Files
JuliaFEM.jl/src/problems_elasticity.jl
T
Jukka Aho 01f8d4afcd refactor: Remove Parameters.jl and TimerOutputs.jl usage
Changes:
- problems_elasticity.jl: Replaced Parameters.@with_kw and @unpack with manual code
- problems_heat.jl: Similar Parameters.jl removal
- solvers_modal.jl: Changed 'using Arpack' to 'import Arpack' (file commented out)

Added no-op @timeit macro in JuliaFEM.jl to replace TimerOutputs.

Result: Two fewer dependencies removed.
2025-11-08 14:33:51 +02:00

595 lines
20 KiB
Julia

# This file is a part of JuliaFEM.
# License is MIT: see https://github.com/JuliaFEM/JuliaFEM.jl/blob/master/LICENSE.md
""" Elasticity equations.
Field equation is:
m∂²u/∂t² = ∇⋅σ - b
Weak form is: find u∈U such that ∀v in V
δW := ∫ρ₀∂²u/∂t²⋅δu dV₀ + ∫S:δE dV₀ - ∫b₀⋅δu dV₀ - ∫t₀⋅δu dA₀ = 0
where
ρ₀ = density
b₀ = displacement load
t₀ = displacement traction
Formulations
------------
plane stress, plane strain, 3D
References
----------
https://en.wikipedia.org/wiki/Linear_elasticity
https://en.wikipedia.org/wiki/Finite_strain_theory
https://en.wikipedia.org/wiki/Stress_measures
https://en.wikipedia.org/wiki/Mooney%E2%80%93Rivlin_solid
https://en.wikipedia.org/wiki/Strain_energy_density_function
https://en.wikipedia.org/wiki/Plane_stress
https://en.wikipedia.org/wiki/Hooke's_law
"""
mutable struct Elasticity <: FieldProblem
# these are found from problem.properties for type Problem{Elasticity}
formulation::Symbol
finite_strain::Bool
geometric_stiffness::Bool
store_fields::Vector{Symbol}
end
function Elasticity()
# formulations: plane_stress, plane_strain, continuum
return Elasticity(:continuum, false, false, [])
end
function get_unknown_field_name(problem::Problem{Elasticity})
return "displacement"
end
function get_formulation_type(problem::Problem{Elasticity})
return :incremental
end
"""
assemble!(assembly:Assembly, problem::Problem{Elasticity}, elements, time)
Start finite element assembly procedure for Elasticity problem.
Function groups elements to arrays by their type and assembles one element type
at time. This makes it possible to pre-allocate matrices common to same type
of elements.
"""
function assemble!(assembly::Assembly, problem::Problem{Elasticity},
elements::Vector{Element}, time)
formulation = Val{problem.properties.formulation}
for (element_type, elements_subset) in group_by_element_type(elements)
assemble!(assembly, problem, elements_subset, time, formulation)
end
end
function assemble!(assembly::Assembly, problem::Problem{Elasticity},
elements::Vector{T}, time, formulation) where {T<:Element}
# Normal assembly (parallel assembly disabled for now - needs property fields)
local_buffer = allocate_buffer(problem, elements)
for i in 1:length(elements)
assemble_element!(assembly, problem, elements[i], local_buffer, time, formulation)
end
end
include("problems_elasticity_2d.jl")
const Elasticity3DSurfaceElements = Union{Poi1,Tri3,Tri6,Quad4,Quad8,Quad9}
const Elasticity3DVolumeElements = Union{Tet4,Pyr5,Wedge6,Wedge15,Hex8,Tet10,Hex20,Hex27}
function initialize_internal_params!(params, ip, type_) #::Type{Val{:type_2d}})
param_keys = keys(params)
all_keys = ip.fields.keys
ip_fields = filter(x -> isassigned(all_keys, x), collect(1:length(all_keys)))
if !("params_initialized" in ip_fields)
for key in param_keys
update!(ip, key, 0.0 => params[key])
end
if type_ == Val{:type_2d}
update!(ip, "stress", 0.0 => [0.0, 0.0, 0.0])
