|
|
Line 1: |
Line 1: |
| [[Category: Users:Structural Optimization]] | | [[Category: Users:Structural Optimization]] |
| | | |
− | | + | info will be added soon |
− | == General Description ==
| + | |
− | | + | |
− | === Short Info ===
| + | |
− | Platzhaltertext (diese gesamtseite ist noch zu schreiben, nur das format ist bereitgestellt).
| + | |
− | | + | |
− | Die verschiedenen Version erklären, evtl. in Tabelle: DIR, NDIR, Node Plane, NodeVec
| + | |
− | | + | |
− | Gehört NodeSpaceBound auch in diese Gruppe? Dann evtl. auch das source-File in den entsprechenden Unterordner schieben.
| + | |
− | | + | |
− | evtl ein bild zur erklärung [[File:Element_hexa_topo.png|400px|border|up|irgendein erklärungstext]]
| + | |
− | | + | |
− | referenzen wie diese:
| + | |
− | <ref name="AnRa93"
| + | |
− | > 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
| + | |
− | </ref>.
| + | |
− | | + | |
− | | + | |
− | === Parameters in the Input File ===
| + | |
− | | + | |
− | {| border="1" cellpadding="3" cellspacing="0"
| + | |
− | |colspan="3" style="background:#efefef;"| 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 <br>
| + | |
− | 20-noded elements are able to perform a uniform reduced integration (2x2x2 instead of 3x3x3) without hourglassing stabilisation
| + | |
− | |-
| + | |
− | |colspan="3" style="background:#efefef;"| Optional Parameters
| + | |
− | |-
| + | |
− | !Parameter
| + | |
− | !Values, Default(*)
| + | |
− | !Description
| + | |
− | |-
| + | |
− | !EAS
| + | |
− | |''int''
| + | |
− | |Flag Enhances Assumed Strains (EAS) method <br>
| + | |
− | 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
| + | |
− | | + | |
− | <pre>
| + | |
− | EL-PROP 1: SOLIDHEXA1
| + | |
− | MAT = EL-MAT 1
| + | |
− | INT_TYPE_HEXA = FULL
| + | |
− | EAS = 0
| + | |
− | </pre>
| + | |
− | | + | |
− | | + | |
− | | + | |
− | == A complete test example ==
| + | |
− | | + | |
− | | + | |
− | === Model description ===
| + | |
− | blabla mit bildern
| + | |
− | <gallery caption="" widths="350px" heights="350px" perrow="2">
| + | |
− | File:Cantilever_locking.JPG | HEXA8
| + | |
− | File:Cantilever_lockingfree.JPG | HEXA8EAS9
| + | |
− | </gallery>
| + | |
− | | + | |
− | | + | |
− | === Input File ===
| + | |
− | | + | |
− | bla
| + | |
− | | + | |
− | | + | |
− | === Documented Results ===
| + | |
− | | + | |
− | bla
| + | |
− | | + | |
− | | + | |
− | == Theory and Details ==
| + | |
− | | + | |
− | bla
| + | |
− | | + | |
− | | + | |
− | == References ==
| + | |
− | | + | |
− | <references/>
| + | |