+
+ ! Compute Potential energy reservoir to be subtracted from potential energy term
+ volumeWeightedPotentialEnergyReservoir(1:nCellsSolve) = areaCell(1:nCellsSolve)*averageThickness*averageThickness*gravity*0.5
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, volumeWeightedPotentialEnergyReservoir, globalPotentialEnergyReservoir)
+ volumeWeightedPotentialEnergyReservoir(1:nCellsSolve) = areaCell(1:nCellsSolve)*averageThickness*h_s(1:nCellsSolve)*gravity
+ call computeGlobalSum(dminfo, nVertLevels, nCellsSolve, volumeWeightedPotentialEnergyReservoir, global_temp)
+
+ globalPotentialEnergyReservoir = (globalPotentialEnergyReservoir + global_temp)/sumCellVolume
+
+ globalPotentialEnergy = globalPotentialEnergy - globalPotentialEnergyReservoir
+ globalEnergy = globalKineticEnergy + globalPotentialEnergy
+
+ ! Compute Coriolis energy tendency term
+ call computeGlobalSum(dminfo, nVertLevels, nEdgesSolve, keTend_CoriolisForce, globalCoriolisEnergyTendency)
+ globalCoriolisEnergyTendency = globalCoriolisEnergyTendency/sumCellVolume
+
+ ! Step 6
+ ! 6. Write out your global stat to the file
+ if (dminfo % my_proc_id == IO_NODE) then
+ fileID = getFreeUnit()
+
+ if (timeIndex/config_stats_interval == 1) then
+ open(fileID, file='GlobalIntegrals.txt',STATUS='unknown')
+ else
+ open(fileID, file='GlobalIntegrals.txt',POSITION='append')
+ endif
+ write(fileID,'(1i0, 100es24.16)') timeIndex, timeIndex*dt, globalFluidThickness, globalPotentialVorticity, globalPotentialEnstrophy, &
+ globalEnergy, globalCoriolisEnergyTendency, globalKineticEnergyTendency+globalPotentialEnergyTendency, &
+ globalKineticEnergy, globalPotentialEnergy
+ close(fileID)
+ end if
+
+ deallocate(areaEdge)
+ end subroutine computeGlobalDiagnostics
+
+ integer function getFreeUnit()
+ implicit none
+
+ integer :: index
+ logical :: isOpened
+
+ getFreeUnit = 0
+ do index = 1,99
+ if((index /= 5) .and. (index /= 6)) then
+ inquire(unit = index, opened = isOpened)
+ if( .not. isOpened) then
+ getFreeUnit = index
+ return
+ end if
+ end if
+ end do
+ end function getFreeUnit
+
+ subroutine computeGlobalSum(dminfo, nVertLevels, nElements, field, globalSum)
+
+ implicit none
+
+ type (dm_info), intent(in) :: dminfo
+ integer, intent(in) :: nVertLevels, nElements
+ real (kind=RKIND), dimension(nVertLevels, nElements), intent(in) :: field
+ real (kind=RKIND), intent(out) :: globalSum
+
+ real (kind=RKIND) :: localSum
+
+ localSum = sum(field)
+ call dmpar_sum_real(dminfo, localSum, globalSum)
+
+ end subroutine computeGlobalSum
+
+ subroutine computeGlobalMin(dminfo, nVertLevels, nElements, field, globalMin)
+
+ implicit none
+
+ type (dm_info), intent(in) :: dminfo
+ integer, intent(in) :: nVertLevels, nElements
+ real (kind=RKIND), dimension(nVertLevels, nElements), intent(in) :: field
+ real (kind=RKIND), intent(out) :: globalMin
+
+ real (kind=RKIND) :: localMin
+
+ localMin = minval(field)
+ call dmpar_min_real(dminfo, localMin, globalMin)
+
+ end subroutine computeGlobalMin
+
+ subroutine computeGlobalMax(dminfo, nVertLevels, nElements, field, globalMax)
+
+ implicit none
+
+ type (dm_info), intent(in) :: dminfo
+ integer, intent(in) :: nVertLevels, nElements
+ real (kind=RKIND), dimension(nVertLevels, nElements), intent(in) :: field
+ real (kind=RKIND), intent(out) :: globalMax
+
+ real (kind=RKIND) :: localMax
+
+ localMax = maxval(field)
+ call dmpar_max_real(dminfo, localMax, globalMax)
+
+ end subroutine computeGlobalMax
+
+ subroutine computeGlobalVertSumHorizMin(dminfo, nVertLevels, nElements, field, globalMin)
+
+ implicit none
+
+ type (dm_info), intent(in) :: dminfo
+ integer, intent(in) :: nVertLevels, nElements
+ real (kind=RKIND), dimension(nVertLevels, nElements), intent(in) :: field
+ real (kind=RKIND), intent(out) :: globalMin
+
+ real (kind=RKIND) :: localMin
+
+ localMin = minval(sum(field,1))
+ call dmpar_min_real(dminfo, localMin, globalMin)
+
+ end subroutine computeGlobalVertSumHorizMin
+
+ subroutine computeGlobalVertSumHorizMax(dminfo, nVertLevels, nElements, field, globalMax)
+
+ implicit none
+
+ type (dm_info), intent(in) :: dminfo
+ integer, intent(in) :: nVertLevels, nElements
+ real (kind=RKIND), dimension(nVertLevels, nElements), intent(in) :: field
+ real (kind=RKIND), intent(out) :: globalMax
+
+ real (kind=RKIND) :: localMax
+
+ localMax = maxval(sum(field,1))
+ call dmpar_max_real(dminfo, localMax, globalMax)
+
+ end subroutine computeGlobalVertSumHorizMax
+
+end module global_diagnostics
Added: branches/land_ice/mpas/src/core_land_ice/module_mpas_core.F
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/module_mpas_core.F         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/module_mpas_core.F        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,217 @@
+module mpas_core
+
+ use mpas_framework
+
+ type (io_output_object) :: restart_obj
+ integer :: restart_frame
+
+
+ contains
+
+
+ subroutine mpas_core_init(domain)
+
+ use configure
+ use grid_types
+ use test_cases
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+
+ real (kind=RKIND) :: dt
+ type (block_type), pointer :: block
+
+
+ if (.not. config_do_restart) call setup_sw_test_case(domain)
+
+ !
+ ! Initialize core
+ !
+ dt = config_dt
+ block => domain % blocklist
+ do while (associated(block))
+ call mpas_init_block(block, block % mesh, dt)
+ block => block % next
+ end do
+
+ restart_frame = 1
+
+ end subroutine mpas_core_init
+
+
+ subroutine mpas_init_block(block, mesh, dt)
+
+ use grid_types
+ use time_integration
+ use RBF_interpolation
+ use vector_reconstruction
+
+ implicit none
+
+ type (block_type), intent(inout) :: block
+ type (mesh_type), intent(inout) :: mesh
+ real (kind=RKIND), intent(in) :: dt
+
+
+ call compute_solve_diagnostics(dt, block % state % time_levs(1) % state, mesh)
+
+ call rbfInterp_initialize(mesh)
+ call init_reconstruct(mesh)
+ call reconstruct(block % state % time_levs(1) % state, mesh)
+
+ if (.not. config_do_restart) block % state % time_levs(1) % state % xtime % scalar = 0.0
+
+ end subroutine mpas_init_block
+
+
+ subroutine mpas_core_run(domain, output_obj, output_frame)
+
+ use grid_types
+ use io_output
+ use timer
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+ type (io_output_object), intent(inout) :: output_obj
+ integer, intent(inout) :: output_frame
+
+ integer :: ntimesteps, itimestep
+ real (kind=RKIND) :: dt
+ type (block_type), pointer :: block_ptr
+
+ ! Eventually, dt should be domain specific
+ dt = config_dt
+ ntimesteps = config_ntimesteps
+
+ call write_output_frame(output_obj, output_frame, domain)
+
+ ! During integration, time level 1 stores the model state at the beginning of the
+ ! time step, and time level 2 stores the state advanced dt in time by timestep(...)
+ do itimestep = 1,ntimesteps
+ write(0,*) 'Doing timestep ', itimestep
+ call timer_start("time integration")
+ call mpas_timestep(domain, itimestep, dt)
+ call timer_stop("time integration")
+
+ ! Move time level 2 fields back into time level 1 for next time step
+ call shift_time_levels_state(domain % blocklist % state)
+
+ if (mod(itimestep, config_output_interval) == 0) then
+ call write_output_frame(output_obj, output_frame, domain)
+ end if
+ if (mod(itimestep, config_restart_interval) == 0 .and. config_restart_interval > 0) then
+ if (restart_frame == 1) call output_state_init(restart_obj, domain, "RESTART")
+ call output_state_for_domain(restart_obj, domain, restart_frame)
+ restart_frame = restart_frame + 1
+ end if
+ end do
+
+ end subroutine mpas_core_run
+
+
+ subroutine write_output_frame(output_obj, output_frame, domain)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Compute diagnostic fields for a domain and write model state to output file
+ !
+ ! Input/Output: domain - contains model state; diagnostic field are computed
+ ! before returning
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ use grid_types
+ use io_output
+
+ implicit none
+
+ integer, intent(inout) :: output_frame
+ type (domain_type), intent(inout) :: domain
+ type (io_output_object), intent(inout) :: output_obj
+
+ integer :: i, j, k
+ integer :: eoe
+ type (block_type), pointer :: block_ptr
+
+ block_ptr => domain % blocklist
+ do while (associated(block_ptr))
+ call compute_output_diagnostics(block_ptr % state % time_levs(1) % state, block_ptr % mesh)
+ block_ptr => block_ptr % next
+ end do
+
+ call output_state_for_domain(output_obj, domain, output_frame)
+ output_frame = output_frame + 1
+
+ end subroutine write_output_frame
+
+
+ subroutine compute_output_diagnostics(state, grid)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Compute diagnostic fields for a domain
+ !
+ ! Input: state - contains model prognostic fields
+ ! grid - contains grid metadata
+ !
+ ! Output: state - upon returning, diagnostic fields will have be computed
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ use grid_types
+
+ implicit none
+
+ type (state_type), intent(inout) :: state
+ type (mesh_type), intent(in) :: grid
+
+ integer :: i, eoe
+ integer :: iEdge, k
+
+ end subroutine compute_output_diagnostics
+
+
+ subroutine mpas_timestep(domain, itimestep, dt)
+
+ use grid_types
+ use time_integration
+ use timer
+ use global_diagnostics
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+ integer, intent(in) :: itimestep
+ real (kind=RKIND), intent(in) :: dt
+ type (block_type), pointer :: block_ptr
+
+ call timestep(domain, dt)
+
+ if(config_stats_interval .gt. 0) then
+ if(mod(itimestep, config_stats_interval) == 0) then
+ block_ptr => domain % blocklist
+ if(associated(block_ptr % next)) then
+ write(0,*) 'Error: computeGlobalDiagnostics assumes ',&
+ 'that there is only one block per processor.'
