Users:Structural Optimization/Design Variables/Nodal Thickness

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=== Short Info ===
 
=== Short Info ===
Platzhaltertext (diese gesamtseite ist noch zu schreiben, nur das format ist bereitgestellt).
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With this design variable, the nodal thickness can be optimized. This is especially usefull in combination with SHELL elements, which are able to take variable thicknesses into account.   
 
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Die verschiedenen Version erklären, evtl. in Tabelle: DIR, NDIR, Node Plane, NodeVec
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Gehört NodeSpaceBound auch in diese Gruppe? Dann evtl. auch das source-File in den entsprechenden Unterordner schieben.
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evtl ein bild zur erklärung [[File:Element_hexa_topo.png|400px|border|up|irgendein erklärungstext]]
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referenzen wie diese:
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<ref name="AnRa93"
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> U. Andelfinger, E. Ramm: „EAS-Elements for two-dimensional, three-dimensional, plate and shell structures and their equivalence to HR-Elements“, in „International Journal for Numerical Methods in Engineeering“, Vol. 36, 1993, pages 1311-1337
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</ref>.   
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The thickness at each node can be initialized by  . Alternatively, the initial thickness is computed as the mean thickness of the surrounding elements.
  
 
=== Parameters in the Input File ===
 
=== Parameters in the Input File ===

Revision as of 13:50, 19 October 2010


Contents

General Description

Short Info

With this design variable, the nodal thickness can be optimized. This is especially usefull in combination with SHELL elements, which are able to take variable thicknesses into account.

The thickness at each node can be initialized by . Alternatively, the initial thickness is computed as the mean thickness of the surrounding elements.

Parameters in the Input File

Compulsory Parameters
Parameter Values, Default(*) Description
MATERIAL EL-MAT int Linking to a material input block
INT_TYPE_HEXA FULL, REDUCED Control of integration type

20-noded elements are able to perform a uniform reduced integration (2x2x2 instead of 3x3x3) without hourglassing stabilisation

Optional Parameters
Parameter Values, Default(*) Description
EAS int Flag Enhances Assumed Strains (EAS) method

Possible values are:

  • 0* = EAS off
  • 9 = full and locking free linear strains can be described (recommended for one axial bending)
  • 15 = ellimination of parasitic bi-linear strains
  • 24 = full and locking free bi-linear strains can be described (recommended for two axial bending)
  • 30 = full tri-linear strains can be described


Example of a Complete Input Block

bla bla blub bla bla

EL-PROP 1: SOLIDHEXA1
MAT           = EL-MAT 1
INT_TYPE_HEXA = FULL
EAS           = 0


A complete test example

Model description

blabla mit bildern


Input File

bla


Documented Results

bla


Theory and Details

bla


References





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