added geometrically nonlinear option to 2d models

This commit is contained in:
Jukka Aho
2016-02-11 02:50:43 +02:00
parent de3383288a
commit 2cca0a5677
+122 -63
View File
@@ -5,13 +5,10 @@
type Elasticity <: FieldProblem
# these are found from problem.properties for type Problem{Elasticity}
formulation :: Symbol
nonlinear_geometry :: Bool
end
function Elasticity()
Elasticity(
:continuum, # formulations: :plane_stress, :continuum
false, # geometrically nonlinear analysis
)
# formulations: plane_stress, plane_strain, continuum
return Elasticity(:continuum)
end
# in case of experimenting new things;
@@ -25,81 +22,143 @@ function get_unknown_field_name(::Type{Elasticity})
return "displacement"
end
function get_formulation_type(problem::Problem{Elasticity})
info("INCREMENTAL FORMULATION")
return :incremental
end
function assemble!(assembly::Assembly, problem::Problem{Elasticity}, element::Element, time::Real)
f = problem.properties.formulation
if f == :continuum
props = problem.properties
if props.formulation == :continuum
return assemble!(assembly, problem, element, time, Val{:continuum})
elseif (f == :plane_stress) || (f == :plane_strain)
return assemble!(assembly, problem, element, time, Val{:plane})
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
end
""" Elasticity equations, plane stress formulation. """
function assemble!(assembly::Assembly, problem::Problem{Elasticity}, element::Element, time::Real, ::Type{Val{:plane}})
""" Elasticity equations for 2d cases. """
function assemble{El<:Union{Tri3,Tri6,Quad4}}(problem::Problem{Elasticity}, element::Element{El}, time::Real, ::Type{Val{:plane}})
props = problem.properties
gdofs = get_gdofs(problem, element)
ndim, nnodes = size(element)
B = zeros(3, 2*nnodes)
dim = get_unknown_field_dimension(problem)
nnodes = size(element, 2)
BL = zeros(3, dim*nnodes)
BNL = zeros(4, dim*nnodes)
Kt = zeros(dim*nnodes, dim*nnodes)
f = zeros(dim*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)
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
# constitutive equations; material model (isotropic linear material here)
# get_material(problem, element, ...)
E = element("youngs modulus", ip, time)
nu = element("poissons ratio", ip, time)
if props.formulation == :plane_stress
D = E/(1.0 - nu^2) .* [
1.0 nu 0.0
nu 1.0 0.0
0.0 0.0 (1.0-nu)/2.0]
elseif props.formulation == :plane_strain
D = E/((1+nu)*(1-2*nu)) .* [
1-nu nu 0
nu 1-nu 0
0 0 (1-2*nu)/2]
else
error("unknown plane formulation: $(props.formulation)")
end
S = D*[GL[1,1]; GL[2,2]; 2*GL[1,2]] # PK2 stress tensor in voigt notation
# add contributions: material and geometric stiffness + internal forces
fill!(BL, 0.0)
for i=1:size(dN, 2)
BL[1, 2*(i-1)+1] = F[1,1]*dN[1,i]
BL[1, 2*(i-1)+2] = F[2,1]*dN[1,i]
BL[2, 2*(i-1)+1] = F[1,2]*dN[2,i]
BL[2, 2*(i-1)+2] = F[2,2]*dN[2,i]
BL[3, 2*(i-1)+1] = F[1,1]*dN[2,i] + F[1,2]*dN[1,i]
BL[3, 2*(i-1)+2] = F[2,1]*dN[2,i] + F[2,2]*dN[1,i]
end
fill!(BNL, 0.0)
for i=1:size(dN, 2)
BNL[1, 2*(i-1)+1] = dN[1,i]
BNL[2, 2*(i-1)+1] = dN[2,i]
BNL[3, 2*(i-1)+2] = dN[1,i]
BNL[4, 2*(i-1)+2] = dN[2,i]
end
S2 = zeros(2*dim, 2*dim)
S2[1,1] = S[1]
S2[2,2] = S[2]
S2[1,2] = S2[2,1] = S[3]
S2[3:4,3:4] = S2[1:2,1:2]
Kt += w*(BL'*D*BL + BNL'*S2*BNL)
f -= w*BL'*S
# volume load
if haskey(element, "displacement load")
T = element("displacement load", ip, time)
f += vec(w*T*N)
end
end
return Kt, f
end
function assemble{El<:Union{Seg2,Seg3}}(problem::Problem{Elasticity}, element::Element{El}, time::Real, ::Type{Val{:plane}})
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)
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)
# Zienkiewicz, p. 91
if props.formulation == :plane_stress
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]
elseif props.formulation == :plane_strain
C = E_/((1+nu)*(1-2*nu)) .* [
1-nu nu 0
nu 1-nu 0
0 0 (1-2*nu)/2]
else
error("unknown plane formulation: $(props.formulation)")
end
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.K, gdofs, gdofs, Kt)
end
if haskey(element, "displacement load")
b = element("displacement load", ip, time)
add!(assembly.f, gdofs, w*N'*b*det(J))
end
w = ip.weight*norm(J)
if haskey(element, "displacement traction force")
T = element("displacement traction force", ip, time)
L = w*T*N*norm(J)
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:get_unknown_field_dimension(problem):end]
L = w*T*N*norm(J)
add!(assembly.f, ldofs, vec(L))
for i=1:dim
# traction force for ith component
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
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.f, gdofs, vec(L))
if haskey(element, "nt displacement traction force")
# traction force given in normal-tangential direction
T = element("nt displacement traction force", ip, time)
Q = element("normal-tangential coordinates", ip, time)
f += vec(w*Q'*T*N)
end
end
return Kt, f
end