+ end if
+
+ call timer_start("global_diagnostics")
+ call computeGlobalDiagnostics(domain % dminfo, &
+ block_ptr % state % time_levs(2) % state, block_ptr % mesh, &
+ itimestep, dt)
+ call timer_stop("global_diagnostics")
+ end if
+ end if
+
+ end subroutine mpas_timestep
+
+
+ subroutine mpas_core_finalize(domain)
+
+ use grid_types
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+
+ if (restart_frame > 1) call output_state_finalize(restart_obj, domain % dminfo)
+
+ end subroutine mpas_core_finalize
+
+end module mpas_core
Added: branches/land_ice/mpas/src/core_land_ice/module_test_cases.F
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/module_test_cases.F         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/module_test_cases.F        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,527 @@
+module test_cases
+
+ use grid_types
+ use configure
+ use constants
+
+
+ contains
+
+
+ subroutine setup_sw_test_case(domain)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Configure grid metadata and model state for the shallow water test case
+ ! specified in the namelist
+ !
+ ! Output: block - a subset (not necessarily proper) of the model domain to be
+ ! initialized
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+
+ integer :: i
+ type (block_type), pointer :: block_ptr
+
+ if (config_test_case == 0) then
+ write(0,*) 'Using initial conditions supplied in input file'
+
+ else if (config_test_case == 1) then
+ write(0,*) 'Setting up shallow water test case 1'
+ write(0,*) ' -- Advection of Cosine Bell over the Pole'
+
+ block_ptr => domain % blocklist
+ do while (associated(block_ptr))
+ call sw_test_case_1(block_ptr % mesh, block_ptr % state % time_levs(1) % state)
+ do i=2,nTimeLevs
+ call copy_state(block_ptr % state % time_levs(i) % state, block_ptr % state % time_levs(1) % state)
+ end do
+
+ block_ptr => block_ptr % next
+ end do
+
+ else if (config_test_case == 2) then
+ write(0,*) 'Setting up shallow water test case 2'
+ write(0,*) ' -- Setup shallow water test case 2: Global Steady State Nonlinear Zonal Geostrophic Flow'
+
+ block_ptr => domain % blocklist
+ do while (associated(block_ptr))
+ call sw_test_case_2(block_ptr % mesh, block_ptr % state % time_levs(1) % state)
+ do i=2,nTimeLevs
+ call copy_state(block_ptr % state % time_levs(i) % state, block_ptr % state % time_levs(1) % state)
+ end do
+
+ block_ptr => block_ptr % next
+ end do
+
+ else if (config_test_case == 5) then
+ write(0,*) 'Setting up shallow water test case 5'
+ write(0,*) ' -- Setup shallow water test case 5: Zonal Flow over an Isolated Mountain'
+
+ block_ptr => domain % blocklist
+ do while (associated(block_ptr))
+ call sw_test_case_5(block_ptr % mesh, block_ptr % state % time_levs(1) % state)
+ do i=2,nTimeLevs
+ call copy_state(block_ptr % state % time_levs(i) % state, block_ptr % state % time_levs(1) % state)
+ end do
+
+ block_ptr => block_ptr % next
+ end do
+
+ else if (config_test_case == 6) then
+ write(0,*) 'Setting up shallow water test case 6'
+ write(0,*) ' -- Rossby-Haurwitz Wave'
+
+ block_ptr => domain % blocklist
+ do while (associated(block_ptr))
+ call sw_test_case_6(block_ptr % mesh, block_ptr % state % time_levs(1) % state)
+ do i=2,nTimeLevs
+ call copy_state(block_ptr % state % time_levs(i) % state, block_ptr % state % time_levs(1) % state)
+ end do
+
+ block_ptr => block_ptr % next
+ end do
+
+ else
+ write(0,*) 'Only test case 1, 2, 5, and 6 are currently supported.'
+ stop
+ end if
+
+ end subroutine setup_sw_test_case
+
+
+ subroutine sw_test_case_1(grid, state)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Setup shallow water test case 1: Advection of Cosine Bell over the Pole
+ !
+ ! Reference: Williamson, D.L., et al., "A Standard Test Set for Numerical
+ ! Approximations to the Shallow Water Equations in Spherical
+ ! Geometry" J. of Comp. Phys., 102, pp. 211--224
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (mesh_type), intent(inout) :: grid
+ type (state_type), intent(inout) :: state
+
+ real (kind=RKIND), parameter :: u0 = 2.0 * pii * a / (12.0 * 86400.0)
+ real (kind=RKIND), parameter :: h0 = 1000.0
+ real (kind=RKIND), parameter :: theta_c = 0.0
+ real (kind=RKIND), parameter :: lambda_c = 3.0*pii/2.0
+ real (kind=RKIND), parameter :: alpha = pii/4.0
+
+ integer :: iCell, iEdge, iVtx
+ real (kind=RKIND) :: r, u, v
+ real (kind=RKIND), allocatable, dimension(:) :: psiVertex
+
+ !
+ ! Scale all distances and areas from a unit sphere to one with radius a
+ !
+ grid % xCell % array = grid % xCell % array * a
+ grid % yCell % array = grid % yCell % array * a
+ grid % zCell % array = grid % zCell % array * a
+ grid % xVertex % array = grid % xVertex % array * a
+ grid % yVertex % array = grid % yVertex % array * a
+ grid % zVertex % array = grid % zVertex % array * a
+ grid % xEdge % array = grid % xEdge % array * a
+ grid % yEdge % array = grid % yEdge % array * a
+ grid % zEdge % array = grid % zEdge % array * a
+ grid % dvEdge % array = grid % dvEdge % array * a
+ grid % dcEdge % array = grid % dcEdge % array * a
+ grid % areaCell % array = grid % areaCell % array * a**2.0
+ grid % areaTriangle % array = grid % areaTriangle % array * a**2.0
+ grid % kiteAreasOnVertex % array = grid % kiteAreasOnVertex % array * a**2.0
+
+ !
+ ! Initialize wind field
+ !
+ allocate(psiVertex(grid % nVertices))
+ do iVtx=1,grid % nVertices
+ psiVertex(iVtx) = -a * u0 * ( &
+ sin(grid%latVertex%array(iVtx)) * cos(alpha) - &
+ cos(grid%lonVertex%array(iVtx)) * cos(grid%latVertex%array(iVtx)) * sin(alpha) &
+ )
+ end do
+ do iEdge=1,grid % nEdges
+ state % u % array(1,iEdge) = -1.0 * ( &
+ psiVertex(grid%verticesOnEdge%array(2,iEdge)) - &
+ psiVertex(grid%verticesOnEdge%array(1,iEdge)) &
+ ) / grid%dvEdge%array(iEdge)
+ end do
+ deallocate(psiVertex)
+
+ !
+ ! Initialize cosine bell at (theta_c, lambda_c)
+ !
+ do iCell=1,grid % nCells
+ r = sphere_distance(theta_c, lambda_c, grid % latCell % array(iCell), grid % lonCell % array(iCell), a)
+ if (r < a/3.0) then
+ state % h % array(1,iCell) = (h0 / 2.0) * (1.0 + cos(pii*r*3.0/a))
+ else
+ state % h % array(1,iCell) = 0.0
+ end if
+ end do
+
+ end subroutine sw_test_case_1
+
+
+ subroutine sw_test_case_2(grid, state)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Setup shallow water test case 2: Global Steady State Nonlinear Zonal
+ ! Geostrophic Flow
+ !
+ ! Reference: Williamson, D.L., et al., "A Standard Test Set for Numerical
+ ! Approximations to the Shallow Water Equations in Spherical
+ ! Geometry" J. of Comp. Phys., 102, pp. 211--224
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (mesh_type), intent(inout) :: grid
+ type (state_type), intent(inout) :: state
+
+ real (kind=RKIND), parameter :: u0 = 2.0 * pii * a / (12.0 * 86400.0)
+ real (kind=RKIND), parameter :: gh0 = 29400.0
+ real (kind=RKIND), parameter :: alpha = 0.0
+
+ integer :: iCell, iEdge, iVtx
+ real (kind=RKIND) :: u, v
+ real (kind=RKIND), allocatable, dimension(:) :: psiVertex
+
+
+ !
+ ! Scale all distances and areas from a unit sphere to one with radius a
+ !
+ grid % xCell % array = grid % xCell % array * a
+ grid % yCell % array = grid % yCell % array * a
+ grid % zCell % array = grid % zCell % array * a
+ grid % xVertex % array = grid % xVertex % array * a
+ grid % yVertex % array = grid % yVertex % array * a
+ grid % zVertex % array = grid % zVertex % array * a
+ grid % xEdge % array = grid % xEdge % array * a
+ grid % yEdge % array = grid % yEdge % array * a
+ grid % zEdge % array = grid % zEdge % array * a
+ grid % dvEdge % array = grid % dvEdge % array * a
+ grid % dcEdge % array = grid % dcEdge % array * a
+ grid % areaCell % array = grid % areaCell % array * a**2.0
+ grid % areaTriangle % array = grid % areaTriangle % array * a**2.0
+ grid % kiteAreasOnVertex % array = grid % kiteAreasOnVertex % array * a**2.0
+
+
+ !
+ ! Initialize wind field
+ !
+ allocate(psiVertex(grid % nVertices))
+ do iVtx=1,grid % nVertices
+ psiVertex(iVtx) = -a * u0 * ( &
+ sin(grid%latVertex%array(iVtx)) * cos(alpha) - &
+ cos(grid%lonVertex%array(iVtx)) * cos(grid%latVertex%array(iVtx)) * sin(alpha) &
+ )
+ end do
+ do iEdge=1,grid % nEdges
+ state % u % array(1,iEdge) = -1.0 * ( &
+ psiVertex(grid%verticesOnEdge%array(2,iEdge)) - &
+ psiVertex(grid%verticesOnEdge%array(1,iEdge)) &
+ ) / grid%dvEdge%array(iEdge)
+ end do
+ deallocate(psiVertex)
+
+ !
+ ! Generate rotated Coriolis field
+ !
+ do iEdge=1,grid % nEdges
+ grid % fEdge % array(iEdge) = 2.0 * omega * &
+ ( -cos(grid%lonEdge%array(iEdge)) * cos(grid%latEdge%array(iEdge)) * sin(alpha) + &
+ sin(grid%latEdge%array(iEdge)) * cos(alpha) &
+ )
+ end do
+ do iVtx=1,grid % nVertices
+ grid % fVertex % array(iVtx) = 2.0 * omega * &
+ (-cos(grid%lonVertex%array(iVtx)) * cos(grid%latVertex%array(iVtx)) * sin(alpha) + &
+ sin(grid%latVertex%array(iVtx)) * cos(alpha) &
+ )
+ end do
+
+ !
