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Francisco Ramírez
comet-fenics
Commits
b7bef5d1
Commit
b7bef5d1
authored
Jul 05, 2018
by
Jeremy BLEYER
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Added beam buckling example
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examples/modal_analysis_dynamics/cantilever_modal.py.rst
examples/modal_analysis_dynamics/cantilever_modal.py.rst
+23
-23
examples/timoshenko/.ipynb_checkpoints/beam_buckling-checkpoint.ipynb
...oshenko/.ipynb_checkpoints/beam_buckling-checkpoint.ipynb
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-0
examples/timoshenko/beam_buckling.ipynb
examples/timoshenko/beam_buckling.ipynb
+1037
-0
examples/viscoelasticity/.ipynb_checkpoints/linear_viscoelasticity-checkpoint.ipynb
...ipynb_checkpoints/linear_viscoelasticity-checkpoint.ipynb
+11393
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examples/viscoelasticity/linear_viscoelasticity.ipynb
examples/viscoelasticity/linear_viscoelasticity.ipynb
+11393
-0
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examples/modal_analysis_dynamics/cantilever_modal.py.rst
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b7bef5d1
...
@@ -10,8 +10,8 @@ Introduction
...
@@ -10,8 +10,8 @@ Introduction
-------------
-------------
This program performs a dynamic modal analysis of an elastic cantilever beam
This program performs a dynamic modal analysis of an elastic cantilever beam
represented by a 3D solid continuum. The eigenmodes are computed using the
represented by a 3D solid continuum. The eigenmodes are computed using the
**SLEPcEigensolver** and compared against an analytical solution of beam theory.
**SLEPcEigensolver** and compared against an analytical solution of beam theory.
The corresponding file can be obtained from :download:`cantilever_modal.py`.
The corresponding file can be obtained from :download:`cantilever_modal.py`.
...
@@ -20,14 +20,14 @@ The first four eigenmodes of this demo will look as follows:
...
@@ -20,14 +20,14 @@ The first four eigenmodes of this demo will look as follows:
.. image:: vibration_modes.gif
.. image:: vibration_modes.gif
:scale: 80 %
:scale: 80 %
The first two fundamental modes are on top with bending along the weak axis (left) and along
The first two fundamental modes are on top with bending along the weak axis (left) and along
the strong axis (right), the next two modes are at the bottom.
the strong axis (right), the next two modes are at the bottom.
---------------
---------------
Implementation
Implementation
---------------
---------------
After importing the relevant modules, the geometry of a beam of length :math:`L=20`
After importing the relevant modules, the geometry of a beam of length :math:`L=20`
and rectangular section of size :math:`B\times H` with :math:`B=0.5, H=1` is first defined::
and rectangular section of size :math:`B\times H` with :math:`B=0.5, H=1` is first defined::
from fenics import *
from fenics import *
...
@@ -43,7 +43,7 @@ and rectangular section of size :math:`B\times H` with :math:`B=0.5, H=1` is fir
...
@@ -43,7 +43,7 @@ and rectangular section of size :math:`B\times H` with :math:`B=0.5, H=1` is fir
Material parameters and elastic constitutive relations are classical (here we
Material parameters and elastic constitutive relations are classical (here we
take :math:`\nu=0`) and we also introduce the material density :math:`\rho` for
take :math:`\nu=0`) and we also introduce the material density :math:`\rho` for
later definition of the mass matrix::
later definition of the mass matrix::
E, nu = 1e5, 0.
E, nu = 1e5, 0.
...
@@ -59,7 +59,7 @@ later definition of the mass matrix::
...
@@ -59,7 +59,7 @@ later definition of the mass matrix::
dim = v.geometric_dimension()
dim = v.geometric_dimension()
return 2.0*mu*eps(v) + lmbda*tr(eps(v))*Identity(dim)
return 2.0*mu*eps(v) + lmbda*tr(eps(v))*Identity(dim)
Standard FunctionSpace is defined and boundary conditions correspond to a
Standard FunctionSpace is defined and boundary conditions correspond to a
fully clamped support at :math:`x=0`::
fully clamped support at :math:`x=0`::
V = VectorFunctionSpace(mesh, 'Lagrange', degree=1)
V = VectorFunctionSpace(mesh, 'Lagrange', degree=1)
...
