This section gives a short theoretical reminder of supported FEM problems. The selection of the formulation for each element group is done through the material and element properties.
6.1.1 3D elasticity
Elements with a p_solid property entry with a non-zero integration rule are described under p_solid. They correspond exactly to the *b elements, which are now obsolete. These elements support 3D mechanics (DOFs .01 to .03 at each node) with full anisotropy, geometric non-linearity, integration rule selection, ... The elements have standard limitations. In particular they do not (yet)
-
have any correction for shear locking found for high aspect ratios
- have any correction for dilatation locking found for nearly incompressible materials
With m_elastic subtypes 1 and 3, p_solid deals with 3D mechanics with strain defined by
where the engineering notation γyz=2єyz, ... is used. Stress by
Note that the strain states are {єx єy єz γyz γzx γxy} which may not be the convention of other software.
Note that NASTRAN, SAMCEF, ANSYS and MODULEF order shear stresses with σxy, σyz, σzx (MODULEF elements are obtained by setting p_solid integ value to zero). Abaqus uses σxy, σxz, σyz
In fe_stress the stress reordering can be accounted for by the definition of the proper TensorTopology matrix.
For isotropic materials
with at nominal G=E/(2(1+ν)). For isotropic materials, interpolation of ρ,η,E,ν,G,α with temperature is supported.
For orthotropic materials, the compliance is given by
For constitutive law building, see p_solid. Material orientation can be interpolated by defining v1 and v2 fields in the InfoAtNode. Interpolation of non isotropic material properties was only implemented for of_mk >= 1.236.
6.1.2 2D elasticity
With m_elastic subtype 4, p_solid deals with 2D mechanical volumes with strain defined by (see q4p constants)
and stress by
For isotropic plane stress (p_solid form=1), one has
For isotropic plane strain (p_solid form=0), one has
6.1.3 Acoustics
With m_elastic subtype 2, p_solid deals with 2D and 3D acoustics (see flui4 constants) where 3D strain is given by
This replaces the earlier flui4 ... elements.
The mass and stiffness matrices are given by
The source associated with a enforced velocity on a surface
When an impedance Z=ρ C R(1+iη) is considered on a surface,
the associated viscous damping matrix is given by
6.1.4 Classical lamination theory
Both isotropic and orthotropic materials are considered. In these cases, the general form of the 3D elastic material law is
Plate formulation consists in assuming one dimension, the thickness along x3, negligible compared with the surface dimensions. Thus, vertical stress σ33=0 on the bottom and upper faces, and assumed to be neglected throughout the thickness,
and for isotropic material,
By eliminating σ33, the plate constitutive law is written, with engineering notations,
The reduced stiffness coefficients Qij (i,j = 1,2,4,5,6) are related to the 3D stiffness coefficients Cij by
The reduced elastic law for an isotropic plate becomes,
and
Under Reissner-Mindlin's kinematic assumption the linearized strain tensor is
So, the strain vector is written,
with єm the membrane, κ the curvature or bending, and γ the shear strains,
Note that the engineering notation with γ12=u1,2+u2,1 is used here rather than the tensor notation with є12=(u1,2+u2,1)/2 . Similarly κ12=β1,2+β2,1, where a factor 1/2 would be needed for the tensor.
The plate formulation links the stress resultants, membrane forces Nαβ, bending moments Mαβ and shear forces Qα3, to the strains, membrane єm, bending κ and shearing γ,
The stress resultants are obtained by integrating the stresses through the thickness of the plate,
with α, β = 1, 2.
Therefore, the matrix extensional stiffness matrix [A], extension/bending coupling matrix [B], and the bending stiffness matrix [D] are calculated by integration over the thickness interval [hb ht]
An improvement of Mindlin's plate theory with tranverse shear consists in modifying the shear coefficients Fij by
where kij are correction factors. Reddy's 3rd order theory brings to kij=2/3. Very commonly, enriched 3rd order theory are used, and kij are equal to 5/6 and give good results. For more details on the assessment of the correction factor, see [41].
For an isotropic symmetric plate (hb=−ht=h/2), the in-plane normal forces N11, N22 and shear force N12 become
the 2 bending moments M11, M22 and twisting moment M12
and the out-of-plane shearing forces Q23 and Q13,
One can notice that because the symmetry of plate, that means the reference plane is the mid-plane of the plate (x3(0)=0) the extension/bending coupling matrix [B] is equal to zero.