+ ! Initialize height field (actually, fluid thickness field)
+ !
+ do iCell=1,grid % nCells
+ state % h % array(1,iCell) = (gh0 - (a * omega * u0 + 0.5 * u0**2.0) * &
+ (-cos(grid%lonCell%array(iCell)) * cos(grid%latCell%array(iCell)) * sin(alpha) + &
+ sin(grid%latCell%array(iCell)) * cos(alpha) &
+ )**2.0 &
+ ) / &
+ gravity
+ end do
+
+ end subroutine sw_test_case_2
+
+
+ subroutine sw_test_case_5(grid, state)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Setup shallow water test case 5: Zonal Flow over an Isolated Mountain
+ !
+ ! Reference: Williamson, D.L., et al., "A Standard Test Set for Numerical
+ ! Approximations to the Shallow Water Equations in Spherical
+ ! Geometry" J. of Comp. Phys., 102, pp. 211--224
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (mesh_type), intent(inout) :: grid
+ type (state_type), intent(inout) :: state
+
+ real (kind=RKIND), parameter :: u0 = 20.
+ real (kind=RKIND), parameter :: gh0 = 5960.0*gravity
+ real (kind=RKIND), parameter :: hs0 = 2000.
+ real (kind=RKIND), parameter :: theta_c = pii/6.0
+ real (kind=RKIND), parameter :: lambda_c = 3.0*pii/2.0
+ real (kind=RKIND), parameter :: rr = pii/9.0
+ real (kind=RKIND), parameter :: alpha = 0.0
+
+ integer :: iCell, iEdge, iVtx
+ real (kind=RKIND) :: r, u, v
+ real (kind=RKIND), allocatable, dimension(:) :: psiVertex
+
+
+ !
+ ! Scale all distances and areas from a unit sphere to one with radius a
+ !
+ grid % xCell % array = grid % xCell % array * a
+ grid % yCell % array = grid % yCell % array * a
+ grid % zCell % array = grid % zCell % array * a
+ grid % xVertex % array = grid % xVertex % array * a
+ grid % yVertex % array = grid % yVertex % array * a
+ grid % zVertex % array = grid % zVertex % array * a
+ grid % xEdge % array = grid % xEdge % array * a
+ grid % yEdge % array = grid % yEdge % array * a
+ grid % zEdge % array = grid % zEdge % array * a
+ grid % dvEdge % array = grid % dvEdge % array * a
+ grid % dcEdge % array = grid % dcEdge % array * a
+ grid % areaCell % array = grid % areaCell % array * a**2.0
+ grid % areaTriangle % array = grid % areaTriangle % array * a**2.0
+ grid % kiteAreasOnVertex % array = grid % kiteAreasOnVertex % array * a**2.0
+
+ !
+ ! Initialize wind field
+ !
+ allocate(psiVertex(grid % nVertices))
+ do iVtx=1,grid % nVertices
+ psiVertex(iVtx) = -a * u0 * ( &
+ sin(grid%latVertex%array(iVtx)) * cos(alpha) - &
+ cos(grid%lonVertex%array(iVtx)) * cos(grid%latVertex%array(iVtx)) * sin(alpha) &
+ )
+ end do
+ do iEdge=1,grid % nEdges
+ state % u % array(1,iEdge) = -1.0 * ( &
+ psiVertex(grid%verticesOnEdge%array(2,iEdge)) - &
+ psiVertex(grid%verticesOnEdge%array(1,iEdge)) &
+ ) / grid%dvEdge%array(iEdge)
+ end do
+ deallocate(psiVertex)
+
+ !
+ ! Generate rotated Coriolis field
+ !
+ do iEdge=1,grid % nEdges
+ grid % fEdge % array(iEdge) = 2.0 * omega * &
+ (-cos(grid%lonEdge%array(iEdge)) * cos(grid%latEdge%array(iEdge)) * sin(alpha) + &
+ sin(grid%latEdge%array(iEdge)) * cos(alpha) &
+ )
+ end do
+ do iVtx=1,grid % nVertices
+ grid % fVertex % array(iVtx) = 2.0 * omega * &
+ (-cos(grid%lonVertex%array(iVtx)) * cos(grid%latVertex%array(iVtx)) * sin(alpha) + &
+ sin(grid%latVertex%array(iVtx)) * cos(alpha) &
+ )
+ end do
+
+ !
+ ! Initialize mountain
+ !
+ do iCell=1,grid % nCells
+ if (grid % lonCell % array(iCell) < 0.0) grid % lonCell % array(iCell) = grid % lonCell % array(iCell) + 2.0 * pii
+ r = sqrt(min(rr**2.0, (grid % lonCell % array(iCell) - lambda_c)**2.0 + (grid % latCell % array(iCell) - theta_c)**2.0))
+ grid % h_s % array(iCell) = hs0 * (1.0 - r/rr)
+ end do
+
+ !
+ ! Initialize tracer fields
+ !
+ do iCell=1,grid % nCells
+ r = sqrt(min(rr**2.0, (grid % lonCell % array(iCell) - lambda_c)**2.0 + (grid % latCell % array(iCell) - theta_c)**2.0))
+ state % tracers % array(1,1,iCell) = 1.0 - r/rr
+ end do
+ if (grid%nTracers > 1) then
+ do iCell=1,grid % nCells
+ r = sqrt(min(rr**2.0, (grid % lonCell % array(iCell) - lambda_c)**2.0 + &
+ (grid % latCell % array(iCell) - theta_c - pii/6.0)**2.0 &
+ ) &
+ )
+ state % tracers % array(2,1,iCell) = 1.0 - r/rr
+ end do
+ end if
+
+ !
+ ! Initialize height field (actually, fluid thickness field)
+ !
+ do iCell=1,grid % nCells
+ state % h % array(1,iCell) = (gh0 - (a * omega * u0 + 0.5 * u0**2.0) * &
+ (-cos(grid%lonCell%array(iCell)) * cos(grid%latCell%array(iCell)) * sin(alpha) + &
+ sin(grid%latCell%array(iCell)) * cos(alpha) &
+ )**2.0 &
+ ) / &
+ gravity
+ state % h % array(1,iCell) = state % h % array(1,iCell) - grid % h_s % array(iCell)
+ end do
+
+ end subroutine sw_test_case_5
+
+
+ subroutine sw_test_case_6(grid, state)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Setup shallow water test case 6: Rossby-Haurwitz Wave
+ !
+ ! Reference: Williamson, D.L., et al., "A Standard Test Set for Numerical
+ ! Approximations to the Shallow Water Equations in Spherical
+ ! Geometry" J. of Comp. Phys., 102, pp. 211--224
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (mesh_type), intent(inout) :: grid
+ type (state_type), intent(inout) :: state
+
+ real (kind=RKIND), parameter :: h0 = 8000.0
+ real (kind=RKIND), parameter :: w = 7.848e-6
+ real (kind=RKIND), parameter :: K = 7.848e-6
+ real (kind=RKIND), parameter :: R = 4.0
+
+ integer :: iCell, iEdge, iVtx
+ real (kind=RKIND) :: u, v
+ real (kind=RKIND), allocatable, dimension(:) :: psiVertex
+
+
+ !
+ ! Scale all distances and areas from a unit sphere to one with radius a
+ !
+ grid % xCell % array = grid % xCell % array * a
+ grid % yCell % array = grid % yCell % array * a
+ grid % zCell % array = grid % zCell % array * a
+ grid % xVertex % array = grid % xVertex % array * a
+ grid % yVertex % array = grid % yVertex % array * a
+ grid % zVertex % array = grid % zVertex % array * a
+ grid % xEdge % array = grid % xEdge % array * a
+ grid % yEdge % array = grid % yEdge % array * a
+ grid % zEdge % array = grid % zEdge % array * a
+ grid % dvEdge % array = grid % dvEdge % array * a
+ grid % dcEdge % array = grid % dcEdge % array * a
+ grid % areaCell % array = grid % areaCell % array * a**2.0
+ grid % areaTriangle % array = grid % areaTriangle % array * a**2.0
+ grid % kiteAreasOnVertex % array = grid % kiteAreasOnVertex % array * a**2.0
+
+ !
+ ! Initialize wind field
+ !
+ allocate(psiVertex(grid % nVertices))
+ do iVtx=1,grid % nVertices
+ psiVertex(iVtx) = -a * a * w * sin(grid%latVertex%array(iVtx)) + &
+ a *a * K * (cos(grid%latVertex%array(iVtx))**R) * &
+ sin(grid%latVertex%array(iVtx)) * cos(R * grid%lonVertex%array(iVtx))
+ end do
+ do iEdge=1,grid % nEdges
+ state % u % array(1,iEdge) = -1.0 * ( &
+ psiVertex(grid%verticesOnEdge%array(2,iEdge)) - &
+ psiVertex(grid%verticesOnEdge%array(1,iEdge)) &
+ ) / grid%dvEdge%array(iEdge)
+ end do
+ deallocate(psiVertex)
+
+ !
+ ! Initialize height field (actually, fluid thickness field)
+ !
+ do iCell=1,grid % nCells
+ state % h % array(1,iCell) = (gravity * h0 + a*a*AA(grid%latCell%array(iCell)) + &
+ a*a*BB(grid%latCell%array(iCell)) * cos(R*grid%lonCell%array(iCell)) + &
+ a*a*CC(grid%latCell%array(iCell)) * cos(2.0*R*grid%lonCell%array(iCell)) &
+ ) / gravity
+ end do
+
+ end subroutine sw_test_case_6
+
+
+ real function sphere_distance(lat1, lon1, lat2, lon2, radius)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Compute the great-circle distance between (lat1, lon1) and (lat2, lon2) on a
+ ! sphere with given radius.