@@ -73,7 +73,7 @@ fully clamped support at :math:`x=0`::
...
@@ -73,7 +73,7 @@ fully clamped support at :math:`x=0`::
bc = DirichletBC(V, Constant((0.,0.,0.)), left)
bc = DirichletBC(V, Constant((0.,0.,0.)), left)
The system stiffness matrix :math:`[K]` and mass matrix :math:`[M]` are
The system stiffness matrix :math:`[K]` and mass matrix :math:`[M]` are
respectively obtained from assembling the corresponding variational forms::
respectively obtained from assembling the corresponding variational forms::
k_form = inner(sigma(du),eps(u_))*dx
k_form = inner(sigma(du),eps(u_))*dx
...
@@ -86,14 +86,14 @@ respectively obtained from assembling the corresponding variational forms::
...
@@ -86,14 +86,14 @@ respectively obtained from assembling the corresponding variational forms::
M = PETScMatrix()
M = PETScMatrix()
assemble(m_form, tensor=M)
assemble(m_form, tensor=M)
Matrices :math:`[K]` and :math:`[M]` are first defined as PETSc Matrix and
Matrices :math:`[K]` and :math:`[M]` are first defined as PETSc Matrix and
forms are assembled into it to ensure that they have the right type.
forms are assembled into it to ensure that they have the right type.
Note that boundary conditions have been applied to the stiffness matrix using
Note that boundary conditions have been applied to the stiffness matrix using
``assemble_system`` so as to preserve symmetry (a dummy ``l_form`` and right-hand side
``assemble_system`` so as to preserve symmetry (a dummy ``l_form`` and right-hand side
vector have been introduced to call this function).
vector have been introduced to call this function).
Modal dynamic analysis consists in solving the following generalized
Modal dynamic analysis consists in solving the following generalized
eigenvalue problem :math:`[K]\{U\}=\lambda[M]\{U\}` where the eigenvalue
eigenvalue problem :math:`[K]\{U\}=\lambda[M]\{U\}` where the eigenvalue
is related to the eigenfrequency :math:`\lambda=\omega^2`. This problem
is related to the eigenfrequency :math:`\lambda=\omega^2`. This problem
can be solved using the ``SLEPcEigenSolver``. ::
can be solved using the ``SLEPcEigenSolver``. ::
...
@@ -121,7 +121,7 @@ We now ask SLEPc to extract the first 6 eigenvalues by calling its solve functio
...
@@ -121,7 +121,7 @@ We now ask SLEPc to extract the first 6 eigenvalues by calling its solve functio
and extract the corresponding eigenpair (first two arguments of ``get_eigenpair``
and extract the corresponding eigenpair (first two arguments of ``get_eigenpair``
correspond to the real and complex part of the eigenvalue, the last two to the
correspond to the real and complex part of the eigenvalue, the last two to the
real and complex part of the eigenvector)::
real and complex part of the eigenvector)::
N_eig = 6 # number of eigenvalues
N_eig = 6 # number of eigenvalues
print "Computing %i first eigenvalues..." % N_eig
print "Computing %i first eigenvalues..." % N_eig
eigensolver.solve(N_eig)
eigensolver.solve(N_eig)
...
@@ -136,31 +136,31 @@ real and complex part of the eigenvector)::
...
@@ -136,31 +136,31 @@ real and complex part of the eigenvector)::
file_results = XDMFFile("modal_analysis.xdmf")
file_results = XDMFFile("modal_analysis.xdmf")
file_results.parameters["flush_output"] = True
file_results.parameters["flush_output"] = True
file_results.parameters["functions_share_mesh"] = True
file_results.parameters["functions_share_mesh"] = True
# Extraction
# Extraction
for i in range(N_eig):
for i in range(N_eig):
# Extract eigenpair
# Extract eigenpair
r, c, rx, cx = eigensolver.get_eigenpair(i)
r, c, rx, cx = eigensolver.get_eigenpair(i)
# 3D eigenfrequency
# 3D eigenfrequency
freq_3D = sqrt(r)/2/pi
freq_3D = sqrt(r)/2/pi
# Beam eigenfrequency
# Beam eigenfrequency
if i % 2 == 0: # exact solution should correspond to weak axis bending
if i % 2 == 0: # exact solution should correspond to weak axis bending
I_bend = H*B**3/12.