Using expression (6.26) for a constant Qij, one sees that for a non-zero offset, one has
where is clearly appears that the constitutive matrix is a polynomial function of h, h3, x3(0)2h and x3(0)h. If the ply thickness is kept constant, the constitutive law is a polynomial function of 1,x3(0),x3(0)2.
6.1.5 Piezo-electric volumes
A revised version of this information is available at http://www.sdtools.com/pdf/piezo.pdf. Missing PDF links will be found there.
The strain state associated with piezoelectric materials is described by the six classical mechanical strain components and the electrical field components. Following the IEEE standards on piezoelectricity and using matrix notations, S denotes the strain vector and E denotes the electric field vector (V/m) :
where φ is the electric potential (V).
The constitutive law associated with this strain state is given by
in which D is the electrical displacement vector (a density of charge in Cb/m2), T is the mechanical stress vector (N/m2). CE is the matrix of elastic constants at zero electric field (E=0, short-circuited condition, see section 6.1.1 for formulas (there CE is noted D). Note that using −E rather than E makes the constitutive law symmetric.
Alternatively, one can use the constitutive equations written in the following manner :
In which sE is the matrix of mechanical compliances, [d]
is the matrix of piezoelectric constants (m/V=Cb/N):
Matrices [e] and [d] are related through
Due to crystal symmetries, [d] may have only a few non-zero elements.
Matrix [єS] is the matrix of dielectric constants
(permittivities) under zero strain (constant volume) given by
It is more usual to find the value of єT
(Permittivity at zero stress) in the datasheet. These two values
are related through the following relationship :
For this reason, the input value for the computation should be
[єT].
Also notice that usually relative permittivities are given in datasheets:
є0 is the permittivity of vacuum (=8.854e-12 F/m)
The most widely used piezoelectric materials are PVDF and PZT. For
both of these, matrix [єT] takes the form
For PVDF, the matrix of piezoelectric constants is given by
and for PZT materials :
6.1.6 Piezo-electric shells
A revised version of this information is available at http://www.sdtools.com/pdf/piezo.pdf.
Shell strain is defined by the membrane, curvature and transverse shear as well as the electric field components. It is assumed that
in each piezoelectric layer i=1...n, the electric field takes
the form E→= (0 0 Ezi). Ezi is assumed
to be constant over the thickness hi of the layer and is
therefore given by Ezi=−Δ φi/hi where
Δ φi is the difference of potential between the
electrodes at the top and bottom of the piezoelectric layer i.
It is also assumed that the piezoelectric principal axes are
parallel to the structural orthotropy axes.
The strain state of a piezoelectric shell takes the form
There are thus n additional degrees of freedom Δ φi,
n being the number of piezoelectric layers in the laminate shell
The constitutive law associated to this strain state is given by :
where Dzi is the electric displacement in piezoelectric layer
(assumed constant and in the z-direction), zmi is the
distance between the midplane of the shell and the midplane of
piezoelectric layer i, and Gi, Hi are given by
where . denotes the direction of polarization. If the piezoelectric is
used in extension mode, the polarization is in the z-direction,
therefore Hi =0 and Gi ={
}i . If the piezoelectric is used in shear mode, the
polarization is in the x or y-direction, therefore Gi=0,
and Hi = {0 e15 }i or Hi = {e24 0 }i . It turns out however that the hypothesis of a uniform transverse shear strain distribution through the thickness is not satisfactory, a more elaborate shell element would be necessary. Shear actuation should therefore be used with caution.
[Rs]i and [R]i are rotation matrices associated to the
angle θ of the piezoelectric layer.
6.1.7 Geometric non-linearity
The following gives the theory of large transformation problem implemented in OpenFEM function of_mk_pre.c Mecha3DInteg.
The principle of virtual work in non-linear total Lagrangian formulation for an hyperelastic medium is
with p the vector of initial position, x = p +u the current
position, and u the displacement vector. The transformation is characterized by
where the N,j is the derivative of the shape functions with respect to Cartesian coordinates at the current integration point and qi corresponds to field i (here translations) and element nodes. The notation is thus really valid within a single element and corresponds to the actual implementation of the element family in elem0 and of_mk. Note that in these functions, a reindexing vector is used to go from engineering ({e11 e22 e33 2e23 2e31 2e12}) to tensor [eij] notations ind_ts_eg=[1 6 5;6 2 4;5 4 3];e_tensor=e_engineering(ind_ts_eg);. One can also simplify a number of computations using the fact that the contraction of a symmetric and non symmetric tensor is equal to the contraction of the symmetric tensor by the symmetric part of the non symmetric tensor.
