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mlb_tmc_linsys_hvec.sif
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!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
!! Elmer Solver input file
!!
!! Vectorized Stokes solution for Midre Lovenbreen.
!! Including Semi-Lagrangian dating solver.
!!
!! All units are in m-MPa-year
!! Temperatures are in Kelvin
!!
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! switch that on for debugging only
! ---------------------------------
! check keywords warn
! echo on
!!!!!!!!!!!!!!!!!!!!!!!!!
! DEFINITIONS used in run
!!!!!!!!!!!!!!!!!!!!!!!!!!
$name="S_1995_DEMs_tmc_vec"
#MINH=20.0
#Tc = -1.0
#directmethod="mumps"
!---LUA BEGIN
! assert(loadfile('./icematerial.lua'))()
!---LUA END
!echo on
! Note that the Mesh2MeshSolver requires solver specific
! mesh and hence this must be different than primary mesh,
! even symlink is ok.
$restartdir="outline62_lc75"
$restartfile="s_1995_dems_init_2d.result"
! Temperature of the simulation in Celsius
! with the formula for A works only if T > -10
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! HEADER
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! Partitioned mesh
Header
Mesh DB "." "outline62_lc75"
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! CONSTANTS
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Constants
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! SIMULATION
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Simulation
Coordinate System = "Cartesian 3D"
Simulation Type = "Steady State"
! Internal extrusion parameters, may be altered.
Extruded Mesh Levels = Integer 9
Extruded Max Coordinate = Real 2000
! Coupled iterations between different solvers
!---------------------------------------------
Steady State Max Iterations = 20
Steady State Min Iterations = 1
Output Intervals = 0
! usually, Dirichlet BC's are initialized before everything else. Sometimes those
! conditions are dependent on solutions of earlier solvers; next line ensures that
! this is not an issue.
!-----------------------------------------
Initialize Dirichlet Conditions = Logical False
! Output files
! ------------
Post File = $name$.vtu
!vtu: Save Bulk Only = Logical True
!Scalars File = $name$.dat
!scalars: Parallel Reduce = Logical True
Output File = $name$.result
! Restart happens in Solver 1
Restart Before Initial Conditions = Logical True
Interpolation Passive Coordinate = Integer 3
! how verbose the solver should be
! 3 = Only warnings
! 32 = Maximum verbosity
!-------------------------------------------------------
Max Output Level = 5
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! SOLVER
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Solver 1
Exec Solver = before all
Equation = "InterpSolver"
! Perform the interpolation solver before all other solvers, only once.
Exec Solver = Before all
Procedure = "Mesh2MeshSolver" "Mesh2MeshSolver"
! Restart is always in a serial mesh
Mesh = -single $restartdir
Restart File = $restartfile
! We use the primary mesh an single process and unextruded
! We want to have unique copy of it.
Mesh Enforce Local Copy = Logical True
! These are the variables for restart
Restart Position = Integer 0
Restart Time = Real 2000.0
Restart Variable 1 = String "bedrockDEM"
Restart Variable 2 = String "surfaceDEM1995"
! Continue even if some node is not found, deal with problems!
Restart Error Continue = Logical True
! These are the variables to be mapped from 2D ThisMesh to 3D TargetMesh'
! All existing variables are automatically mapped.
! Variable 1 = "bedrockDEM"
! Variable 2 = "surfaceDEM1995"
! Ensures that we perform interpolation on plane
Interpolation Passive Coordinate = Integer 3
End
! Maps the constant-thickness mesh between given bedrock and surface topology
Solver 2
Exec Solver = "before simulation"
Equation = "MapCoordinate"
Procedure = "StructuredMeshMapper" "StructuredMeshMapper"
Active Coordinate = Integer 3
Displacement Mode = Logical False
Correct Surface = Logical True
Minimum Height = Real #MINH
Correct Surface Mask = String "Glaciated"
Dot Product Tolerance = 1.0e-3
! These are needed to host the variables that are read in
Variable = -nooutput "DummyMesh"
Exported Variable 1 = "bedrockDEM"
!Exported Variable 1 Mask = String "BedRock"
Exported Variable 2 = "surfaceDEM1995"
!Exported Variable 2 Mask = String "Surface"
End
! Computes height and depth assuming an extruded mesh.
Solver 3
Exec Solver = "before simulation"
Equation = "HeightDepth"
Procedure = "StructuredProjectToPlane" "StructuredProjectToPlane"
Active Coordinate = Integer 3
Operator 1 = depth
Operator 2 = height
End
! vectorized & threaded version of the Navier-Stokes solver.
Solver 4
!Exec Solver = "Never"
Equation = "Stokes-Vec"
Procedure = "IncompressibleNSVec" "IncompressibleNSSolver"
Div-Curl Discretization = Logical False
Optimize Bandwidth = Logical True
Flow Model = Stokes
Stabilization Method = String Stabilized
!Non-linear iteration settings:
!------------------------------
Nonlinear System Max Iterations = 1
Nonlinear System Convergence Tolerance = 1.0e-5
Nonlinear System Newton After Iterations = 10
Nonlinear System Newton After Tolerance = 1.0e-1
! Nonlinear System Relaxation Factor = 1.00
! Nonlinear System Reset Newton = Logical True
include linsys.sif
! Convergence on timelevel (not required here)
!---------------------------------------------
Steady State Convergence Tolerance = Real 1.0e-3
!Relative Integration Order = -1
Number of Integration Points = Integer 44 ! 21, 28, 44, 64, ...
