Geometrically nonlinear formulation for 3d.

This commit is contained in:
Jukka Aho
2016-02-11 16:16:15 +02:00
parent 56a0ed04e1
commit 3fdb61d2a5
2 changed files with 145 additions and 129 deletions
+114 -56
View File
@@ -29,14 +29,14 @@ end
function assemble!(assembly::Assembly, problem::Problem{Elasticity}, element::Element, time::Real)
props = problem.properties
gdofs = get_gdofs(problem, element)
if props.formulation == :continuum
return assemble!(assembly, problem, element, time, Val{:continuum})
Kt, f = assemble(problem, element, time, Val{:continuum})
elseif (props.formulation == :plane_stress) || (props.formulation == :plane_strain)
gdofs = get_gdofs(problem, element)
Kt, f = assemble(problem, element, time, Val{:plane})
add!(assembly.K, gdofs, gdofs, Kt)
add!(assembly.f, gdofs, f)
end
add!(assembly.K, gdofs, gdofs, Kt)
add!(assembly.f, gdofs, f)
end
@@ -163,71 +163,129 @@ end
""" Elasticity equations, continuum formulation. """
function assemble!(assembly::Assembly, problem::Problem{Elasticity}, element::Element, time::Real, ::Type{Val{:continuum}})
function assemble{El<:Union{Tet4, Tet10, Hex8}}(problem::Problem{Elasticity}, element::Element{El}, time::Real, ::Type{Val{:continuum}})
props = problem.properties
dim = get_unknown_field_dimension(problem)
nnodes = size(element, 2)
BL = zeros(6, dim*nnodes)
BNL = zeros(9, dim*nnodes)
Kt = zeros(dim*nnodes, dim*nnodes)
f = zeros(dim*nnodes)
gdofs = get_gdofs(problem, element)
ndim, nnodes = size(element)
B = zeros(6, 3*nnodes)
for ip in get_integration_points(element)
w = ip.weight
J = get_jacobian(element, ip, time)
w = ip.weight*det(J)
N = element(ip, time)
if haskey(element, "youngs modulus") && haskey(element, "poissons ratio")
v = element("poissons ratio", ip, time)
E_ = element("youngs modulus", ip, time)
a = 1 - v
b = 1 - 2*v
c = 1 + v
C = E_/(b*c) .* [
a v v 0 0 0
v a v 0 0 0
v v a 0 0 0
0 0 0 b 0 0
0 0 0 0 b 0
0 0 0 0 0 b]
dN = element(ip, time, Val{:grad})
fill!(B, 0.0)
for i=1:size(dN, 2)
B[1, 3*(i-1)+1] = dN[1,i]
B[2, 3*(i-1)+2] = dN[2,i]
B[3, 3*(i-1)+3] = dN[3,i]
B[4, 3*(i-1)+1] = dN[2,i]
B[4, 3*(i-1)+2] = dN[1,i]
B[5, 3*(i-1)+2] = dN[3,i]
B[5, 3*(i-1)+3] = dN[2,i]
B[6, 3*(i-1)+1] = dN[3,i]
B[6, 3*(i-1)+3] = dN[1,i]
end
# L = b * B'
# D = 0.5 * (L' + L)
# F = ...
# E = 0.5 * (F'*F - I)
# de = E - E_last
# S = vonMisesStress(de, stress)
# K = B' * S * J * w
Kt = w*B'*C*B*det(J)
add!(assembly.K, gdofs, gdofs, Kt)
dN = element(ip, time, Val{:grad})
# kinematics; calculate deformation gradient and strain
F = eye(dim)
if haskey(element, "displacement")
gradu = element("displacement", ip, time, Val{:grad})
F += gradu
end
GL = 1/2*(F'*F - I) # green-lagrange strain
E = element("youngs modulus", ip, time)
nu = element("poissons ratio", ip, time)
a = 1 - nu
b = 1 - 2*nu
c = 1 + nu
D = E/(b*c) .* [
a nu nu 0 0 0
nu a nu 0 0 0
nu nu a 0 0 0
0 0 0 b 0 0
0 0 0 0 b 0
0 0 0 0 0 b]
# # PK2 stress tensor in voigt notation
S = D*[GL[1,1]; GL[2,2]; GL[3,3]; 2*GL[2,3]; 2*GL[1,3]; 2*GL[1,2]]
# add contributions: material and geometric stiffness + internal forces
fill!(BL, 0.0)
for i=1:size(dN, 2)
BL[1, 3*(i-1)+1] = F[1,1]*dN[1,i]
BL[1, 3*(i-1)+2] = F[2,1]*dN[1,i]
BL[1, 3*(i-1)+3] = F[3,1]*dN[1,i]
BL[2, 3*(i-1)+1] = F[1,2]*dN[2,i]
BL[2, 3*(i-1)+2] = F[2,2]*dN[2,i]
BL[2, 3*(i-1)+3] = F[3,2]*dN[2,i]
BL[3, 3*(i-1)+1] = F[1,3]*dN[3,i]
BL[3, 3*(i-1)+2] = F[2,3]*dN[3,i]
