new style concrete problem

This commit is contained in:
Jukka Aho
2016-02-02 22:22:21 +02:00
parent fe98a75cbe
commit 60046942e5
4 changed files with 167 additions and 179 deletions
+71 -75
View File
@@ -6,13 +6,80 @@ abstract StandardBasis
abstract DualBasis
global const BiorthogonalBasis = DualBasis
function DirichletProblem(parent_field_name::ASCIIString, parent_field_dim::Int, dim::Int=1, elements=Element[]; basis=StandardBasis)
return BoundaryProblem{DirichletProblem{basis}}("dirichlet boundary", parent_field_name, parent_field_dim, dim, elements)
type Dirichlet <: AbstractProblem
dual_basis :: Bool
end
function DirichletProblem(problem_name::ASCIIString, parent_field_name::ASCIIString, parent_field_dim::Int, dim::Int=1, elements=Element[]; basis=StandardBasis)
return BoundaryProblem{DirichletProblem{basis}}(problem_name, parent_field_name, parent_field_dim, dim, elements)
function Dirichlet()
Dirichlet(true)
end
function assemble!(assembly::BoundaryAssembly, problem::BoundaryProblem{Dirichlet}, element::Element, time::Real)
@assert problem.properties.dual_basis
# get dimension and name of PARENT field
field_dim = problem.parent_field_dim
field_name = problem.parent_field_name
gdofs = get_gdofs(element, field_dim)
# calculate bi-orthogonal basis transformation matrix Ae
nnodes = size(element, 2)
De = zeros(nnodes, nnodes)
Me = zeros(nnodes, nnodes)
for ip in get_integration_points(element, Val{2})
w = ip.weight
J = get_jacobian(element, ip, time)
JT = transpose(J)
if size(JT, 2) == 1 # plane problem
w *= norm(JT)
else
w *= norm(cross(JT[:,1], JT[:,2]))
end
N = element(ip, time)
De += w*diagm(vec(N))
Me += w*N'*N
end
Ae = De*inv(Me)
# do the actual integration
for ip in get_integration_points(element, Val{2})
w = ip.weight
J = get_jacobian(element, ip, time)
JT = transpose(J)
if size(JT, 2) == 1 # plane problem
w *= norm(JT)
else
w *= norm(cross(JT[:,1], JT[:,2]))
end
N = element(ip, time)
Phi = (Ae*N')'
A = w*Phi'*N
A[abs(A) .< 1.0e-12] = 0
if haskey(element, field_name)
for i=1:field_dim
g = element(field_name, ip, time)
ldofs = gdofs[i:field_dim:end]
add!(assembly.C1, ldofs, ldofs, A)
add!(assembly.C2, ldofs, ldofs, A)
add!(assembly.g, ldofs, w*g*Phi')
end
else
for i=1:field_dim
ldofs = gdofs[i:field_dim:end]
if haskey(element, field_name*" $i")
g = element(field_name*" $i", ip, time)
add!(assembly.C1, ldofs, ldofs, A)
add!(assembly.C2, ldofs, ldofs, A)
add!(assembly.g, ldofs, w*g*Phi')
end
end
end
end
end
function assemble!(assembly::BoundaryAssembly, problem::BoundaryProblem{DirichletProblem}, element::Element, time::Real)
# get dimension and name of PARENT field
@@ -61,74 +128,3 @@ function assemble!(assembly::BoundaryAssembly, problem::BoundaryProblem{Dirichle
end
end
function assemble!(assembly::BoundaryAssembly, problem::BoundaryProblem{DirichletProblem{BiorthogonalBasis}}, element::Element, time::Real)
# get dimension and name of PARENT field
field_dim = problem.parent_field_dim
field_name = problem.parent_field_name
gdofs = get_gdofs(element, field_dim)
# calculate bi-orthogonal basis transformation matrix Ae
nnodes = size(element, 2)
De = zeros(nnodes, nnodes)