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ real (kind=RKIND), intent(in) :: lat1, lon1, lat2, lon2, radius
+
+ real (kind=RKIND) :: arg1
+
+ arg1 = sqrt( sin(0.5*(lat2-lat1))**2 + &
+ cos(lat1)*cos(lat2)*sin(0.5*(lon2-lon1))**2 )
+ sphere_distance = 2.*radius*asin(arg1)
+
+ end function sphere_distance
+
+
+ real function AA(theta)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! A, used in height field computation for Rossby-Haurwitz wave
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ real (kind=RKIND), parameter :: w = 7.848e-6
+ real (kind=RKIND), parameter :: K = 7.848e-6
+ real (kind=RKIND), parameter :: R = 4.0
+
+ real (kind=RKIND), intent(in) :: theta
+
+ AA = 0.5 * w * (2.0 * omega + w) * cos(theta)**2.0 + &
+ 0.25 * K**2.0 * cos(theta)**(2.0*R) * ((R+1.0)*cos(theta)**2.0 + 2.0*R**2.0 - R - 2.0 - 2.0*R**2.0 * cos(theta)**(-2.0))
+
+ end function AA
+
+
+ real function BB(theta)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! B, used in height field computation for Rossby-Haurwitz wave
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ real (kind=RKIND), parameter :: w = 7.848e-6
+ real (kind=RKIND), parameter :: K = 7.848e-6
+ real (kind=RKIND), parameter :: R = 4.0
+
+ real (kind=RKIND), intent(in) :: theta
+
+ BB = (2.0*(omega + w)*K / ((R+1.0)*(R+2.0))) * cos(theta)**R * ((R**2.0 + 2.0*R + 2.0) - ((R+1.0)*cos(theta))**2.0)
+
+ end function BB
+
+
+ real function CC(theta)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! C, used in height field computation for Rossby-Haurwitz wave
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ real (kind=RKIND), parameter :: w = 7.848e-6
+ real (kind=RKIND), parameter :: K = 7.848e-6
+ real (kind=RKIND), parameter :: R = 4.0
+
+ real (kind=RKIND), intent(in) :: theta
+
+ CC = 0.25 * K**2.0 * cos(theta)**(2.0*R) * ((R+1.0)*cos(theta)**2.0 - R - 2.0)
+
+ end function CC
+
+end module test_cases
Added: branches/land_ice/mpas/src/core_land_ice/module_time_integration.F
===================================================================
--- branches/land_ice/mpas/src/core_land_ice/module_time_integration.F         (rev 0)
+++ branches/land_ice/mpas/src/core_land_ice/module_time_integration.F        2010-11-16 22:06:26 UTC (rev 621)
@@ -0,0 +1,1259 @@
+module time_integration
+
+ use vector_reconstruction
+ use grid_types
+ use configure
+ use constants
+ use dmpar
+
+
+ contains
+
+
+ subroutine timestep(domain, dt)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Advance model state forward in time by the specified time step
+ !
+ ! Input: domain - current model state in time level 1 (e.g., time_levs(1)state%h(:,:))
+ ! plus grid meta-data
+ ! Output: domain - upon exit, time level 2 (e.g., time_levs(2)%state%h(:,:)) contains
+ ! model state advanced forward in time by dt seconds
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+ real (kind=RKIND), intent(in) :: dt
+
+ type (block_type), pointer :: block
+
+ if (trim(config_time_integration) == 'RK4') then
+ call rk4(domain, dt)
+ else
+ write(0,*) 'Unknown time integration option '//trim(config_time_integration)
+ write(0,*) 'Currently, only ''RK4'' is supported.'
+ stop
+ end if
+
+ block => domain % blocklist
+ do while (associated(block))
+ block % state % time_levs(2) % state % xtime % scalar = block % state % time_levs(1) % state % xtime % scalar + dt
+ block => block % next
+ end do
+
+ end subroutine timestep
+
+
+ subroutine rk4(domain, dt)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Advance model state forward in time by the specified time step using
+ ! 4th order Runge-Kutta
+ !
+ ! Input: domain - current model state in time level 1 (e.g., time_levs(1)state%h(:,:))
+ ! plus grid meta-data
+ ! Output: domain - upon exit, time level 2 (e.g., time_levs(2)%state%h(:,:)) contains
+ ! model state advanced forward in time by dt seconds
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (domain_type), intent(inout) :: domain
+ real (kind=RKIND), intent(in) :: dt
+
+ integer :: iCell, k
+ type (block_type), pointer :: block
+ type (state_type) :: provis
+
+ integer :: rk_step
+
+ real (kind=RKIND), dimension(4) :: rk_weights, rk_substep_weights
+
+ block => domain % blocklist
+ call allocate_state(provis, &
+ block % mesh % nCells, block % mesh % nEdges, block % mesh % maxEdges, block % mesh % maxEdges2, &
+ block % mesh % nVertices, block % mesh % vertexDegree, block % mesh % nVertLevels, &
+ block % mesh % nTracers)
+
+ !
+ ! Initialize time_levs(2) with state at current time
+ ! Initialize first RK state
+ ! Couple tracers time_levs(2) with h in time-levels
+ ! Initialize RK weights
+ !
+ block => domain % blocklist
+ do while (associated(block))
+
+ block % state % time_levs(2) % state % u % array(:,:) = block % state % time_levs(1) % state % u % array(:,:)
+ block % state % time_levs(2) % state % h % array(:,:) = block % state % time_levs(1) % state % h % array(:,:)
+ do iCell=1,block % mesh % nCells ! couple tracers to h
+ do k=1,block % mesh % nVertLevels
+ block % state % time_levs(2) % state % tracers % array(:,k,iCell) = block % state % time_levs(1) % state % tracers % array(:,k,iCell) &
+ * block % state % time_levs(1) % state % h % array(k,iCell)
+ end do
+ end do
+
+ call copy_state(provis, block % state % time_levs(1) % state)
+
+ block => block % next
+ end do
+
+ rk_weights(1) = dt/6.
+ rk_weights(2) = dt/3.
+ rk_weights(3) = dt/3.
+ rk_weights(4) = dt/6.
+
+ rk_substep_weights(1) = dt/2.
+ rk_substep_weights(2) = dt/2.
+ rk_substep_weights(3) = dt
+ rk_substep_weights(4) = 0.
+
+
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! BEGIN RK loop
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ do rk_step = 1, 4
+
+! --- update halos for diagnostic variables
+
+ block => domain % blocklist
+ do while (associated(block))
+ call dmpar_exch_halo_field2dReal(domain % dminfo, provis % pv_edge % array(:,:), &
+ block % mesh % nVertLevels, block % mesh % nEdges, &
+ block % parinfo % edgesToSend, block % parinfo % edgesToRecv)
+
+ if (config_h_mom_eddy_visc4 > 0.0) then
+ call dmpar_exch_halo_field2dReal(domain % dminfo, block % state % time_levs(2) % state % divergence % array(:,:), &
+ block % mesh % nVertLevels, block % mesh % nCells, &
+ block % parinfo % cellsToSend, block % parinfo % cellsToRecv)
+ call dmpar_exch_halo_field2dReal(domain % dminfo, block % state % time_levs(2) % state % vorticity % array(:,:), &
+ block % mesh % nVertLevels, block % mesh % nVertices, &
+ block % parinfo % verticesToSend, block % parinfo % verticesToRecv)
+ end if
+
+ block => block % next
+ end do
+
+! --- compute tendencies
+
+ block => domain % blocklist
+ do while (associated(block))
+ call compute_tend(block % tend, provis, block % mesh)
+ call compute_scalar_tend(block % tend, provis, block % mesh)
+ call enforce_boundaryEdge(block % tend, block % mesh)
+ block => block % next
+ end do
+
+! --- update halos for prognostic variables
+
+ block => domain % blocklist
+ do while (associated(block))
+ call dmpar_exch_halo_field2dReal(domain % dminfo, block % tend % u % array(:,:), &
+ block % mesh % nVertLevels, block % mesh % nEdges, &
+ block % parinfo % edgesToSend, block % parinfo % edgesToRecv)
+ call dmpar_exch_halo_field2dReal(domain % dminfo, block % tend % h % array(:,:), &
+ block % mesh % nVertLevels, block % mesh % nCells, &
+ block % parinfo % cellsToSend, block % parinfo % cellsToRecv)
+ call dmpar_exch_halo_field3dReal(domain % dminfo, block % tend % tracers % array(:,:,:), &
+ block % mesh % nTracers, block % mesh % nVertLevels, block % mesh % nCells, &
+ block % parinfo % cellsToSend, block % parinfo % cellsToRecv)
+ block => block % next
+ end do
+
+! --- compute next substep state
+
+ if (rk_step < 4) then
+ block => domain % blocklist
+ do while (associated(block))
+ provis % u % array(:,:) = block % state % time_levs(1) % state % u % array(:,:) &
+ + rk_substep_weights(rk_step) * block % tend % u % array(:,:)
+ provis % h % array(:,:) = block % state % time_levs(1) % state % h % array(:,:) &
+ + rk_substep_weights(rk_step) * block % tend % h % array(:,:)
+ do iCell=1,block % mesh % nCells
+ do k=1,block % mesh % nVertLevels
+ provis % tracers % array(:,k,iCell) = ( &
+ block % state % time_levs(1) % state % h % array(k,iCell) * &
+ block % state % time_levs(1) % state % tracers % array(:,k,iCell) &
+ + rk_substep_weights(rk_step) * block % tend % tracers % array(:,k,iCell) &
+ ) / provis % h % array(k,iCell)
+ end do
+ end do
+ if (config_test_case == 1) then ! For case 1, wind field should be fixed
+ provis % u % array(:,:) = block % state % time_levs(1) % state % u % array(:,:)
+ end if
+ call compute_solve_diagnostics(dt, provis, block % mesh)
+ block => block % next
+ end do
+ end if
+
+!--- accumulate update (for RK4)
+
+ block => domain % blocklist
+ do while (associated(block))
+ block % state % time_levs(2) % state % u % array(:,:) = block % state % time_levs(2) % state % u % array(:,:) &
+ + rk_weights(rk_step) * block % tend % u % array(:,:)
+ block % state % time_levs(2) % state % h % array(:,:) = block % state % time_levs(2) % state % h % array(:,:) &
+ + rk_weights(rk_step) * block % tend % h % array(:,:)
+ do iCell=1,block % mesh % nCells
+ do k=1,block % mesh % nVertLevels
+ block % state % time_levs(2) % state % tracers % array(:,k,iCell) = &
+ block % state % time_levs(2) % state % tracers % array(:,k,iCell) &
+ + rk_weights(rk_step) * block % tend % tracers % array(:,k,iCell)
+ end do
+ end do
+ block => block % next
+ end do
+
+ end do
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! END RK loop
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+
+ !
+ ! A little clean up at the end: decouple new scalar fields and compute diagnostics for new state
+ !
+ block => domain % blocklist
+ do while (associated(block))
+ do iCell=1,block % mesh % nCells
+ do k=1,block % mesh % nVertLevels
+ block % state % time_levs(2) % state % tracers % array(:,k,iCell) = &
+ block % state % time_levs(2) % state % tracers % array(:,k,iCell) &
+ / block % state % time_levs(2) % state % h % array(k,iCell)
+ end do
+ end do
+
+ if (config_test_case == 1) then ! For case 1, wind field should be fixed
+ block % state % time_levs(2) % state % u % array(:,:) = block % state % time_levs(1) % state % u % array(:,:)
+ end if
+
+ call compute_solve_diagnostics(dt, block % state % time_levs(2) % state, block % mesh)
+
+ call reconstruct(block % state % time_levs(2) % state, block % mesh)
+
+ block => block % next
+ end do
+
+ call deallocate_state(provis)
+
+ end subroutine rk4
+
+
+ subroutine compute_tend(tend, s, grid)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Compute height and normal wind tendencies, as well as diagnostic variables
+ !
