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ca7e2904cf
* Fix deprecation warnings from tests * Refactor tests so that ´@testset` is usually called in master file `runtests.jl`, not inside test file. Later on we can convert tests to examples. * Syntax of tests now follow more closely syntax used currently in JuliaFEM. We have had earlier studies with different kind of syntaxes, now we have kind of explicit way to do things.
68 lines
2.1 KiB
Julia
68 lines
2.1 KiB
Julia
# This file is a part of JuliaFEM.
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# License is MIT: see https://github.com/JuliaFEM/JuliaFEM.jl/blob/master/LICENSE.md
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using JuliaFEM, Test
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abstract type PlaneStressElasticityProblem <: AbstractProblem end
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function PlaneStressElasticityProblem(dim::Int=2, elements=[])
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return Problem{PlaneStressElasticityProblem}(dim, elements)
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end
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function get_unknown_field_name(::Type{P}) where P<:PlaneStressElasticityProblem
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return "displacement"
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end
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function get_unknown_field_type(::Type{P}) where P<:PlaneStressElasticityProblem
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return Vector{Float64}
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end
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function get_residual_vector(problem::Problem{PlaneStressElasticityProblem}, element::Element, ip::IntegrationPoint, time::Number; variation=nothing)
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basis = element(ip, time)
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dbasis = element(ip, time, Val{:grad})
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# material parameters
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E = element("youngs modulus", ip, time)
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nu = element("poissons ratio", ip, time)
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mu = E/(2*(1+nu))
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la = E*nu/((1+nu)*(1-2*nu))
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la = 2*la*mu/(la + 2*mu) # <- correction for 2d
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# elasticity formulation
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u = element("displacement", ip, time, variation)
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gradu = element("displacement", ip, time, Val{:grad}, variation)
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F = I + gradu
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E = 1/2*(F'*F - I)
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S = la*trace(E)*I + 2*mu*E
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r = F*S*dbasis
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b = element("displacement volume load", ip, time)
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r -= b*basis
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return vec(r)
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end
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function test_residual_form()
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# create model -- start
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element = Quad4([1, 2, 3, 4])
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element["geometry"] = Vector[[0.0,0.0], [10.0,0.0], [10.0,1.0], [0.0,1.0]]
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element["youngs modulus"] = 500.0
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element["poissons ratio"] = 0.3
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element["displacement volume load"] = Vector[[0.0,-10.0], [0.0,-10.0], [0.0,-10.0], [0.0,-10.0]]
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element["displacement"] = (0.0 => Vector{Float64}[zeros(2) for i=1:length(element)])
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problem = PlaneStressElasticityProblem()
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push!(problem, element)
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# create model -- end
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free_dofs = [3, 4, 5, 6]
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solve!(problem, free_dofs, 0.0) # launch a newton solver for single element
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disp = element("displacement", [1.0, 1.0], 0.0)
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@info("displacement at tip: $disp")
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# verified using Code Aster.
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@test isapprox(disp[2], -8.77303119819776E+00)
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end
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