Commit 91a2eec4 authored by Jeremy BLEYER's avatar Jeremy BLEYER

2D elasticity example

parent 77250941
......@@ -12,7 +12,7 @@ Contents:
:maxdepth: 2
intro
2D_elasticity
demo/elasticity/2D_elasticity.py.rst
demo/modal_analysis_dynamics/cantilever_modal.py.rst
demo/reissner_mindlin/reissner_mindlin.rst
......
.. # gedit: set fileencoding=utf8 :
.. _LinearElasticity2D::
=========================
2D linear elasticity
=========================
Introduction
------------
In this first numerical tour, we will show how to compute a small strain solution for
a 2D isotropic linear elastic medium, either in plane stress or in plane strain,
in a tradtional displacement-based finite element formulation. Extension to 3D
is straightforward and an example can be found in the :ref:`ModalAnalysis` example.
We consider here the case of a cantilever beam modeled as a 2D medium of dimensions
:math:`L\times H`. Geometrical parameters and mesh density are first defined
and the rectangular domain is generated using the ``RectangleMesh`` function.
We also choose a criss-crossed structured mesh::
from __future__ import print_function
from fenics import *
L = 25.
H = 1.
Nx = 250
Ny = 10
mesh = RectangleMesh(Point(0., 0.), Point(L, H), Nx, Ny, "crossed")
Constitutive relation
---------------------
We now define the material parameters which are here given in terms of a Young's
modulus :math:`E` and a Poisson coefficient :math:`\nu`. In the following, we will
need to define the constitutive relation between the stress tensor :math:`\boldsymbol{\sigma}`
and the strain tensor :math:`\boldsymbol{\varepsilon}`. Let us recall
that the general expression of the linear elastic isotropic constitutive relation
for a 3D medium is given by:
.. math::
\boldsymbol{\sigma} = \lambda \text{tr}(\boldsymbol{\varepsilon})\mathbf{1} + 2\mu\boldsymbol{\varepsilon}
:label: constitutive_3D
for a natural (no prestress) initial state where the Lamé coefficients are given by:
.. math::
\lambda = \dfrac{E\nu}{(1+\nu)(1-2\nu)}, \quad \mu = \dfrac{E}{2(1+\nu)}
:label: Lame_coeff
In this demo, we consider a 2D model either in plane strain or in plane stress conditions.
Irrespective of this choice, we will work only with a 2D displacement vector :math:`\boldsymbol{u}=(u_x,u_y)`
and will subsequently define the strain operator ``eps`` as follows::
def eps(v):
return sym(grad(v))
which computes the 2x2 plane components of the symmetrized gradient tensor of
any 2D vectorial field. In the plane strain case, the full 3D strain tensor is defined as follows:
.. math::
\boldsymbol{\varepsilon} = \begin{bmatrix} \varepsilon_{xx} & \varepsilon_{xy} & 0\\
\varepsilon_{xy} & \varepsilon_{yy} & 0 \\ 0 & 0 & 0\end{bmatrix}
so that the 2x2 plane part of the stress tensor is defined in the same way as for the 3D case
(the out-of-plane stress component being given by :math:`\sigma_{zz}=\lambda(\varepsilon_{xx}+\varepsilon_{yy})`.
In the plane stress case, an out-of-plane strain component :math:`\varepsilon_{zz}`
must be considered so that :math:`\sigma_{zz}=0`. Using this condition in the
3D constitutive relation, one has :math:`\varepsilon_{zz}=-\dfrac{\lambda}{\lambda+2\mu}(\varepsilon_{xx}+\varepsilon_{yy})`.
Injecting into :eq:`constitutive_3D`, we have for the 2D plane stress relation:
.. math::
\boldsymbol{\sigma} = \lambda^* \text{tr}(\boldsymbol{\varepsilon})\mathbf{1} + 2\mu\boldsymbol{\varepsilon}
where :math:`\boldsymbol{\sigma}, \boldsymbol{\varepsilon}, \mathbf{1}` are 2D tensors and with
:math:`\lambda^* = \dfrac{\lambda^2}{\lambda+\mu}`. Hence, the 2D constitutive relation
is identical to the plane strain case by changing only the value of the Lamé coefficient :math:`\lambda`
(equivalently, this corresponds to using a pseudo-Poisson coefficient :math:`\nu^*=\dfrac{\nu}{1-\nu}`
instead of :math:`\nu` when defining :math:`\lambda` in :eq:`Lame_coeff`). We can then have::
E = Constant(1e5)
nu = Constant(0.3)
model = "plane_stress"
mu = E/2/(1+nu)
lmbda = E*nu/(1+nu)/(1-2*nu)
if model == "plane_stress":
lmbda = lmbda**2/(lmbda+mu)
def sigma(v):
return lmbda*tr(eps(v))*Identity(2) + 2.0*mu*eps(v)
.. note::
Note that we used the variable name ``lmbda`` to avoid any confusion with the
lambda functions of Python
We also used an intrinsic formulation of the constitutive relation. Example of
constitutive relation implemented with a matrix/vector engineering notation
will be provided in the :ref:`OrthotropicElasticity` example.
Variational formulation
-----------------------
For this example, we consider a continuous polynomial interpolation of degree 2
and a uniformly distributed loading :math:`\boldsymbol{f}=(0,-f)` corresponding
to the beam self-weight. The continuum mechanics variational formulation (obtained
from the virtual work principle) is given by:
.. math::
\text{Find } \boldsymbol{u}\in V \text{ s.t. } \int_{\Omega}
\boldsymbol{\sigma}(\boldsymbol{u}):\boldsymbol{\varepsilon}(\boldsymbol{v}) d\Omega
= \int_{\Omega} \boldsymbol{f}\cdot\boldsymbol{v} d\Omega \quad \forall\boldsymbol{v} \in V
which translates into the following FEniCS code::
rho_g = 1e-3
f = Constant((0,-rho_g))
V = VectorFunctionSpace(mesh, 'Lagrange', degree=2)
du = TrialFunction(V)
u_ = TestFunction(V)
a = inner(sigma(du), eps(u_))*dx
l = inner(f, u_)*dx
Resolution
----------
Fixed displacements are imposed on the left part of the beam, the ``solve``
function is then called and solution is plotted by deforming the mesh::
def left(x, on_boundary):
return near(x[0],0.)
bc = DirichletBC(V, Constant((0.,0.)), left)
u = Function(V, name="Displacement")
solve(a == l, u, bc)
plot(1e3*u, mode="displacement")
The (amplified) solution should look like this:
.. image:: cantilever_deformed.png
:scale: 15%
Validation and post-processing
------------------------------
The maximal deflection is compared against the analytical solution from
Euler-Bernoulli beam theory which is here :math:`w_{beam} = \dfrac{qL^4}{8EI}`::
print("Maximal deflection:", -u(L,H/2.)[1])
print("Beam theory deflection:", float(3*rho_g*L**4/2/E/H**3))
One finds :math:`w_{FE} = 5.8172\text{e-3}` against :math:`w_{beam} = 5.8594\text{e-3}`
that is a 0.72% difference.
\ No newline at end of file
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