! 1st iteration viscosity is constant
Constant-Viscosity Start = Logical True
! Some timing info
!Boundary Assembly Timing = Logical True
!Bulk Assembly Timing = Logical True
!Solver Timing = Logical True
!Linear System Timing = Logical True
End
!-----------------------------------------------------
! heat transfer limited by the pressure melting point
! as upper limit
!-----------------------------------------------------
Solver 5
! Exec Solver = "Never"
Equation = String "Relative Temperature Equation"
Procedure = "HeatSolveVec" "HeatSolver"
Variable = "Temperature"
! Linear System Solver = Iterative
! Linear System Iterative Method = BiCGStab
! Linear System Max Iterations = 500
Linear System Solver = Direct
Linear System Direct Method = #directmethod
! It seems that 21 Ip's is sufficient!
Element = p:1 b:3
Bubbles in Global System = False
Number of Integration Points = Integer 21 ! 21, 28, 44, 64, ...
Linear System Convergence Tolerance = 1.0e-8
Linear System Preconditioning = ILU1
Linear System Residual Output = 1
Nonlinear System Max Iterations = 100
Nonlinear System Convergence Tolerance = 1.0e-6
Apply Limiter = Logical True
Limiter Value Tolerance = Real 0.0001
Vector Assembly = Logical True
Solver Timing = Logical True
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! BODIES (i.e., domains to compute on)
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Body 1
Name = "glacier"
Equation = 1
Material = 1
Body Force = 1
Initial Condition = 1
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! EQUATION
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Equation 1
Active Solvers(5) = 1 2 3 4 5
Convection = "Computed"
Flow Solution Name = String "Flow Solution"
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! INITIAL CONDITIONS
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Initial Condition 1
! Initial velocity is not really needed when using newtonian start
Velocity 1 = 0.0
Velocity 2 = 0.0
Velocity 3 = 0.0
Temperature = Variable Coordinate 3 ! lapserate of -10/1000 C/m
Real
0.0 272.14
100.0 272.15
1000.0 263.15
End
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! BODY FORCE
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Body Force 1
Flow BodyForce 1 = 0.0
Flow BodyForce 2 = 0.0
Flow BodyForce 3 = #gravity
Temperature = Real 273.15
Temperature Condition =Variable Coordinate 3
Real
0.0 -1.0
399.9999 -1.0
400. 1.0
1000.0 1.0
End
Temperature Upper Limit = Real 273.15 ! we ignore pressure melting point
!Variable Coordinate 3
! Real lua "settemperate(tx[0])"
End
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
! MATERIAL
!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!!
Material 1
Name = "Ice"
Density = Real #rhoi*(yearinsec^(-2.0))*Pa2MPa
! First viscosity with newtonian fluid
! happens to give velocities of proper size
Viscosity = Real 1.0
! Nonnewtonian viscosity
Viscosity Model = String Glen
Glen Exponent = Real 3.0
Critical Shear Rate = Real 1.0E-10
! Paterson value in MPa^-3a^-1
Limit Temperature = Real -10.0
! those are already transferred to Mpa-m-a system
Rate Factor 1 = Real #A1
Rate Factor 2 = Real #A2
Activation Energy 1 = Real #Q1
Activation Energy 2 = Real #Q2
!------------------------------------
Glen Enhancement Factor = Real 1.0
Relative Temperature = Variable Temperature
Real lua "tx[0] - 273.15"
! Heat transfer stuff
Heat Capacity = Variable Temperature
Real lua "capacity(tx[0])*yearinsec^(2.0)"
! Real lua "capacity(tx[0])*yearinsec^(2.0)"
Heat Conductivity = Variable Temperature
Real lua "conductivity(tx[0])*yearinsec*Pa2MPa"
End
Boundary Condition 1
ComputeNormal = Logical False
Name = "sides1"
Target Boundaries(1) = 1
! no slip
!-------------------------
Velocity 1 = 0
Velocity 2 = 0
Velocity 3 = 0
End
Boundary Condition 2
ComputeNormal = Logical False
Name = "sides2"
Target Boundaries(1) = 2
! no slip
!-------------------------
Velocity 1 = 0
Velocity 2 = 0
Velocity 3 = 0
End
!! DON'T CHANGE ORDER OF NEXT 2 BC's!
!! They are automaticaly created in internal extrusion
!! bedrock:
Boundary Condition 3
ComputeNormal = Logical True
Name = "bedrock"
! No-slip velocity conditions
Velocity 1 = Real 0.0
Velocity 2 = Real 0.0
Velocity 3 = Real 0.0
Bottom Surface = Equals "bedrockDEM"
! Mask for creating the restart fields only where needed
! Refererred by: Exported Variable 1 Mask = ...
Bedrock = Logical True
Heat Flux = Real #0.050 * yearinsec * Pa2MPa
! 50 mW m^-2
End
Boundary Condition 4
ComputeNormal = Logical False
Name = "surface"
Top Surface = Equals "surfaceDEM1995"
! Referred by: Exported Variable 2 Mask = ...
Surface = Logical True
Temperature = Variable Coordinate 3 ! lapserate of -10/1000 C/m
Real
0.0 272.15
100.0 272.14
1000.0 263.15
End
End