Me = zeros(nnodes, nnodes)
for ip in get_integration_points(element, Val{2})
w = ip.weight
J = get_jacobian(element, ip, time)
JT = transpose(J)
if size(JT, 2) == 1 # plane problem
w *= norm(JT)
else
w *= norm(cross(JT[:,1], JT[:,2]))
end
N = element(ip, time)
De += w*diagm(vec(N))
Me += w*N'*N
end
Ae = De*inv(Me)
# do the actual integration
for ip in get_integration_points(element, Val{2})
w = ip.weight
J = get_jacobian(element, ip, time)
JT = transpose(J)
if size(JT, 2) == 1 # plane problem
w *= norm(JT)
else
w *= norm(cross(JT[:,1], JT[:,2]))
end
N = element(ip, time)
Phi = (Ae*N')'
A = w*Phi'*N
A[abs(A) .< 1.0e-9] = 0
# C1 matrix is always the same
# for i=1:field_dim
# ldofs = gdofs[i:field_dim:end]
# add!(assembly.C1, ldofs, ldofs, A)
# end
if haskey(element, field_name)
# add all dimensions at once if defined element["blaa"] = 0.0
for i=1:field_dim
g = element(field_name, ip, time)
ldofs = gdofs[i:field_dim:end]
add!(assembly.C1, ldofs, ldofs, A)
add!(assembly.C2, ldofs, ldofs, A)
add!(assembly.g, ldofs, w*g*Phi')
end
else
for i=1:field_dim
ldofs = gdofs[i:field_dim:end]
if haskey(element, field_name*" $i")
g = element(field_name*" $i", ip, time)
add!(assembly.C1, ldofs, ldofs, A)
add!(assembly.C2, ldofs, ldofs, A)
add!(assembly.g, ldofs, w*g*Phi')
# else
# add!(assembly.D, ldofs, ldofs, A)
end
end
end
end
end
+82 -70
View File
@@ -3,6 +3,88 @@
# Linear elasticity
""" Concrete Elasticity type. """
type Elasticity <: AbstractProblem
plane_stress :: Bool
nonlinear_geometry :: Bool
end
function Elasticity()
Elasticity(false, false)
end
function get_unknown_field_name(::Type{Elasticity})
return "displacement"
end
function assemble!(assembly::Assembly, problem::Problem{Elasticity}, element::Element, time::Real)
# assemble plane stress problem
if problem.properties.plane_stress
return assemble!(assembly, problem, element, time, Val{:plane_stress})
end
end
""" Elasticity equations, plane stress. """
function assemble!(assembly::Assembly, problem::Problem{Elasticity}, element::Element, time::Real, ::Type{Val{:plane_stress}})
gdofs = get_gdofs(element, problem.dim)
ndim, nnodes = size(element)
B = zeros(3, 2*nnodes)
for ip in get_integration_points(element)
w = ip.weight
J = get_jacobian(element, ip, time)
N = element(ip, time)
if haskey(element, "youngs modulus") && haskey(element, "poissons ratio")
nu = element("poissons ratio", ip, time)
E_ = element("youngs modulus", ip, time)
C = E_/(1.0 - nu^2) .* [
1.0 nu 0.0
nu 1.0 0.0
0.0 0.0 (1.0-nu)/2.0]
dN = element(ip, time, Val{:grad})
fill!(B, 0.0)
for i=1:size(dN, 2)
B[1, 2*(i-1)+1] = dN[1,i]
B[2, 2*(i-1)+2] = dN[2,i]
B[3, 2*(i-1)+1] = dN[2,i]
B[3, 2*(i-1)+2] = dN[1,i]
end
Kt = w*B'*C*B*det(J)
add!(assembly.stiffness_matrix, gdofs, gdofs, Kt)
end
if haskey(element, "displacement load")
b = element("displacement load", ip, time)
add!(assembly.force_vector, gdofs, w*N'*b*det(J))
end
if haskey(element, "displacement traction force")
T = element("displacement traction force", ip, time)
L = w*T*N*norm(J)
add!(assembly.force_vector, gdofs, vec(L))
end
for dim in 1:problem.dim
if haskey(element, "displacement traction force $dim")