update!(ip, "strain", 0.0 => [0.0, 0.0, 0.0])
elseif type_ == Val{:type_3d}
update!(ip, "stress", 0.0 => [0.0, 0.0, 0.0, 0.0, 0.0, 0.0])
update!(ip, "strain", 0.0 => [0.0, 0.0, 0.0, 0.0, 0.0, 0.0])
else
error("daa")
end
update!(ip, "prev_time", 0.0 => 0.0)
update!(ip, "params_initialized", 0.0 => true)
end
end
# Buffer for elasticity assembly (keyword constructor without Parameters.jl)
struct Elasticity3DLocalBuffers{B,T}
ndofs::Int
dim::Int
bi::BasisInfo{B,T}
BL::Matrix{T}
BNL::Matrix{T}
Km::Matrix{T}
Kg::Matrix{T}
f_int::Vector{T}
f_ext::Vector{T}
f_buffer::Vector{T}
f_buffer_dim::Vector{T}
gdofs::Vector{Int}
gradu::Matrix{T}
strain::Matrix{T}
strain_vec::Vector{T}
stress_vec::Vector{T}
F::Matrix{T}
D::Matrix{T}
Dtan::Matrix{T}
Bt_mul_D::Matrix{T}
Bt_mul_D_mul_B::Matrix{T}
Bt_mul_S::Vector{T}
# Keyword constructor
function Elasticity3DLocalBuffers(; ndofs::Int, dim::Int, bi::BasisInfo{B,T}) where {B,T}
new{B,T}(
ndofs, dim, bi,
zeros(T, 6, ndofs), # BL
zeros(T, 9, ndofs), # BNL
zeros(T, ndofs, ndofs), # Km
zeros(T, ndofs, ndofs), # Kg
zeros(T, ndofs), # f_int
zeros(T, ndofs), # f_ext
zeros(T, ndofs), # f_buffer
zeros(T, div(ndofs, dim)), # f_buffer_dim
zeros(Int, ndofs), # gdofs
zeros(T, dim, dim), # gradu
zeros(T, dim, dim), # strain
zeros(T, 6), # strain_vec
zeros(T, 6), # stress_vec
zeros(T, dim, dim), # F
zeros(T, 6, 6), # D
zeros(T, 6, 6), # Dtan
zeros(T, ndofs, 6), # Bt_mul_D
zeros(T, ndofs, ndofs), # Bt_mul_D_mul_B
zeros(T, ndofs) # Bt_mul_S
)
end
end
function allocate_buffer(problem::Problem{Elasticity}, ::Vector{Element{El}}) where El<:Elasticity3DVolumeElements
dim = get_unknown_field_dimension(problem)
nnodes = length(El)
ndofs = dim * nnodes
return Elasticity3DLocalBuffers(ndofs=ndofs, dim=dim, bi=BasisInfo(El))
end
function reset_element!(buf::Elasticity3DLocalBuffers)
fill!(buf.Km, 0.0)
fill!(buf.Kg, 0.0)
fill!(buf.f_int, 0.0)
fill!(buf.f_ext, 0.0)
return
end
function reset_integration_point!(buf::Elasticity3DLocalBuffers)
fill!(buf.F, 0.0)
fill!(buf.strain, 0.0)
fill!(buf.D, 0.0)
fill!(buf.BL, 0.0)
fill!(buf.BNL, 0.0)
return
end
function to_voigt!(strain_vec, strain)
strain_vec[1] = strain[1, 1]
strain_vec[2] = strain[2, 2]
strain_vec[3] = strain[3, 3]
strain_vec[4] = 2.0 * strain[1, 2]
strain_vec[5] = 2.0 * strain[2, 3]
strain_vec[6] = 2.0 * strain[1, 3]
return
end
const u = ([0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0], [0.0, 0.0, 0.0])
const X = ([-93.7197, -93.7197, 150.883], [-91.657, -85.8251, 157.885], [-100.523, -88.8309, 157.883], [-91.6593, -88.8309, 157.883], [-92.6883, -89.7724, 154.384], [-96.0902, -87.328, 157.883], [-97.1216, -91.2753, 154.383], [-92.6895, -91.2753, 154.383], [-91.6581, -87.328, 157.883], [-96.0914, -88.8309, 157.883])
const displacement_load_string = [string("displacement load ", i) for i in 1:3]
""" Assemble 3d continuum elements in general solid mechanics problem. """
function assemble_element!(assembly::Assembly,
assembler::AssemblerSparsityPattern,
problem::Problem{Elasticity},
element::Element{El},
local_buffer::Elasticity3DLocalBuffers,
time, ::Type{Val{:continuum}},
use_csc=false) where El<:Elasticity3DVolumeElements
cheating = false
props = problem.properties
dim = get_unknown_field_dimension(problem)
nnodes = length(El)
ndofs = dim * nnodes
# Unpack buffer fields (replaced Parameters.@unpack)
bi = local_buffer.bi
BL = local_buffer.BL
BNL = local_buffer.BNL
Km = local_buffer.Km
Kg = local_buffer.Kg