BL[3, 3*(i-1)+3] = F[3,3]*dN[3,i]
BL[4, 3*(i-1)+1] = F[1,1]*dN[2,i] + F[1,2]*dN[1,i]
BL[4, 3*(i-1)+2] = F[2,1]*dN[2,i] + F[2,2]*dN[1,i]
BL[4, 3*(i-1)+3] = F[3,1]*dN[2,i] + F[3,2]*dN[1,i]
BL[5, 3*(i-1)+1] = F[1,2]*dN[3,i] + F[1,3]*dN[2,i]
BL[5, 3*(i-1)+2] = F[2,2]*dN[3,i] + F[2,3]*dN[2,i]
BL[5, 3*(i-1)+3] = F[3,2]*dN[3,i] + F[3,3]*dN[2,i]
BL[6, 3*(i-1)+1] = F[1,3]*dN[1,i] + F[1,1]*dN[3,i]
BL[6, 3*(i-1)+2] = F[2,3]*dN[1,i] + F[2,1]*dN[3,i]
BL[6, 3*(i-1)+3] = F[3,3]*dN[1,i] + F[3,1]*dN[3,i]
end
fill!(BNL, 0.0)
for i=1:size(dN, 2)
BNL[1, 3*(i-1)+1] = dN[1,i]
BNL[2, 3*(i-1)+1] = dN[2,i]
BNL[3, 3*(i-1)+1] = dN[3,i]
BNL[4, 3*(i-1)+2] = dN[1,i]
BNL[5, 3*(i-1)+2] = dN[2,i]
BNL[6, 3*(i-1)+2] = dN[3,i]
BNL[7, 3*(i-1)+3] = dN[1,i]
BNL[8, 3*(i-1)+3] = dN[2,i]
BNL[9, 3*(i-1)+3] = dN[3,i]
end
S3 = zeros(3*dim, 3*dim)
S3[1,1] = S[1]
S3[2,2] = S[2]
S3[3,3] = S[3]
S3[2,3] = S3[3,2] = S[4]
S3[1,3] = S3[3,1] = S[5]
S3[1,2] = S3[2,1] = S[6]
S3[4:6,4:6] = S3[7:9,7:9] = S3[1:3,1:3]
Kt += w*(BL'*D*BL + BNL'*S3*BNL)
f -= w*BL'*S
# volume load
if haskey(element, "displacement load")
b = element("displacement load", ip, time)
add!(assembly.f, gdofs, w*N'*b*det(J))
T = element("displacement load", ip, time)
f += vec(w*T*N)
end
end
return Kt, f
end
""" Elasticity equations, surface traction for continuum formulation. """
function assemble{El<:Union{Tri3, Tri6, Quad4}}(problem::Problem{Elasticity}, element::Element{El}, time::Real, ::Type{Val{:continuum}})
props = problem.properties
dim = get_unknown_field_dimension(problem)
nnodes = size(element, 2)
Kt = zeros(dim*nnodes, dim*nnodes)
f = zeros(dim*nnodes)
for ip in get_integration_points(element)
JT = transpose(get_jacobian(element, ip, time))
N = element(ip, time)
w = ip.weight*norm(cross(JT[:,1], JT[:,2]))
if haskey(element, "displacement traction force")
T = element("displacement traction force", ip, time)
JT = transpose(J)
L = w*T*N*norm(cross(JT[:,1], JT[:,2]))
add!(assembly.f, gdofs, vec(L))
f += vec(w*T*N)
end
for dim in 1:get_unknown_field_dimension(problem)
if haskey(element, "displacement traction force $dim")
T = element("displacement traction force $dim", ip, time)
ldofs = gdofs[dim:unknown_field_dimension(problem):end]
JT = transpose(J)
L = w*T*N*norm(cross(JT[:,1], JT[:,2]))
add!(assembly.f, ldofs, vec(L))
for i in 1:dim
if haskey(element, "displacement traction force $i")
T = element("displacement traction force $i", ip, time)
f[i:dim:end] += vec(w*T*N)
end
end
end
return Kt, f
end
+31 -73
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@@ -2,7 +2,7 @@
# License is MIT: see https://github.com/JuliaFEM/JuliaFEM.jl/blob/master/LICENSE.md
using JuliaFEM.Test
using JuliaFEM.Core: Node, update!, Quad4, Seg2, Problem, Elasticity, Solver, Dirichlet
using JuliaFEM.Core: Node, update!, Quad4, Seg2, Hex8, Problem, Elasticity, Solver, Dirichlet
using JuliaFEM.Preprocess: aster_parse_nodes
@testset "test 2d linear elasticity with surface load" begin
@@ -40,7 +40,7 @@ using JuliaFEM.Preprocess: aster_parse_nodes
# type, name, dimension, unknown_field_name
boundary_problem = Problem(Dirichlet, "symmetry boundaries", 2, "displacement")
push!(boundary_problem, sym13, sym23)
solver = Solver("solve block problem")
solver.is_linear_system = true # to get linear solution
push!(solver, elasticity_problem)
@@ -95,87 +95,45 @@ end
@testset "test continuum linear elasticity with surface load" begin