One defines the Green-Lagrange strain tensor e=1/2(FTF −I) and its variation
Thus the virtual work of internal loads (which corresponds to the residual in non-linear iterations) is given by
and the tangent stiffness matrix (its derivative with respect to the current position) can be written as
which using the notation ui,j = {N,j}T{qi} leads to
The term associated with stress at the current point is generally called geometric stiffness or pre-stress contribution.
For implementation, the variable names are d2wde2, Sigma and the large displacement computation (Fmk
∂2 W/∂ e2ijkl Fni + Slj) has a reference implementation in elem0('LdDD'). The result is called dd in the code.
In isotropic elasticity, the 2nd tensor of Piola-Kirchhoff stress is given by
the building of the constitutive law matrix D is performed in p_solid BuildConstit for isotropic, orthotropic and full anisotropic materials. of_mk_pre.c nonlin_elas then implements element level computations. For hyperelastic materials ∂2 W/∂ e2 is not constant and is computed at each integration point as implemented in hyper.c.
For a geometric non-linear static computation, a Newton solver will thus iterate with
where external forces f are assumed to be non following.
For an example see staticNewton.
6.1.8 Thermal pre-stress
Note that more recent developments are found in SDT-nlsim, see sdtweb('hyper3D'). The following gives the theory of the thermoelastic problem implemented in OpenFEM function of_mk_pre.c nonlin_elas.
In presence of a temperature difference, the thermal strain is given by [eT] = [α] (T−T0), where in general the thermal expansion matrix α is proportional to identity (isotropic expansion). The stress is found by computing the contribution of the mechanical deformation
This expression of the stress is then used in the equilibrium (6.49), the tangent matrix computation(6.53), or the Newton iteration (6.56). Note that the fixed contribution ∫Ω0 (−C:eT) : δ e can be considered as an internal load of thermal origin.
The modes of the heated structure can be computed with the tangent matrix.
An example of static thermal computation is given in ofdemos ThermalCube.
6.1.9 Hyperelasticity
The following gives the theory of the thermoelastic problem implemented in OpenFEM function hyper.c (called by of_mk.c MatrixIntegration).
For hyperelastic media S=∂ W/∂ e with W the hyperelastic energy. hyper.c currently supports Mooney-Rivlin materials for which the energy takes one of following forms
where (J1,J2,J3) are the so-called reduced invariants of the Cauchy-Green tensor
linked to the classical invariants (I1,I2,I3) by
where one recalls that
Note : this definition of energy based on reduced invariants is used to have the hydrostatic pressure given directly by p=−K(J3−1) (K "bulk modulus"), and the third term of W is a penalty on incompressibility.
Hence, computing the corresponding tangent stiffness and residual operators will require the derivatives of the above invariants with respect to e (or C). In an orthonormal basis the first-order derivatives are given by:
where (Cij−1) denotes the coefficients of the inverse matrix of (Cij). For second-order derivatives we have:
where the єijk coefficients are defined by
Note: when the strain components are seen as a column vector ("engineering strains") in the form (e11,e22,e33,2e23,2e31,2e12)′, the last two terms of (6.64) thus correspond to the following 2 matrices
We finally use chain-rule differentiation to compute
Note that a factor 2 arise each time we differentiate the invariants with respect to e instead of C.
The specification of a material is given by specification of the derivatives of the energy with respect to invariants. The laws are implemented in the hyper.c EnPassiv function.
6.1.10 Gyroscopic effects
Written by Arnaud Sternchuss ECP/MSSMat.
In the fixed reference frame which is Galilean, the Eulerian speed of the particle in x whose initial position is p is
and its acceleration is
Ω is the rotation vector of the structure with
in a (x,y,z) orthonormal frame.
The skew-symmetric matrix [Ω] is defined such that
The speed can be rewritten
and the acceleration becomes
In this expression appear
-
the acceleration in the rotating frame
,
- the centrifugal acceleration
,
- the Coriolis acceleration
.
S0e is an element of the mesh of the initial configuration S0 whose density is ρ0. [N] is the matrix of shape functions on these elements, one defines the following elementary matrices
The traditional fe_mknl MatType in SDT are 7 for gyroscopic
coupling and 8 for centrifugal softening.