T = element("displacement traction force $dim", ip, time)
ldofs = gdofs[dim:problem.dim:end]
L = w*T*N*norm(J)
add!(assembly.force_vector, ldofs, vec(L))
end
end
if haskey(element, "displacement traction force N")
# surface pressure
p = zeros(2)
p[1] = element("displacement traction force N", ip, time)
R = element("normal-tangential coordinates", ip, time)
T = R'*p
L = w*T*N*norm(J)
add!(assembly.force_vector, gdofs, vec(L))
end
end
end
abstract LinearElasticityProblem <: ElasticityProblem
function LinearElasticityProblem(name="linear elasticity", dim::Int=3, elements=[])
@@ -84,76 +166,6 @@ function assemble!{E<:CG, P<:LinearElasticityProblem}(assembly::Assembly, proble
end
end
abstract PlaneStressLinearElasticityProblem <: LinearElasticityProblem
function PlaneStressLinearElasticityProblem(name="plane stress linear elasticity", dim::Int=2, elements=[])
return Problem{PlaneStressLinearElasticityProblem}(name, dim, elements)
end
""" Elasticity equations, plane stress. """
function assemble!{E<:CG, P<:PlaneStressLinearElasticityProblem}(assembly::Assembly, problem::Problem{P}, element::Element{E}, time::Real)
gdofs = get_gdofs(element, problem.dim)
ndim, nnodes = size(E)
B = zeros(3, 2*nnodes)
for ip in get_integration_points(element)
w = ip.weight
J = get_jacobian(element, ip, time)
N = element(ip, time)
if haskey(element, "youngs modulus") && haskey(element, "poissons ratio")
nu = element("poissons ratio", ip, time)
E_ = element("youngs modulus", ip, time)
C = E_/(1.0 - nu^2) .* [
1.0 nu 0.0
nu 1.0 0.0
0.0 0.0 (1.0-nu)/2.0]
dN = element(ip, time, Val{:grad})
fill!(B, 0.0)
for i=1:size(dN, 2)
B[1, 2*(i-1)+1] = dN[1,i]
B[2, 2*(i-1)+2] = dN[2,i]
B[3, 2*(i-1)+1] = dN[2,i]
B[3, 2*(i-1)+2] = dN[1,i]
end
Kt = w*B'*C*B*det(J)
add!(assembly.stiffness_matrix, gdofs, gdofs, Kt)
# solve residual, i.e. K du = K \ -(Ku(prev) - F)
# in first iteration u(prev) typically 0 -> no effect
# but if geometrical or material nonlinearities iterations are needed
# if haskey(element, "displacement")
# u_prev = element("displacement", time)
# u_prev = vec(u_prev)
# add!(assembly.force_vector, gdofs, -Kt*u_prev)
# end
end
if haskey(element, "displacement load")
b = element("displacement load", ip, time)
add!(assembly.force_vector, gdofs, w*N'*b*det(J))
end
if haskey(element, "displacement traction force")
T = element("displacement traction force", ip, time)
L = w*T*N*norm(J)
add!(assembly.force_vector, gdofs, vec(L))
end
for dim in 1:problem.dim
if haskey(element, "displacement traction force $dim")
T = element("displacement traction force $dim", ip, time)
ldofs = gdofs[dim:problem.dim:end]
L = w*T*N*norm(J)
add!(assembly.force_vector, ldofs, vec(L))
end
end
if haskey(element, "displacement traction force N")
# surface pressure
p = zeros(2)
p[1] = element("displacement traction force N", ip, time)
R = element("normal-tangential coordinates", ip, time)
T = R'*p
L = w*T*N*norm(J)
add!(assembly.force_vector, gdofs, vec(L))
end
end
end
###############################
# Plastic material #
+7 -5
View File
@@ -50,10 +50,11 @@ type FieldProblem{T}
dim :: Int
elements :: Vector{Element}
assembly :: FieldAssembly
properties :: T