nodes = JuliaFEM.Preprocess.aster_parse_nodes("""
COOR_3D
N1 0.0 0.0 0.0
N2 1.0 0.0 0.0
N3 1.0 1.0 0.0
N4 0.0 1.0 0.0
N5 0.0 0.0 1.0
N6 1.0 0.0 1.0
N7 1.0 1.0 1.0
N8 0.0 1.0 1.0
FINSF
""")
nodes = Dict{Int64, Node}(
1 => [0.0, 0.0, 0.0],
2 => [1.0, 0.0, 0.0],
3 => [1.0, 1.0, 0.0],
4 => [0.0, 1.0, 0.0],
5 => [0.0, 0.0, 1.0],
6 => [1.0, 0.0, 1.0],
7 => [1.0, 1.0, 1.0],
8 => [0.0, 1.0, 1.0])
function set_geometry!(element, nodes)
element["geometry"] = Vector{Float64}[nodes[i] for i in get_connectivity(element)]
end
element1 = Hex8([1, 2, 3, 4, 5, 6, 7, 8])
set_geometry!(element1, nodes)
element1["youngs modulus"] = 900.0
element1["poissons ratio"] = 0.25
element1["displacement"] = (0.0 => Vector{Float64}[[0.0, 0.0, 0.0] for i=1:8])
element2 = Quad4([5, 6, 7, 8])
set_geometry!(element2, nodes)
element2["displacement traction force"] = Vector{Float64}[[0.0, 0.0, -100.0] for i=1:4]
element2["displacement"] = (0.0 => Vector{Float64}[[0.0, 0.0, 0.0] for i=1:4])
update!([element1, element2], "geometry", nodes)
update!([element1], "youngs modulus", 900.0)
update!([element1], "poissons ratio", 0.25)
update!([element2], "displacement traction force", Vector{Float64}[[0.0, 0.0, -100.0] for i=1:4])
problem = ElasticityProblem()
push!(problem, element1)
push!(problem, element2)
elasticity_problem = Problem(Elasticity, "solve continuum block", 3)
push!(elasticity_problem, element1)
push!(elasticity_problem, element2)
free_dofs = zeros(Bool, 8, 3)
x = 1
y = 2
z = 3
free_dofs[2, x] = true
free_dofs[3, [x, y]] = true
free_dofs[4, y] = true
free_dofs[5, z] = true
free_dofs[6, [x, z]] = true
free_dofs[7, [x, y, z]] = true
free_dofs[8, [y, z]] = true
free_dofs = find(vec(free_dofs'))
info("free dofs: $free_dofs")
symxy = Quad4([1, 2, 3, 4])
symxz = Quad4([1, 2, 6, 5])
symyz = Quad4([1, 4, 8, 5])
update!([symxy, symxz, symyz], "geometry", nodes)
symxy["displacement 3"] = 0.0
symxz["displacement 2"] = 0.0
symyz["displacement 1"] = 0.0
boundary_problem = Problem(Dirichlet, "symmetry boundary conditions", 3, "displacement")
push!(boundary_problem, symxy, symxz, symyz)
info("initial force vector")
ass = JuliaFEM.Core.assemble(problem, 0.0)
info(reshape(full(ass.force_vector), 3, 8))
info("initial stiffness matrix")
dump(round(Int, full(ass.stiffness_matrix))[free_dofs, free_dofs])
solve!(problem, free_dofs, 0.0; max_iterations=10)
#=
dx = Quad4([1, 4, 8, 5])
dx["displacement 1"] = 0.0
dy = Quad4([1, 5, 6, 2])
dy["displacement 2"] = 0.0
dz = Quad4([1, 2, 3, 4])
dz["displacement 3"] = 0.0
bc = DirichletProblem("displacement", 3)
for el in [dx, dy, dz]
set_geometry!(el, nodes)
push!(bc, el)
end
solver = JuliaFEM.Core.DirectSolver()
push!(solver, problem)
push!(solver, bc)
solver.dump_matrices = true
solver.name = "3d_hex8"
solver(0.0)
=#
solver = Solver("solve 3d block")
push!(solver, elasticity_problem)
push!(solver, boundary_problem)
call(solver)
disp = element1("displacement", [1.0, 1.0, 1.0], 0.0)
info("displacement at tip: $disp")
info("displacement on element: ")
for (i, d) in enumerate(element1("displacement", 0.0))
@printf "%d % f % f % f\n" [i;d]...
end
# verified using Code Aster.
# 2015-12-12-continuum-elasticity/vim c3d_grot_gdep_traction_force.comm
@test isapprox(disp, [3.17431158889468E-02, 3.17431158889468E-02, -1.38591518927826E-01])
#@test isapprox(disp, [2.80559539222183E-03, 2.80559539222183E-03, -1.13019918093242E-02])
end