6.1.11 Centrifugal follower forces
This is the embryo of the theory for the future implementation of centrifugal follower forces.
where δ vR designates the radial component (in deformed configuration) of δv. One assumes that the rotation axis is along ez. Noting nR = 1/R {x1 x2 0}T, one then has
Thus the non-linear stiffness term is given by
One has dR=nR· dx(= dxR) and dδ vR = dnR·δ v, with
Thus, finally
Which gives
with α=1,2.
6.1.12 Poroelastic materials
The poroelastic formulation comes from [42], recalled and detailed in [43].
Domain and variables description:
 | Poroelastic domain |
 | Bounding surface of poroelastic domain |
 | Unit external normal of  |
 | Solid phase displacement vector |
 | Fluid phase displacement vector |  |
 | Fluid phase pressure |
 | Stress tensor of solid phase |
 | Total stress tensor of porous material |  |
Weak formulation, for harmonic time dependence at pulsation ω:
Matrix formulation, for harmonic time dependence at pulsation ω:
where the frequency-dependent matrices correspond to:
N.B. if the material of the solid phase is homogeneous, the frequency-dependent parameters can be eventually factorized from the matrices:
where the matrices marked with bars are frequency independent:
Material parameters:
| φ | Porosity of the porous material |
| σ | Resistivity of the porous material |
| α∞ | Tortuosity of the porous material |
| Λ | Viscous characteristic length of the porous material |
| Λ′ | Thermal characteristic length of the skeleton |
| ρ | Density of the skeleton |
| G | Shear modulus of the skeleton |
| ν | Poisson coefficient of the skeleton |
| ηs | Structural loss factor of the skeleton |
| ρo | Fluid density |
| γ | Heat capacity ratio of fluid (=1.4 for air) |
| η | Shear viscosity of fluid (=1.84×10−5 kg m−1 s−1 for air) |
Constants:
| Po=1,01× 105 Pa | Ambient pressure |
| Pr=0.71 | Prandtl number |
Poroelastic specific (frequency dependent) variables:
 | Apparent density of solid phase |  |
 | Apparent density of fluid phase |  |
 | Interaction apparent density |  |
 | Effective density of solid phase |  |
 | Effective density of solid phase |  |
 | Effective density of fluid phase |  |
 | Interaction effective density |  |
 | Viscous damping coefficient |  |
 | Coupling coefficient |  |
 | Elastic coupling coefficient |
| | Biot formulation |  |
| | Approximation from  |  |
 | Bulk modulus of air in fraction volume |
| | Biot formulation |  |
| | Approximation from  |  |
 | Bulk modulus of porous material in vacuo |  |
 | Bulk modulus of elastic solid |
| | est. from Hashin-Shtrikman's upper bound |  |
 | Effective bulk modulus of air in pores |  |
 | Function in  (Champoux-Allard model) |  |
 | Thermal characteristic frequency | 
|
To add here:
-
coupling conditions with poroelastic medium, elastic medium, acoustic medium
- dissipated power in medium
6.1.13 Heat equation
This section is based on an OpenFEM contribution by Bourquin Frédéric and Nassiopoulos Alexandre from Laboratoire Central des Ponts et Chaussées.
The variational form of the Heat equation is given by
with
-
ρ the density, c the specific heat capacity.
- K the conductivity tensor of the material. The tensor K is symmetric, positive definite, and is often taken as diagonal. If conduction is isotropic, one can write K=k(x)Id where k(x) is called the (scalar) conductivity of the material.
- Acceptable loads and boundary conditions are
Test case
One considers a solid square prism of dimensions Lx,Ly, Lz in the three directions (Ox), (Oy) and (Oz) respectively. The solid is made of homogeneous isotropic material, and its conductivity tensor thus reduces to a constant k.
The faces, 
, are subject to the following boundary conditions and loads
-
f=40 is a constant uniform internal heat source
- Γ1 (x=0) : exchange & heat flux (Fourier-Robin) given by α=1,g1=α θext + α f Lx2/2k=25
- Γ2 (x=Lx) : prescribed temperature : θ(Lx,y,z)=θext=20
- Γ3 (y=0), Γ4 (y=Ly), Γ5 (z=0), Γ6 (z=Lz): exchange & heat flux g+α θext =αθext +α f/2 k (Lx2−x2)+g1=25−x2/20
The problem can be solved by the method of separation of variables. It admits
the solution
| θ(x,y,z) =− | | x2 + θext + | | = | | = 25 − | |
The resolution for this example can be found in demo/heat_equation.
| Figure 6.1: Temperature distribution along the x-axis |
©1991-2024 by SDTools