+ ! Input: s - current model state
+ ! grid - grid metadata
+ !
+ ! Output: tend - computed tendencies for prognostic variables
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (tend_type), intent(inout) :: tend
+ type (state_type), intent(in) :: s
+ type (mesh_type), intent(in) :: grid
+
+ integer :: iEdge, iCell, iVertex, k, cell1, cell2, vertex1, vertex2, eoe, i, j
+ real (kind=RKIND) :: flux, vorticity_abs, workpv, q, upstream_bias
+
+ integer :: nCells, nEdges, nVertices, nVertLevels
+ real (kind=RKIND), dimension(:), pointer :: h_s, fVertex, fEdge, dvEdge, dcEdge, areaCell, areaTriangle
+ real (kind=RKIND), dimension(:,:), pointer :: vh, weightsOnEdge, kiteAreasOnVertex, h_edge, h, u, v, tend_h, tend_u, &
+ circulation, vorticity, ke, pv_edge, divergence, h_vertex
+ integer, dimension(:,:), pointer :: cellsOnEdge, cellsOnVertex, verticesOnEdge, edgesOnCell, edgesOnEdge, edgesOnVertex
+ integer, dimension(:), pointer :: nEdgesOnCell, nEdgesOnEdge
+ real (kind=RKIND) :: r, u_diffusion
+
+ real (kind=RKIND), allocatable, dimension(:,:) :: delsq_divergence
+ real (kind=RKIND), allocatable, dimension(:,:) :: delsq_u
+ real (kind=RKIND), allocatable, dimension(:,:) :: delsq_circulation, delsq_vorticity
+
+
+
+ h => s % h % array
+ u => s % u % array
+ v => s % v % array
+ h_edge => s % h_edge % array
+ circulation => s % circulation % array
+ vorticity => s % vorticity % array
+ divergence => s % divergence % array
+ ke => s % ke % array
+ pv_edge => s % pv_edge % array
+ vh => s % vh % array
+
+ weightsOnEdge => grid % weightsOnEdge % array
+ kiteAreasOnVertex => grid % kiteAreasOnVertex % array
+ cellsOnEdge => grid % cellsOnEdge % array
+ cellsOnVertex => grid % cellsOnVertex % array
+ verticesOnEdge => grid % verticesOnEdge % array
+ nEdgesOnCell => grid % nEdgesOnCell % array
+ edgesOnCell => grid % edgesOnCell % array
+ nEdgesOnEdge => grid % nEdgesOnEdge % array
+ edgesOnEdge => grid % edgesOnEdge % array
+ edgesOnVertex => grid % edgesOnVertex % array
+ dcEdge => grid % dcEdge % array
+ dvEdge => grid % dvEdge % array
+ areaCell => grid % areaCell % array
+ areaTriangle => grid % areaTriangle % array
+ h_s => grid % h_s % array
+ fVertex => grid % fVertex % array
+ fEdge => grid % fEdge % array
+
+ tend_h => tend % h % array
+ tend_u => tend % u % array
+
+ nCells = grid % nCells
+ nEdges = grid % nEdges
+ nVertices = grid % nVertices
+ nVertLevels = grid % nVertLevels
+
+
+ !
+ ! Compute height tendency for each cell
+ !
+ tend_h(:,:) = 0.0
+ do iEdge=1,nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ if (cell1 <= nCells) then
+ do k=1,nVertLevels
+ flux = u(k,iEdge) * dvEdge(iEdge) * h_edge(k,iEdge)
+ tend_h(k,cell1) = tend_h(k,cell1) - flux
+ end do
+ end if
+ if (cell2 <= nCells) then
+ do k=1,nVertLevels
+ flux = u(k,iEdge) * dvEdge(iEdge) * h_edge(k,iEdge)
+ tend_h(k,cell2) = tend_h(k,cell2) + flux
+ end do
+ end if
+ end do
+ do iCell=1,grid % nCellsSolve
+ do k=1,nVertLevels
+ tend_h(k,iCell) = tend_h(k,iCell) / areaCell(iCell)
+ end do
+ end do
+
+#ifdef LANL_FORMULATION
+ !
+ ! Compute u (normal) velocity tendency for each edge (cell face)
+ !
+ tend_u(:,:) = 0.0
+ do iEdge=1,grid % nEdgesSolve
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ vertex1 = verticesOnEdge(1,iEdge)
+ vertex2 = verticesOnEdge(2,iEdge)
+
+ do k=1,nVertLevels
+ q = 0.0
+ do j = 1,nEdgesOnEdge(iEdge)
+ eoe = edgesOnEdge(j,iEdge)
+ workpv = 0.5 * (pv_edge(k,iEdge) + pv_edge(k,eoe))
+ q = q + weightsOnEdge(j,iEdge) * u(k,eoe) * workpv * h_edge(k,eoe)
+ end do
+
+ tend_u(k,iEdge) = &
+ q &
+ - ( ke(k,cell2) - ke(k,cell1) + &
+ gravity * (h(k,cell2) + h_s(cell2) - h(k,cell1) - h_s(cell1)) &
+ ) / dcEdge(iEdge)
+ end do
+ end do
+
+
+#endif
+
+#ifdef NCAR_FORMULATION
+ !
+ ! Compute u (normal) velocity tendency for each edge (cell face)
+ !
+ tend_u(:,:) = 0.0
+ do iEdge=1,grid % nEdgesSolve
+ vertex1 = verticesOnEdge(1,iEdge)
+ vertex2 = verticesOnEdge(2,iEdge)
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+
+ do k=1,nVertLevels
+ vorticity_abs = fEdge(iEdge) + (circulation(k,vertex1) + circulation(k,vertex2)) / &
+ (areaTriangle(vertex1) + areaTriangle(vertex2))
+
+ workpv = 2.0 * vorticity_abs / (h(k,cell1) + h(k,cell2))
+
+ tend_u(k,iEdge) = workpv * vh(k,iEdge) - &
+ (ke(k,cell2) - ke(k,cell1) + &
+ gravity * (h(k,cell2) + h_s(cell2) - h(k,cell1) - h_s(cell1)) &
+ ) / &
+ dcEdge(iEdge)
+ end do
+ end do
+#endif
+
+ ! Compute diffusion, computed as </font>
<font color="black">abla divergence - k \times </font>
<font color="blue">abla vorticity
+ ! only valid for visc == constant
+ if (config_h_mom_eddy_visc2 > 0.0) then
+ do iEdge=1,grid % nEdgesSolve
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ vertex1 = verticesOnEdge(1,iEdge)
+ vertex2 = verticesOnEdge(2,iEdge)
+
+ do k=1,nVertLevels
+ u_diffusion = ( divergence(k,cell2) - divergence(k,cell1) ) / dcEdge(iEdge) &
+ -(vorticity(k,vertex2) - vorticity(k,vertex1) ) / dvEdge(iEdge)
+ u_diffusion = config_h_mom_eddy_visc2 * u_diffusion
+ tend_u(k,iEdge) = tend_u(k,iEdge) + u_diffusion
+ end do
+ end do
+ end if
+
+ !
+ ! velocity tendency: del4 dissipation, -</font>
<font color="black">u_4 </font>
<font color="blue">abla^4 u
+ ! computed as </font>
<font color="black">abla^2 u = </font>
<font color="black">abla divergence + k \times </font>
<font color="blue">abla vorticity
+ ! applied recursively.
+ ! strictly only valid for h_mom_eddy_visc4 == constant
+ !
+ if (config_h_mom_eddy_visc4 > 0.0) then
+ allocate(delsq_divergence(nVertLevels, nCells+1))
+ allocate(delsq_u(nVertLevels, nEdges+1))
+ allocate(delsq_circulation(nVertLevels, nVertices+1))
+ allocate(delsq_vorticity(nVertLevels, nVertices+1))
+
+ delsq_u(:,:) = 0.0
+
+ ! Compute </font>
<font color="black">abla^2 u = </font>
<font color="black">abla divergence + k \times </font>
<font color="blue">abla vorticity
+ do iEdge=1,grid % nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ vertex1 = verticesOnEdge(1,iEdge)
+ vertex2 = verticesOnEdge(2,iEdge)
+
+ do k=1,nVertLevels
+
+ delsq_u(k,iEdge) = ( divergence(k,cell2) - divergence(k,cell1) ) / dcEdge(iEdge) &
+ -( vorticity(k,vertex2) - vorticity(k,vertex1)) / dvEdge(iEdge)
+
+ end do
+ end do
+
+ ! vorticity using </font>
<font color="blue">abla^2 u
+ delsq_circulation(:,:) = 0.0
+ do iEdge=1,nEdges
+ vertex1 = verticesOnEdge(1,iEdge)
+ vertex2 = verticesOnEdge(2,iEdge)
+ do k=1,nVertLevels
+ delsq_circulation(k,vertex1) = delsq_circulation(k,vertex1) &
+ - dcEdge(iEdge) * delsq_u(k,iEdge)
+ delsq_circulation(k,vertex2) = delsq_circulation(k,vertex2) &
+ + dcEdge(iEdge) * delsq_u(k,iEdge)
+ end do
+ end do
+ do iVertex=1,nVertices
+ r = 1.0 / areaTriangle(iVertex)
+ do k=1,nVertLevels
+ delsq_vorticity(k,iVertex) = delsq_circulation(k,iVertex) * r
+ end do
+ end do
+
+ ! Divergence using </font>
<font color="blue">abla^2 u
+ delsq_divergence(:,:) = 0.0
+ do iEdge=1,nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ do k=1,nVertLevels
+ delsq_divergence(k,cell1) = delsq_divergence(k,cell1) &
+ + delsq_u(k,iEdge)*dvEdge(iEdge)
+ delsq_divergence(k,cell2) = delsq_divergence(k,cell2) &
+ - delsq_u(k,iEdge)*dvEdge(iEdge)
+ end do
+ end do
+ do iCell = 1,nCells
+ r = 1.0 / areaCell(iCell)
+ do k = 1,nVertLevels
+ delsq_divergence(k,iCell) = delsq_divergence(k,iCell) * r
+ end do
+ end do
+
+ ! Compute - \kappa </font>
<font color="blue">abla^4 u
+ ! as </font>
<font color="black">abla div(</font>
<font color="black">abla^2 u) + k \times </font>
<font color="black">abla ( k \cross curl(</font>
<font color="blue">abla^2 u) )
+ do iEdge=1,grid % nEdgesSolve
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ vertex1 = verticesOnEdge(1,iEdge)
+ vertex2 = verticesOnEdge(2,iEdge)
+
+ do k=1,nVertLevels
+
+ u_diffusion = ( delsq_divergence(k,cell2) &
+ - delsq_divergence(k,cell1) ) / dcEdge(iEdge) &
+ -( delsq_vorticity(k,vertex2) &
+ - delsq_vorticity(k,vertex1) ) / dvEdge(iEdge)
+
+ u_diffusion = config_h_mom_eddy_visc4 * u_diffusion
+ tend_u(k,iEdge) = tend_u(k,iEdge) - u_diffusion
+
+ end do
+ end do
+
+ deallocate(delsq_divergence)
+ deallocate(delsq_u)
+ deallocate(delsq_circulation)
+ deallocate(delsq_vorticity)
+
+ end if
+
+ end subroutine compute_tend
+
+
+ subroutine compute_scalar_tend(tend, s, grid)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ !
+ ! Input: s - current model state
+ ! grid - grid metadata
+ !
+ ! Output: tend - computed scalar tendencies
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ type (tend_type), intent(inout) :: tend
+ type (state_type), intent(in) :: s
+ type (mesh_type), intent(in) :: grid
+
+ integer :: iCell, iEdge, k, iTracer, cell1, cell2, i
+ real (kind=RKIND) :: flux, tracer_edge, r
+ real (kind=RKIND) :: invAreaCell1, invAreaCell2, tracer_turb_flux
+ integer, dimension(:,:), pointer :: boundaryEdge
+ real (kind=RKIND), dimension(:,:), allocatable :: boundaryMask
+ real (kind=RKIND), dimension(:,:,:), allocatable:: delsq_tracer
+
+ real (kind=RKIND) :: d2fdx2_cell1, d2fdx2_cell2
+ real (kind=RKIND), dimension(:), pointer :: dvEdge, dcEdge, areaCell
+ real (kind=RKIND), dimension(:,:,:), pointer :: tracers, tracer_tend
+ integer, dimension(:,:), pointer :: cellsOnEdge, boundaryCell
+ real (kind=RKIND), dimension(:,:,:), pointer :: deriv_two
+ real (kind=RKIND) :: coef_3rd_order
+ real (kind=RKIND), dimension(:,:), pointer :: u, h_edge
+
+ u => s % u % array
+ h_edge => s % h_edge % array
+ dcEdge => grid % dcEdge % array
+ deriv_two => grid % deriv_two % array
+ dvEdge => grid % dvEdge % array
+ tracers => s % tracers % array
+ cellsOnEdge => grid % cellsOnEdge % array
+ boundaryCell=> grid % boundaryCell % array
+ boundaryEdge=> grid % boundaryEdge % array
+ areaCell => grid % areaCell % array
+ tracer_tend => tend % tracers % array
+
+ coef_3rd_order = 0.
+ if (config_tracer_adv_order == 3) coef_3rd_order = 1.0
+ if (config_tracer_adv_order == 3 .and. config_monotonic) coef_3rd_order = 0.25
+
+
+ tracer_tend(:,:,:) = 0.0
+
+ if (config_tracer_adv_order == 2) then
+
+ do iEdge=1,grid % nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ if (cell1 <= grid%nCells .and. cell2 <= grid%nCells) then
+ do k=1,grid % nVertLevels
+ do iTracer=1,grid % nTracers
+ tracer_edge = 0.5 * (tracers(iTracer,k,cell1) + tracers(iTracer,k,cell2))
+ flux = u(k,iEdge) * dvEdge(iEdge) * h_edge(k,iEdge) * tracer_edge
+ tracer_tend(iTracer,k,cell1) = tracer_tend(iTracer,k,cell1) - flux/areaCell(cell1)
+ tracer_tend(iTracer,k,cell2) = tracer_tend(iTracer,k,cell2) + flux/areaCell(cell2)
+ end do
+ end do
+ end if
+ end do
+
+ else if (config_tracer_adv_order == 3) then
+
+ do iEdge=1,grid%nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+
+ !-- if a cell not on the most outside ring of the halo
+ if (cell1 <= grid%nCells .and. cell2 <= grid%nCells) then
+
+ do k=1,grid % nVertLevels
+
+ d2fdx2_cell1 = 0.0
+ d2fdx2_cell2 = 0.0
+
+ do iTracer=1,grid % nTracers
+
+ !-- if not a boundary cell
+ if(boundaryCell(k,cell1).eq.0.and.boundaryCell(k,cell2).eq.0) then
+
+ d2fdx2_cell1 = deriv_two(1,1,iEdge) * tracers(iTracer,k,cell1)
+ d2fdx2_cell2 = deriv_two(1,2,iEdge) * tracers(iTracer,k,cell2)
+
+ !-- all edges of cell 1
+ do i=1, grid % nEdgesOnCell % array (cell1)
+ d2fdx2_cell1 = d2fdx2_cell1 + &
+ deriv_two(i+1,1,iEdge) * tracers(iTracer,k,grid % CellsOnCell % array (i,cell1))
+ end do
+
+ !-- all edges of cell 2
+ do i=1, grid % nEdgesOnCell % array (cell2)
+ d2fdx2_cell2 = d2fdx2_cell2 + &
+ deriv_two(i+1,2,iEdge) * tracers(iTracer,k,grid % CellsOnCell % array (i,cell2))
+ end do
+
+ endif
+
+ !-- if u > 0:
+ if (u(k,iEdge) > 0) then
+ flux = dvEdge(iEdge) * u(k,iEdge) * h_edge(k,iEdge) * ( &
+ 0.5*(tracers(iTracer,k,cell1) + tracers(iTracer,k,cell2)) &
+ -(dcEdge(iEdge) **2) * (d2fdx2_cell1 + d2fdx2_cell2) / 12. &
+ -(dcEdge(iEdge) **2) * coef_3rd_order*(d2fdx2_cell1 - d2fdx2_cell2) / 12. )
+ !-- else u <= 0:
+ else
+ flux = dvEdge(iEdge) * u(k,iEdge) * h_edge(k,iEdge) * ( &
+ 0.5*(tracers(iTracer,k,cell1) + tracers(iTracer,k,cell2)) &
+ -(dcEdge(iEdge) **2) * (d2fdx2_cell1 + d2fdx2_cell2) / 12. &
+ +(dcEdge(iEdge) **2) * coef_3rd_order*(d2fdx2_cell1 - d2fdx2_cell2) / 12. )
+ end if
+
+ !-- update tendency
+ tracer_tend(iTracer,k,cell1) = tracer_tend(iTracer,k,cell1) - flux/areaCell(cell1)
+ tracer_tend(iTracer,k,cell2) = tracer_tend(iTracer,k,cell2) + flux/areaCell(cell2)
+ enddo
+ end do
+ end if
+ end do
+
+ else if (config_tracer_adv_order == 4) then
+
+ do iEdge=1,grid%nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+
+ !-- if an edge is not on the outer-most ring of the halo
+ if (cell1 <= grid%nCells .and. cell2 <= grid%nCells) then
+
+ do k=1,grid % nVertLevels
+
+ d2fdx2_cell1 = 0.0
+ d2fdx2_cell2 = 0.0
+
+ do iTracer=1,grid % nTracers
+
+ !-- if not a boundary cell
+ if(boundaryCell(k,cell1).eq.0.and.boundaryCell(k,cell2).eq.0) then
+
+ d2fdx2_cell1 = deriv_two(1,1,iEdge) * tracers(iTracer,k,cell1)
+ d2fdx2_cell2 = deriv_two(1,2,iEdge) * tracers(iTracer,k,cell2)
+
+ !-- all edges of cell 1
+ do i=1, grid % nEdgesOnCell % array (cell1)
+ d2fdx2_cell1 = d2fdx2_cell1 + &
+ deriv_two(i+1,1,iEdge) * tracers(iTracer,k,grid % CellsOnCell % array (i,cell1))
+ end do
+
+ !-- all edges of cell 2
+ do i=1, grid % nEdgesOnCell % array (cell2)
+ d2fdx2_cell2 = d2fdx2_cell2 + &
+ deriv_two(i+1,2,iEdge) * tracers(iTracer,k,grid % CellsOnCell % array (i,cell2))
+ end do
+
+ endif
+
+ flux = dvEdge(iEdge) * u(k,iEdge) * h_edge(k,iEdge) * ( &
+ 0.5*(tracers(iTracer,k,cell1) + tracers(iTracer,k,cell2)) &
+ -(dcEdge(iEdge) **2) * (d2fdx2_cell1 + d2fdx2_cell2) / 12. )
+
+ !-- update tendency
+ tracer_tend(iTracer,k,cell1) = tracer_tend(iTracer,k,cell1) - flux/areaCell(cell1)
+ tracer_tend(iTracer,k,cell2) = tracer_tend(iTracer,k,cell2) + flux/areaCell(cell2)
+ enddo
+ end do
+ end if
+ end do
+
+ endif ! if (config_tracer_adv_order == 2 )
+
+ !
+ ! tracer tendency: del2 horizontal tracer diffusion, div(h \kappa_2 </font>
<font color="blue">abla \phi)
+ !
+ if ( config_h_tracer_eddy_diff2 > 0.0 ) then
+
+ !
+ ! compute a boundary mask to enforce insulating boundary conditions in the horizontal
+ !
+ allocate(boundaryMask(grid % nVertLevels, grid % nEdges+1))
+ boundaryMask = 1.0
+ where(boundaryEdge.eq.1) boundaryMask=0.0
+
+ do iEdge=1,grid % nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ invAreaCell1 = 1.0/areaCell(cell1)
+ invAreaCell2 = 1.0/areaCell(cell2)
+
+ do k=1,grid % nVertLevels
+ do iTracer=1, grid % nTracers
+ ! \kappa_2 </font>
<font color="blue">abla \phi on edge
+ tracer_turb_flux = config_h_tracer_eddy_diff2 &
+ *( tracers(iTracer,k,cell2) - tracers(iTracer,k,cell1)) / dcEdge(iEdge)
+
+ ! div(h \kappa_2 </font>
<font color="blue">abla \phi) at cell center
+ flux = dvEdge(iEdge) * h_edge(k,iEdge) * tracer_turb_flux * boundaryMask(k, iEdge)
+ tracer_tend(iTracer,k,cell1) = tracer_tend(iTracer,k,cell1) + flux * invAreaCell1
+ tracer_tend(iTracer,k,cell2) = tracer_tend(iTracer,k,cell2) - flux * invAreaCell2
+ end do
+ end do
+
+ end do
+
+ deallocate(boundaryMask)
+
+ end if
+
+ !
+ ! tracer tendency: del4 horizontal tracer diffusion, &
+ ! div(h \kappa_4 </font>
<font color="black">abla [div(h </font>
<font color="blue">abla \phi)])
+ !
+ if ( config_h_tracer_eddy_diff4 > 0.0 ) then
+
+ !
+ ! compute a boundary mask to enforce insulating boundary conditions in the horizontal
+ !
+ allocate(boundaryMask(grid % nVertLevels, grid % nEdges+1))
+ boundaryMask = 1.0
+ where(boundaryEdge.eq.1) boundaryMask=0.0
+
+ allocate(delsq_tracer(grid % nTracers, grid % nVertLevels, grid % nCells+1))
+
+ delsq_tracer(:,:,:) = 0.