end
function FieldProblem(problem_type::DataType, name::ASCIIString, dim::Int,
function FieldProblem(problem::DataType, name::ASCIIString, dim::Int,
elements=[])
FieldProblem{problem_type}(name, dim, elements, FieldAssembly())
FieldProblem{problem}(name, dim, elements, FieldAssembly(), problem())
end
@@ -124,14 +125,15 @@ type BoundaryProblem{T}
parent_field_dim :: Int
elements :: Vector{Element}
assembly :: BoundaryAssembly
properties :: T
end
function BoundaryProblem(problem_type::DataType,
function BoundaryProblem(problem::DataType,
name::ASCIIString,
parent_field_name::ASCIIString,
parent_field_dim::Int,
elements=[])
BoundaryProblem{problem_type}(name, parent_field_name, parent_field_dim,
elements, BoundaryAssembly())
BoundaryProblem{problem}(name, parent_field_name, parent_field_dim,
elements, BoundaryAssembly(), problem())
end
function update!{P}(problem::BoundaryProblem{P}, solution::Vector{Float64})
+7 -29
View File
@@ -2,9 +2,8 @@
# License is MIT: see https://github.com/JuliaFEM/JuliaFEM.jl/blob/master/LICENSE.md
using JuliaFEM.Test
using JuliaFEM.Core: Node, update!, Quad4, Seg2, PlaneStressLinearElasticityProblem,
assemble, FieldProblem, BoundaryProblem, DirichletProblem,
DirectSolver, DualBasis
using JuliaFEM.Core: Node, update!, Quad4, Seg2, assemble, BoundaryProblem,
Problem, Elasticity, Solver, Dirichlet
@testset "test 2d linear elasticity with surface load." begin
@@ -27,7 +26,8 @@ using JuliaFEM.Core: Node, update!, Quad4, Seg2, PlaneStressLinearElasticityProb
update!(element1, "poissons ratio", nu)
# update!(element2, "displacement traction force", [0.0, f])
update!(element2, "displacement traction force", Vector{Float64}[[0.0, f], [0.0, f]])
elasticity_problem = FieldProblem(PlaneStressLinearElasticityProblem, "block", 2)
elasticity_problem = Problem(Elasticity, "block", 2)
elasticity_problem.properties.plane_stress = true
push!(elasticity_problem, element1, element2)
# dirichlet boundary condition, symmetry
@@ -36,37 +36,15 @@ using JuliaFEM.Core: Node, update!, Quad4, Seg2, PlaneStressLinearElasticityProb
update!([sym13, sym23], "geometry", nodes)
update!(sym13, "displacement 2", 0.0)
update!(sym23, "displacement 1", 0.0)
#sym23["displacement 1"] = 0.0
#sym13["displacement 2"] = 0.0
# name, unknown field, unknown field dimension
boundary_problem = BoundaryProblem(DirichletProblem, "symmetry boundaries", "displacement", 2)
boundary_problem = BoundaryProblem(Dirichlet, "symmetry boundaries", "displacement", 2)
push!(boundary_problem, sym13, sym23)
solver = DirectSolver("solve block problem")
solver.solve_residual = false
solver = Solver("solve block problem")
push!(solver, elasticity_problem)
push!(solver, boundary_problem)
#=
add_linear_system_solver_posthook!(solver,
function (solver)
info("solution vector")
dump(solver.x)
end)
=#
call(solver, 0.0)
#=
free_dofs = Int64[3, 5, 6, 8]
ass = assemble(problem, 0.0)
f = full(ass.force_vector)
K = full(ass.stiffness_matrix)
u = zeros(2, 4)
u[free_dofs] = K[free_dofs, free_dofs] \ f[free_dofs]
info("result vector")
dump(u)
=#
call(solver)
u_disp = element1("displacement", [1.0, 1.0], 0.0)
info("Displacement = $u_disp")