I_bend = H*B**3/12.
else: #exact solution should correspond to strong axis bending
else: #exact solution should correspond to strong axis bending
I_bend = B*H**3/12.
I_bend = B*H**3/12.
freq_beam = alpha(i/2)**2*sqrt(E*I_bend/(rho*B*H*L**4))/2/pi
freq_beam = alpha(i/2)**2*sqrt(E*I_bend/(rho*B*H*L**4))/2/pi
print("Solid FE: {0:8.5f} [Hz] Beam theory: {1:8.5f} [Hz]".format(freq_3D, freq_beam))
print("Solid FE: {0:8.5f} [Hz] Beam theory: {1:8.5f} [Hz]".format(freq_3D, freq_beam))
# Initialize function and assign eigenvector (renormalize by stiffness matrix)
# Initialize function and assign eigenvector (renormalize by stiffness matrix)
eigenmode = Function(V,name="Eigenvector "+str(i))
eigenmode = Function(V,name="Eigenvector "+str(i))
eigenmode.vector()[:] = rx
/omega
eigenmode.vector()[:] = rx
The beam analytical solution is obtained using the eigenfrequencies of a clamped
The beam analytical solution is obtained using the eigenfrequencies of a clamped
beam in bending given by :math:`\omega_n = \alpha_n^2\sqrt{\dfrac{EI}{\rho S L^4}}`
beam in bending given by :math:`\omega_n = \alpha_n^2\sqrt{\dfrac{EI}{\rho S L^4}}`
where :math:`S=BH` is the beam section, :math:`I` the bending inertia and
where :math:`S=BH` is the beam section, :math:`I` the bending inertia and
:math:`\alpha_n` is the solution of the following nonlinear equation:
:math:`\alpha_n` is the solution of the following nonlinear equation:
.. math::
.. math::
...
@@ -173,9 +173,9 @@ and the other along the strong axis (:math:`I=I_{\text{strong}} = BH^3/12`). Sin
...
@@ -173,9 +173,9 @@ and the other along the strong axis (:math:`I=I_{\text{strong}} = BH^3/12`). Sin
for the considered numerical values, the strong axis bending frequency will be twice that corresponsing
for the considered numerical values, the strong axis bending frequency will be twice that corresponsing
to bending along the weak axis. The solution :math:`\alpha_n` are computed using the
to bending along the weak axis. The solution :math:`\alpha_n` are computed using the
``scipy.optimize.root`` function with initial guess given by :math:`(2n+1)\pi/2`.
``scipy.optimize.root`` function with initial guess given by :math:`(2n+1)\pi/2`.
With ``Nx=400``, we obtain the following comparison between the FE eigenfrequencies
With ``Nx=400``, we obtain the following comparison between the FE eigenfrequencies
and the beam theory eigenfrequencies :
and the beam theory eigenfrequencies :
===== ============= =================
===== ============= =================
...
@@ -184,11 +184,11 @@ Mode Eigenfrequencies
...
@@ -184,11 +184,11 @@ Mode Eigenfrequencies
# Solid FE [Hz] Beam theory [Hz]
# Solid FE [Hz] Beam theory [Hz]
===== ============= =================
===== ============= =================
1 2.04991 2.01925
1 2.04991 2.01925
2 4.04854 4.03850
2 4.04854 4.03850
3 12.81504 12.65443
3 12.81504 12.65443
4 25.12717 25.30886
4 25.12717 25.30886
5 35.74168 35.43277
5 35.74168 35.43277
6 66.94816 70.86554
6 66.94816 70.86554
===== ============= =================
===== ============= =================
examples/timoshenko/.ipynb_checkpoints/beam_buckling-checkpoint.ipynb
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examples/timoshenko/beam_buckling.ipynb
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examples/viscoelasticity/.ipynb_checkpoints/linear_viscoelasticity-checkpoint.ipynb
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examples/viscoelasticity/linear_viscoelasticity.ipynb
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