+
+ ! first del2: div(h </font>
<font color="blue">abla \phi) at cell center
+ do iEdge=1,grid % nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+
+ do k=1,grid % nVertLevels
+ do iTracer=1, grid % nTracers
+ delsq_tracer(iTracer,k,cell1) = delsq_tracer(iTracer,k,cell1) &
+ + dvEdge(iEdge) * h_edge(k,iEdge) * (tracers(iTracer,k,cell2) - tracers(iTracer,k,cell1)) / dcEdge(iEdge) * boundaryMask(k,iEdge)
+ delsq_tracer(iTracer,k,cell2) = delsq_tracer(iTracer,k,cell2) &
+ - dvEdge(iEdge) * h_edge(k,iEdge) * (tracers(iTracer,k,cell2) - tracers(iTracer,k,cell1)) / dcEdge(iEdge) * boundaryMask(k,iEdge)
+ end do
+ end do
+
+ end do
+
+ do iCell = 1, grid % nCells
+ r = 1.0 / grid % areaCell % array(iCell)
+ do k=1,grid % nVertLevels
+ do iTracer=1,grid % nTracers
+ delsq_tracer(iTracer,k,iCell) = delsq_tracer(iTracer,k,iCell) * r
+ end do
+ end do
+ end do
+
+ ! second del2: div(h </font>
<font color="blue">abla [delsq_tracer]) at cell center
+ do iEdge=1,grid % nEdges
+ cell1 = grid % cellsOnEdge % array(1,iEdge)
+ cell2 = grid % cellsOnEdge % array(2,iEdge)
+ invAreaCell1 = 1.0 / grid % areaCell % array(cell1)
+ invAreaCell2 = 1.0 / grid % areaCell % array(cell2)
+
+ do k=1,grid % nVertLevels
+ do iTracer=1,grid % nTracers
+ tracer_turb_flux = config_h_tracer_eddy_diff4 * (delsq_tracer(iTracer,k,cell2) - delsq_tracer(iTracer,k,cell1)) / dcEdge(iEdge)
+ flux = dvEdge(iEdge) * tracer_turb_flux
+ tracer_tend(iTracer,k,cell1) = tracer_tend(iTracer,k,cell1) - flux * invAreaCell1 * boundaryMask(k,iEdge)
+ tracer_tend(iTracer,k,cell2) = tracer_tend(iTracer,k,cell2) + flux * invAreaCell2 * boundaryMask(k,iEdge)
+ end do
+ enddo
+
+ end do
+
+ deallocate(delsq_tracer)
+ deallocate(boundaryMask)
+
+ end if
+
+ end subroutine compute_scalar_tend
+
+
+ subroutine compute_solve_diagnostics(dt, s, grid)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Compute diagnostic fields used in the tendency computations
+ !
+ ! Input: grid - grid metadata
+ !
+ ! Output: s - computed diagnostics
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+ implicit none
+
+ real (kind=RKIND), intent(in) :: dt
+ type (state_type), intent(inout) :: s
+ type (mesh_type), intent(in) :: grid
+
+
+ integer :: iEdge, iCell, iVertex, k, cell1, cell2, vertex1, vertex2, eoe, i, j, cov
+ real (kind=RKIND) :: flux, vorticity_abs, workpv
+
+ integer :: nCells, nEdges, nVertices, nVertLevels
+ real (kind=RKIND), dimension(:), pointer :: h_s, fVertex, fEdge, dvEdge, dcEdge, areaCell, areaTriangle
+ real (kind=RKIND), dimension(:,:), pointer :: vh, weightsOnEdge, kiteAreasOnVertex, h_edge, h, u, v, tend_h, tend_u, &
+ circulation, vorticity, ke, pv_edge, pv_vertex, pv_cell, gradPVn, gradPVt, divergence, &
+ h_vertex, vorticity_cell
+ integer, dimension(:,:), pointer :: cellsOnEdge, cellsOnVertex, verticesOnEdge, edgesOnCell, edgesOnEdge, edgesOnVertex, boundaryEdge, boundaryCell
+ integer, dimension(:), pointer :: nEdgesOnCell, nEdgesOnEdge
+ real (kind=RKIND) :: r, h1, h2
+ real (kind=RKIND) :: d2fdx2_cell1, d2fdx2_cell2
+ real (kind=RKIND), dimension(:,:,:), pointer :: deriv_two
+ real (kind=RKIND) :: coef_3rd_order
+
+ h => s % h % array
+ u => s % u % array
+ v => s % v % array
+ vh => s % vh % array
+ h_edge => s % h_edge % array
+ h_vertex => s % h_vertex % array
+ tend_h => s % h % array
+ tend_u => s % u % array
+ circulation => s % circulation % array
+ vorticity => s % vorticity % array
+ divergence => s % divergence % array
+ ke => s % ke % array
+ pv_edge => s % pv_edge % array
+ pv_vertex => s % pv_vertex % array
+ pv_cell => s % pv_cell % array
+ vorticity_cell => s % vorticity_cell % array
+ gradPVn => s % gradPVn % array
+ gradPVt => s % gradPVt % array
+
+ weightsOnEdge => grid % weightsOnEdge % array
+ kiteAreasOnVertex => grid % kiteAreasOnVertex % array
+ cellsOnEdge => grid % cellsOnEdge % array
+ cellsOnVertex => grid % cellsOnVertex % array
+ verticesOnEdge => grid % verticesOnEdge % array
+ nEdgesOnCell => grid % nEdgesOnCell % array
+ edgesOnCell => grid % edgesOnCell % array
+ nEdgesOnEdge => grid % nEdgesOnEdge % array
+ edgesOnEdge => grid % edgesOnEdge % array
+ edgesOnVertex => grid % edgesOnVertex % array
+ dcEdge => grid % dcEdge % array
+ dvEdge => grid % dvEdge % array
+ areaCell => grid % areaCell % array
+ areaTriangle => grid % areaTriangle % array
+ h_s => grid % h_s % array
+ fVertex => grid % fVertex % array
+ fEdge => grid % fEdge % array
+ deriv_two => grid % deriv_two % array
+
+ nCells = grid % nCells
+ nEdges = grid % nEdges
+ nVertices = grid % nVertices
+ nVertLevels = grid % nVertLevels
+
+ boundaryEdge => grid % boundaryEdge % array
+ boundaryCell => grid % boundaryCell % array
+
+ !
+ ! Find those cells that have an edge on the boundary
+ !
+ boundaryCell(:,:) = 0
+ do iEdge=1,nEdges
+ do k=1,nVertLevels
+ if(boundaryEdge(k,iEdge).eq.1) then
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ boundaryCell(k,cell1) = 1
+ boundaryCell(k,cell2) = 1
+ endif
+ enddo
+ enddo
+
+ !
+ ! Compute height on cell edges at velocity locations
+ ! Namelist options control the order of accuracy of the reconstructed h_edge value
+ !
+
+ coef_3rd_order = 0.
+ if (config_thickness_adv_order == 3) coef_3rd_order = 1.0
+ if (config_thickness_adv_order == 3 .and. config_monotonic) coef_3rd_order = 0.25
+
+ if (config_thickness_adv_order == 2) then
+
+ do iEdge=1,grid % nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ if (cell1 <= grid%nCells .and. cell2 <= grid%nCells) then
+ do k=1,grid % nVertLevels
+ h_edge(k,iEdge) = 0.5 * (h(k,cell1) + h(k,cell2))
+ end do
+ end if
+ end do
+
+ else if (config_thickness_adv_order == 3) then
+
+ do iEdge=1,grid%nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+
+ !-- if a cell not on the most outside ring of the halo
+ if (cell1 <= grid%nCells .and. cell2 <= grid%nCells) then
+
+ do k=1,grid % nVertLevels
+
+ d2fdx2_cell1 = 0.0
+ d2fdx2_cell2 = 0.0
+
+ !-- if not a boundary cell
+ if(boundaryCell(k,cell1).eq.0.and.boundaryCell(k,cell2).eq.0) then
+
+ d2fdx2_cell1 = deriv_two(1,1,iEdge) * h(k,cell1)
+ d2fdx2_cell2 = deriv_two(1,2,iEdge) * h(k,cell2)
+
+ !-- all edges of cell 1
+ do i=1, grid % nEdgesOnCell % array (cell1)
+ d2fdx2_cell1 = d2fdx2_cell1 + &
+ deriv_two(i+1,1,iEdge) * h(k,grid % CellsOnCell % array (i,cell1))
+ end do
+
+ !-- all edges of cell 2
+ do i=1, grid % nEdgesOnCell % array (cell2)
+ d2fdx2_cell2 = d2fdx2_cell2 + &
+ deriv_two(i+1,2,iEdge) * h(k,grid % CellsOnCell % array (i,cell2))
+ end do
+
+ endif
+
+ !-- if u > 0:
+ if (u(k,iEdge) > 0) then
+ h_edge(k,iEdge) = &
+ 0.5*(h(k,cell1) + h(k,cell2)) &
+ -(dcEdge(iEdge) **2) * (d2fdx2_cell1 + d2fdx2_cell2) / 12. &
+ -(dcEdge(iEdge) **2) * coef_3rd_order*(d2fdx2_cell1 - d2fdx2_cell2) / 12.
+ !-- else u <= 0:
+ else
+ h_edge(k,iEdge) = &
+ 0.5*(h(k,cell1) + h(k,cell2)) &
+ -(dcEdge(iEdge) **2) * (d2fdx2_cell1 + d2fdx2_cell2) / 12. &
+ +(dcEdge(iEdge) **2) * coef_3rd_order*(d2fdx2_cell1 - d2fdx2_cell2) / 12.
+ end if
+
+ end do ! do k
+ end if ! if (cell1 <=
+ end do ! do iEdge
+
+ else if (config_thickness_adv_order == 4) then
+
+ do iEdge=1,grid%nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+
+ !-- if a cell not on the most outside ring of the halo
+ if (cell1 <= grid%nCells .and. cell2 <= grid%nCells) then
+
+ do k=1,grid % nVertLevels
+
+ d2fdx2_cell1 = 0.0
+ d2fdx2_cell2 = 0.0
+
+ !-- if not a boundary cell
+ if(boundaryCell(k,cell1).eq.0.and.boundaryCell(k,cell2).eq.0) then
+
+ d2fdx2_cell1 = deriv_two(1,1,iEdge) * h(k,cell1)
+ d2fdx2_cell2 = deriv_two(1,2,iEdge) * h(k,cell2)
+
+ !-- all edges of cell 1
+ do i=1, grid % nEdgesOnCell % array (cell1)
+ d2fdx2_cell1 = d2fdx2_cell1 + &
+ deriv_two(i+1,1,iEdge) * h(k,grid % CellsOnCell % array (i,cell1))
+ end do
+
+ !-- all edges of cell 2
+ do i=1, grid % nEdgesOnCell % array (cell2)
+ d2fdx2_cell2 = d2fdx2_cell2 + &
+ deriv_two(i+1,2,iEdge) * h(k,grid % CellsOnCell % array (i,cell2))
+ end do
+
+ endif
+
+ h_edge(k,iEdge) = &
+ 0.5*(h(k,cell1) + h(k,cell2)) &
+ -(dcEdge(iEdge) **2) * (d2fdx2_cell1 + d2fdx2_cell2) / 12.