f_int = local_buffer.f_int
f_ext = local_buffer.f_ext
f_buffer = local_buffer.f_buffer
f_buffer_dim = local_buffer.f_buffer_dim
gdofs = local_buffer.gdofs
gradu = local_buffer.gradu
strain = local_buffer.strain
strain_vec = local_buffer.strain_vec
stress_vec = local_buffer.stress_vec
F = local_buffer.F
D = local_buffer.D
Dtan = local_buffer.Dtan
Bt_mul_D = local_buffer.Bt_mul_D
Bt_mul_D_mul_B = local_buffer.Bt_mul_D_mul_B
Bt_mul_S = local_buffer.Bt_mul_S
if !cheating
u = element("displacement", time)
X = element("geometry", time)
end
reset_element!(local_buffer)
for ip in get_integration_points(element)
reset_integration_point!(local_buffer)
eval_basis!(bi, X, ip)
w = ip.weight * bi.detJ
N = bi.N
dN = bi.grad # deriatives of basis functions w.r.t. X, i.e. ∂N/∂X
grad!(bi, gradu, u) # displacement gradient ∇u
# calculate strain tensor and deformation gradient
#F[:,:] += I
for i in 1:dim
F[i, i] += 1.0
end
if props.finite_strain
strain[:, :] = 1 / 2 * (gradu + gradu' + gradu' * gradu)
F[:, :] += gradu
else
strain[:, :] .= 1 / 2 .* (gradu .+ gradu')
end
to_voigt!(strain_vec, strain)
# material stiffness start
if props.finite_strain
for i = 1:nnodes
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
else
for i = 1:nnodes
BL[1, 3*(i-1)+1] = dN[1, i]
BL[2, 3*(i-1)+2] = dN[2, i]
BL[3, 3*(i-1)+3] = dN[3, i]
BL[4, 3*(i-1)+1] = dN[2, i]
BL[4, 3*(i-1)+2] = dN[1, i]
BL[5, 3*(i-1)+2] = dN[3, i]
BL[5, 3*(i-1)+3] = dN[2, i]
BL[6, 3*(i-1)+1] = dN[3, i]
BL[6, 3*(i-1)+3] = dN[1, i]
end
end
# calculate stress
if cheating
E = 200e3
nu = 0.3
else
E = element("youngs modulus", ip, time)::Float64
nu = element("poissons ratio", ip, time)::Float64
end
la = E * nu / ((1.0 + nu) * (1.0 - 2.0 * nu))
mu = E / (2.0 * (1.0 + nu))
D[1, 1] = D[2, 2] = D[3, 3] = 2 * mu + la
D[4, 4] = D[5, 5] = D[6, 6] = mu
D[1, 2] = D[2, 1] = D[2, 3] = D[3, 2] = D[1, 3] = D[3, 1] = la
# determine material model
material_model = :linear_elasticity
if haskey(element, "plasticity")
material_model = :ideal_plasticity
end
# calculate stress vector based on material model
if material_model == :linear_elasticity
copyto!(Dtan, D)
mul!(stress_vec, Dtan, strain_vec)
end
if material_model == :ideal_plasticity
plastic_def = element("plasticity")[ip.id]
calculate_stress! = plastic_def["type"]
yield_surface_ = plastic_def["yield_surface"]
params = plastic_def["params"]
initialize_internal_params!(params, ip, Val{:type_3d})
if time == 0.0
error("Given step time = $(time). Please select time > 0.0")
end
t_last = ip("prev_time", time)
update!(ip, "prev_time", time => t_last)
dt = time - t_last
stress_last = ip("stress", t_last)
strain_last = ip("strain", t_last)
dstrain_vec = strain_vec - strain_last
fill!(stress_vec, 0.0)
fill!(Dtan, 0.0)
plastic_strain = [0.0, 0.0, 0.0, 0.0, 0.0, 0.0]
calculate_stress!(stress_vec, stress_last, dstrain_vec, plastic_strain, D, params, Dtan, yield_surface_, time, dt, Val{:type_3d})
end
:strain in props.store_fields && update!(ip, "strain", time => strain_vec)
:stress in props.store_fields && update!(ip, "stress", time => stress_vec)
:stress11 in props.store_fields && update!(ip, "stress11", time => stress_vec[1])
:stress22 in props.store_fields && update!(ip, "stress22", time => stress_vec[2])
:stress33 in props.store_fields && update!(ip, "stress33", time => stress_vec[3])
:stress12 in props.store_fields && update!(ip, "stress12", time => stress_vec[4])
