Users:General FEM Analysis/Elements Reference/Membrane1
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The theory and finite element formulation is described in detail in the work of Dieringer | The theory and finite element formulation is described in detail in the work of Dieringer |
Revision as of 08:01, 2 September 2010
Contents |
General Description
Element Type
- This membrane element is a plane stress element with 3 degrees of freedom per node
- The membrane element neglects the bending stiffness
- The ratio of the thickness and the lengths in the other two directions is much smaller than one ( t/Lx << 1 and t/Ly << 1).
- The thickness is constant over the element
Degrees of Freedom
For the membrane element use the 3 translatoric degrees of freedom. DISP_X, DISP_Y, DISP_Z
Input Parameters
Parameter Description
Compulsory Parameters | ||
Parameter | Values, Default(*) | Description |
---|---|---|
MAT | EL-MAT int | Number for the used Material
e.g. MAT=EL-MAT 1 \tabularnewline |
THICKNESS | int | Thickness of the membrane |
A_X, A_Y, A_Z
B_X, B_Y, B_Z |
Definition of the principle directions of the surface. To define the prestress dirctions. (see description below) | |
SIG11
SIG22 SIG12 |
Prestress state of the membrane. (see description below) | |
LAGRANGE | TOTAL, UPDATED | Definition of lagrange type. UPDATED for form finding and TOTAL for statics or dynamics. (e.g. LAGRANGE=UPDATED) |
Optional Parameters |
Example of a Complete Input Block
EL-PROP 1 : MEMBRANE1 MAT= EL-MAT 1 THICKNESS=1.0 PRESTRESS SIG11=1.0 SIG22=1.0 SIG12=0.0 A_X=1.0 A_Y=0.0 A_Z=0.0 B_X=0.0 B_Y=1.0 B_Z=0.0 LAGRANGE=UPDATED
Element Loading
Pressure
Dead Load
Snow Load
Theory
The theory and finite element formulation is described in detail in the work of Dieringer [1] and Linhard [2]
For the correct use of the membrane element and the interpretation of related results, the following aspects should be considered:
Material parameter
With the parameter MAT the material, that would be used in the calculation, for the membrane element is defined. A very popular mistake is that a material number would be used, that isn't defined already. Please ensure that the material that you would like to use at this point are already exits. The following materials are testet for the membrane element:
- linear elastic isotropic
- linear elastic orthotropic (Münsch-Reinhardt)
- multilinear elastic isotropic
- elastoplastic isotropic
- material on the basis of response functions
Thickness parameter
The parameter THICKNESS defines the thickness of the membrane. The thickness should be constant over the element.
Prestress directions on the surface
The parameters A_X, A_Y, A_Z and B_X, B_Y, B_Z are used to define the prestress directions on the surface. In this approach the principle directions of the prestress are defined in a plane area (see figure below). The definition of the area is given by the two vectors f1 and f2. The normal vector of the area can be calculated with the cross product of the in plane vectors f3=f1 x f2. Afterwards the line of intersection T1 of the area which is given by f1 and f3 and the curved surface can be calculated. In this approach T1 is interpreted as the first principle direction of the prestress on the curved surface. With the assumption that T3 is equal to the surface normal vector G3 (not uniformed), the second direction of the prestress is calculated as T2=T1 x T3. W.r.t. the parameters for the input file, only the plane area with the vectors f1 and f2 have to be defined. Referring to the depict approach the vector A defines the vector f1 and the vector B defines the vector f2.
Prestress state &sigma
SIG11, SIG22, SIG12 describes the prestress of the membrane element. The element is based on the plane stress assuption. Due to that only normal and shear stresses in the midplane have to be defined. SIGG11 is the stress acting in T1, SIG22 acting in T2 and SIG12 is the in plane shear, whereas SIG12=SIG21 (see figure below).
Lagrange type
With the LARANGE parameter it is possible to switch between form finding and statical/dynamical analysis. For the value UPDATED the element is for form finding and for the value TOTAL the element is for statical/dynamical analysis. It is important that the LANGRANGE parameter match to the type of analysis.
References
- ↑ Dieringer, F.: Implementierung eines geometrisch nichtlinearen Membranelements in einer objektorientierten Programmierumgebung, Masterthesis, Chair of structural analysis, Technische Universität München, 2009
- ↑ Linhard, J.: Numerisch-mechanische Betrachtung des Entwurfsprozesses von Membrantragwerken, PhD-Thesis, Chair of structural analysis, Technische Universität München, 2009
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