+
+ end do ! do k
+ end if ! if (cell1 <=
+ end do ! do iEdge
+
+ endif ! if(config_thickness_adv_order == 2)
+
+ !
+ ! set the velocity in the nEdges+1 slot to zero, this is a dummy address
+ ! used to when reading for edges that do not exist
+ !
+ u(:,nEdges+1) = 0.0
+
+ !
+ ! Compute circulation and relative vorticity at each vertex
+ !
+ circulation(:,:) = 0.0
+ do iEdge=1,nEdges
+ do k=1,nVertLevels
+ circulation(k,verticesOnEdge(1,iEdge)) = circulation(k,verticesOnEdge(1,iEdge)) - dcEdge(iEdge) * u(k,iEdge)
+ circulation(k,verticesOnEdge(2,iEdge)) = circulation(k,verticesOnEdge(2,iEdge)) + dcEdge(iEdge) * u(k,iEdge)
+ end do
+ end do
+ do iVertex=1,nVertices
+ do k=1,nVertLevels
+ vorticity(k,iVertex) = circulation(k,iVertex) / areaTriangle(iVertex)
+ end do
+ end do
+
+
+ !
+ ! Compute the divergence at each cell center
+ !
+ divergence(:,:) = 0.0
+ do iEdge=1,nEdges
+ cell1 = cellsOnEdge(1,iEdge)
+ cell2 = cellsOnEdge(2,iEdge)
+ if (cell1 <= nCells) then
+ do k=1,nVertLevels
+ divergence(k,cell1) = divergence(k,cell1) + u(k,iEdge)*dvEdge(iEdge)
+ enddo
+ endif
+ if(cell2 <= nCells) then
+ do k=1,nVertLevels
+ divergence(k,cell2) = divergence(k,cell2) - u(k,iEdge)*dvEdge(iEdge)
+ enddo
+ end if
+ end do
+ do iCell = 1,nCells
+ r = 1.0 / areaCell(iCell)
+ do k = 1,nVertLevels
+ divergence(k,iCell) = divergence(k,iCell) * r
+ enddo
+ enddo
+
+ !
+ ! Compute kinetic energy in each cell
+ !
+ ke(:,:) = 0.0
+ do iCell=1,nCells
+ do i=1,nEdgesOnCell(iCell)
+ iEdge = edgesOnCell(i,iCell)
+ do k=1,nVertLevels
+ ke(k,iCell) = ke(k,iCell) + 0.25 * dcEdge(iEdge) * dvEdge(iEdge) * u(k,iEdge)**2.0
+ end do
+ end do
+ do k=1,nVertLevels
+ ke(k,iCell) = ke(k,iCell) / areaCell(iCell)
+ end do
+ end do
+
+ !
+ ! Compute v (tangential) velocities
+ !
+ v(:,:) = 0.0
+ do iEdge = 1,nEdges
+ do i=1,nEdgesOnEdge(iEdge)
+ eoe = edgesOnEdge(i,iEdge)
+ do k = 1,nVertLevels
+ v(k,iEdge) = v(k,iEdge) + weightsOnEdge(i,iEdge) * u(k, eoe)
+ end do
+ end do
+ end do
+
+#ifdef NCAR_FORMULATION
+ !
+ ! Compute mass fluxes tangential to each edge (i.e., through the faces of dual grid cells)
+ !
+ vh(:,:) = 0.0
+ do iEdge=1,grid % nEdgesSolve
+ do j=1,nEdgesOnEdge(iEdge)
+ eoe = edgesOnEdge(j,iEdge)
+ do k=1,nVertLevels
+ vh(k,iEdge) = vh(k,iEdge) + weightsOnEdge(j,iEdge) * u(k,eoe) * h_edge(k,eoe)
+ end do
+ end do
+ end do
+#endif
+
+
+ !
+ ! Compute height at vertices, pv at vertices, and average pv to edge locations
+ ! ( this computes pv_vertex at all vertices bounding real cells and distance-1 ghost cells )
+ !
+ VTX_LOOP: do iVertex = 1,nVertices
+ do i=1,grid % vertexDegree
+ if (cellsOnVertex(i,iVertex) > nCells) cycle VTX_LOOP
+ end do
+ do k=1,nVertLevels
+ h_vertex(k,iVertex) = 0.0
+ do i=1,grid % vertexDegree
+ h_vertex(k,iVertex) = h_vertex(k,iVertex) + h(k,cellsOnVertex(i,iVertex)) * kiteAreasOnVertex(i,iVertex)
+ end do
+ h_vertex(k,iVertex) = h_vertex(k,iVertex) / areaTriangle(iVertex)
+
+ pv_vertex(k,iVertex) = (fVertex(iVertex) + vorticity(k,iVertex)) / h_vertex(k,iVertex)
+ end do
+ end do VTX_LOOP
+
+
+ !
+ ! Compute gradient of PV in the tangent direction
+ ! ( this computes gradPVt at all edges bounding real cells and distance-1 ghost cells )
+ !
+ do iEdge = 1,nEdges
+ do k = 1,nVertLevels
+ gradPVt(k,iEdge) = (pv_vertex(k,verticesOnEdge(2,iEdge)) - pv_vertex(k,verticesOnEdge(1,iEdge))) / &
+ dvEdge(iEdge)
+ enddo
+ enddo
+
+ !
+ ! Compute pv at the edges
+ ! ( this computes pv_edge at all edges bounding real cells )
+ !
+ pv_edge(:,:) = 0.0
+ do iVertex = 1,nVertices
+ do i=1,grid % vertexDegree
+ iEdge = edgesOnVertex(i,iVertex)
+ do k=1,nVertLevels
+ pv_edge(k,iEdge) = pv_edge(k,iEdge) + 0.5 * pv_vertex(k,iVertex)
+ end do
+ end do
+ end do
+
+
+ !
+ ! Modify PV edge with upstream bias.
+ !
+ do iEdge = 1,nEdges
+ do k = 1,nVertLevels
+ pv_edge(k,iEdge) = pv_edge(k,iEdge) - config_apvm_upwinding * v(k,iEdge) * dt * gradPVt(k,iEdge)
+ enddo
+ enddo
+
+
+ !
+ ! Compute pv at cell centers
+ ! ( this computes pv_cell for all real cells and distance-1 ghost cells )
+ !
+ pv_cell(:,:) = 0.0
+ vorticity_cell(:,:) = 0.0
+ do iVertex = 1, nVertices
+ do i=1,grid % vertexDegree
+ iCell = cellsOnVertex(i,iVertex)
+ if (iCell <= nCells) then
+ do k = 1,nVertLevels
+ pv_cell(k,iCell) = pv_cell(k,iCell) + kiteAreasOnVertex(i, iVertex) * pv_vertex(k, iVertex) / areaCell(iCell)
+ vorticity_cell(k,iCell) = vorticity_cell(k,iCell) + kiteAreasOnVertex(i, iVertex) * vorticity(k, iVertex) / areaCell(iCell)
+ enddo
+ endif
+ enddo
+ enddo
+
+
+ !
+ ! Compute gradient of PV in normal direction
+ ! ( this computes gradPVn for all edges bounding real cells )
+ !
+ gradPVn(:,:) = 0.0
+ do iEdge = 1,nEdges
+ if( cellsOnEdge(1,iEdge) <= nCells .and. cellsOnEdge(2,iEdge) <= nCells) then
+ do k = 1,nVertLevels
+ gradPVn(k,iEdge) = (pv_cell(k,cellsOnEdge(2,iEdge)) - pv_cell(k,cellsOnEdge(1,iEdge))) / &
+ dcEdge(iEdge)
+ enddo
+ endif
+ enddo
+
+ ! Modify PV edge with upstream bias.
+ !
+ do iEdge = 1,nEdges
+ do k = 1,nVertLevels
+ pv_edge(k,iEdge) = pv_edge(k,iEdge) - config_apvm_upwinding * u(k,iEdge) * dt * gradPVn(k,iEdge)
+ enddo
+ enddo
+
+ !
+ ! set pv_edge = fEdge / h_edge at boundary points
+ !
+ ! if (maxval(boundaryEdge).ge.0) then
+ ! do iEdge = 1,nEdges
+ ! cell1 = cellsOnEdge(1,iEdge)
+ ! cell2 = cellsOnEdge(2,iEdge)
+ ! do k = 1,nVertLevels
+ ! if(boundaryEdge(k,iEdge).eq.1) then
+ ! v(k,iEdge) = 0.0
+ ! if(cell1.gt.0) then
+ ! h1 = h(k,cell1)
+ ! pv_edge(k,iEdge) = fEdge(iEdge) / h1
+ ! h_edge(k,iEdge) = h1
+ ! else
+ ! h2 = h(k,cell2)
+ ! pv_edge(k,iEdge) = fEdge(iEdge) / h2
+ ! h_edge(k,iEdge) = h2
+ ! endif
+ ! endif
+ ! enddo
+ ! enddo
+ ! endif
+
+
+ end subroutine compute_solve_diagnostics
+
+
+ subroutine enforce_boundaryEdge(tend, grid)
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+ ! Enforce any boundary conditions on the normal velocity at each edge
+ !
+ ! Input: grid - grid metadata
+ !
+ ! Output: tend_u set to zero at boundaryEdge == 1 locations
+ !!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
+
+
+ implicit none
+
+ type (tend_type), intent(inout) :: tend
+ type (mesh_type), intent(in) :: grid
+
+ integer, dimension(:,:), pointer :: boundaryEdge
+ real (kind=RKIND), dimension(:,:), pointer :: tend_u
+ integer :: nCells, nEdges, nVertices, nVertLevels
+ integer :: iEdge, k
+
+ nCells = grid % nCells
+ nEdges = grid % nEdges
+ nVertices = grid % nVertices
+ nVertLevels = grid % nVertLevels
+
+ boundaryEdge => grid % boundaryEdge % array
+ tend_u => tend % u % array
+
+ if(maxval(boundaryEdge).le.0) return
+
+ do iEdge = 1,nEdges
+ do k = 1,nVertLevels
+
+ if(boundaryEdge(k,iEdge).eq.1) then
+ tend_u(k,iEdge) = 0.0
+ endif
+
+ enddo
+ enddo
+
+ end subroutine enforce_boundaryEdge
+
+
+end module time_integration
</font>
</pre>