:stress23 in props.store_fields && update!(ip, "stress23", time => stress_vec[5])
:stress13 in props.store_fields && update!(ip, "stress13", time => stress_vec[6])
:plastic_strain in props.store_fields && update!(ip, "plastic_strain", time => plastic_strain)
#Km += w*BL'*Dtan*BL
mul!(Bt_mul_D, transpose(BL), Dtan)
mul!(Bt_mul_D_mul_B, Bt_mul_D, BL)
rmul!(Bt_mul_D_mul_B, w)
for i = 1:ndofs^2
@inbounds Km[i] += Bt_mul_D_mul_B[i]
end
# material stiffness end
if props.geometric_stiffness
# take geometric stiffness into account
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] = stress_vec[1]
S3[2, 2] = stress_vec[2]
S3[3, 3] = stress_vec[3]
S3[1, 2] = S3[2, 1] = stress_vec[4]
S3[2, 3] = S3[3, 2] = stress_vec[5]
S3[1, 3] = S3[3, 1] = stress_vec[6]
S3[4:6, 4:6] = S3[7:9, 7:9] = S3[1:3, 1:3]
Kg += w * BNL' * S3 * BNL
end
# internal load
mul!(Bt_mul_S, transpose(BL), stress_vec)
rmul!(Bt_mul_S, w)
f_int .+= Bt_mul_S
# external load start
if haskey(element, "displacement load")
T = element("displacement load", ip, time)::Vector{Float64}
mul!(f_buffer, w, vec(T * N))
f_ext .+= f_buffer
end
for i = 1:dim
if haskey(element, displacement_load_string[i])
b = element(displacement_load_string[i], ip, time)::Float64
mul!(f_buffer_dim, w, N)
for (i, j) in enumerate(1:dim:length(f_ext))
f_ext[j] = b * f_buffer_dim[i]
end
end
end
# external load end
end
FEMBase.get_gdofs!(gdofs, problem, element)
# Update f_ext in place to be f_ext - f_int
f_ext .-= f_int
if use_csc
# add contributions to K, Kg, f
@inbounds assemble_local!(assembler, gdofs, Km, f_ext)
if props.geometric_stiffness
@inbounds assemble_local_matrix!(assembler, gdofs, Kg)
end
else
add!(assembly.f, gdofs, f_ext)
add!(assembly.K, gdofs, gdofs, Km)
if props.geometric_stiffness
add!(assembly.Kg, gdofs, gdofs, Kg)
end
end
return nothing
end
""" Elasticity equations, surface traction for continuum formulation. """
function assemble!(assembly::Assembly,
problem::Problem{Elasticity},
elements::Vector{Element{El}},
time, ::Type{Val{:continuum}}) where El<:Elasticity3DSurfaceElements
props = problem.properties
dim = get_unknown_field_dimension(problem)
for element in elements
nnodes = size(element, 2)
f = zeros(dim * nnodes)
has_concentrated_forces = false
for ip in get_integration_points(element)
detJ = element(ip, time, Val{:detJ})
w = ip.weight * detJ
N = element(ip, time)
if haskey(element, "displacement traction force")
T = element("displacement traction force", ip, time)
f += w * vec(T * N)
end
for i in 1:dim
if haskey(element, "displacement traction force $i")
T = element("displacement traction force $i", ip, time)
f[i:dim:end] += w * vec(T * N)
end
if haskey(element, "concentrated force $i")
has_concentrated_forces = true
T = element("concentrated force $i", ip, time)
f[i:dim:end] += w * vec(T * N)
end
end
if haskey(element, "surface pressure")
J = element(ip, time, Val{:Jacobian})'
n = cross(J[:, 1], J[:, 2])
n /= norm(n)
# sign convention, positive pressure is towards surface
p = -element("surface pressure", ip, time)
f += w * p * vec(n * N)
end
end
if has_concentrated_forces
update!(element, "concentrated force", time => Any[f])
end
gdofs = get_gdofs(problem, element)
add!(assembly.f, gdofs, f)
end
end
"""
assemble!(assembly, problem, elements, time, ::Type{Val{:continuum}})
Assemble all other elements for continuum elasticity problems. Basically, throw
an exception telling to filter invalid elements out from the element set.
"""
function assemble!(assembly::Assembly,
problem::Problem{Elasticity},
elements::Vector{Element{El}},
time, ::Type{Val{:continuum}}) where El
@info("It looks that you are trying to assemble elements of type $El to 3d continuum " *
"problem. However, they are not supported yet. To filter out elements from a " *
"element set, try `filter(element->!isa(element, Element{$El}), elements)`")
error("Tried to assemble unsupported elements of type $El to 3d continuum problem.")
end
""" Return strain tensor. """
function get_strain_tensor(problem, element, ip, time)
gradu = element("displacement", ip, time, Val{:Grad})
eps = 0.5 * (gradu' + gradu)
return eps
end
""" Return stress tensor. """
function get_stress_tensor(problem, element, ip, time)
eps = get_strain_tensor(problem, element, ip, time)
E = element("youngs modulus", ip, time)
nu = element("poissons ratio", ip, time)
mu = E / (2.0 * (1.0 + nu))
la = E * nu / ((1.0 + nu) * (1.0 - 2.0 * nu))
S = la * tr(eps) * I + 2.0 * mu * eps
return S
end
""" Return stain vector in "ABAQUS" order 11, 22, 33, 12, 23, 13. """
function get_strain_vector(problem, element, ip, time)
eps = get_strain_tensor(problem, element, ip, time)
return [eps[1, 1], eps[2, 2], eps[3, 3], eps[1, 2], eps[2, 3], eps[1, 3]]
end
""" Return stress vector in "ABAQUS" order 11, 22, 33, 12, 23, 13. """
function get_stress_vector(problem, element, ip, time)
S = get_stress_tensor(problem, element, ip, time)
return [S[1, 1], S[2, 2], S[3, 3], S[1, 2], S[2, 3], S[1, 3]]
end
""" Make least squares fit for some field to nodes. """
function lsq_fit(problem, elements, field, time)
A = SparseMatrixCOO()
b = SparseMatrixCOO()
volume = 0.0
for element in elements
gdofs = get_connectivity(element)
for ip in get_integration_points(element)
detJ = element(ip, time, Val{:detJ})
w = ip.weight * detJ
N = element(ip, time)
f = field(problem, element, ip, time)
add!(A, gdofs, gdofs, w * kron(N', N))
for i = 1:length(f)
add!(b, gdofs, w * f[i] * N, i)
end
volume += w
end
end
A = sparse(A)
b = sparse(b)
A = 1 / 2 * (A + A')
nz = get_nonzero_rows(A)
F = ldlt(A[nz, nz])
x = F \ b[nz, :]
nodal_values = Dict(node_id => Vector(x[idx, :]) for (idx, node_id) in enumerate(nz))
return nodal_values
end
""" Postprocessing, extrapolate strain to nodes using least-squares fit. """
function postprocess!(problem::Problem{Elasticity}, time::Float64, ::Type{Val{:strain}})
elements = get_elements(problem)
strain = lsq_fit(problem, elements, get_strain_vector, time)
update!(elements, "strain", time => strain)
end
function postprocess!(problem::Problem{Elasticity}, time::Float64, ::Type{Val{:stress}})
elements = get_elements(problem)
stress = lsq_fit(problem, elements, get_stress_vector, time)
update!(elements, "stress", time => stress)
end