Difference between revisions of "Contrib:KeesWouters/shell/static"
(→'''Definition of the geometry''') |
(→'''Definition of the geometry''') |
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* Presure3 (Ftop) = 24.3e3 Pa <br> | * Presure3 (Ftop) = 24.3e3 Pa <br> | ||
* Presure4 (Fcentre1,Fcentre2)= 182.6e3 Pa <br> | * Presure4 (Fcentre1,Fcentre2)= 182.6e3 Pa <br> | ||
− | ''' | + | '''Boundary conditions:''' <br> |
* Lbot (DX=0.0, DY=0.0, DZ=0.0) <br> | * Lbot (DX=0.0, DY=0.0, DZ=0.0) <br> | ||
* Ltop (DZ=0.0) <br> | * Ltop (DZ=0.0) <br> |
Revision as of 12:58, 7 March 2010
Contents
[hide]Static analysis of a shell construction
[ .... under construction .... ]
This contribution is in close cooperation with Bridge.
In this example the following items are discussed:
- preproccesing:
- definition of geometry in Salome
- partitioning of the geometry and groups
- meshing of the geometry
- definition of the groups
- (maybe: python script which makes editing much easier ...)
- static analysis with pressure or force applied on a group or nodes
- postprocessing:
- viewing displacement in Salome
- determination of stresses
- interface ASTK
Definition of the geometry
planar shell
Geometry:
- L = 11.38 m
- Thickness = 0.55 m
Loads:
[type] [group] [value]
- Presure1 (Fbot) = 29.5e3 Pa
- Presure2 (Fmain)= 25.8e3 Pa
- Presure3 (Ftop) = 24.3e3 Pa
- Presure4 (Fcentre1,Fcentre2)= 182.6e3 Pa
Boundary conditions:
- Lbot (DX=0.0, DY=0.0, DZ=0.0)
- Ltop (DZ=0.0)
Material:
Concrete
- E = 32e9 Pa
- Nu = 0.2
Create all points and lines using: [New Entity]->[Basic}->[Point] and [New Entity]->[Basic]->[Line]
Create one big face Ftotal [New Entity]->[Build]->[Face]
Ftotal: Line7,Line6,Line8,Line12,Line11,Line10,Line9,Line1
Create three wires [New Entity]->[Build]->[Wire]
- Wire1: Line3,Line4,Line5
- Wire2: Line17,Line18,Line19
- Wire3: Line13,Line14,Line15,Line16
Create vector [New Entity]->[Basic]->[Vector]
(0,0,1)
Create four extrusions [New Entity]->[Generation]->[Extrusion]
- Extrusion1: Wire1,vz
- Extrusion2: Wire2,vz
- Extrusion3: Wire3,vz
- Extrusion4: Line2,vz
Partitioning of the geometry
why: we need groups for loads and boundary conditions
how: we define planes
Create partition [Operations]->[Partition]
- Part_main: Ftotal,Extrusion1,Extrusion2,Extrusion3,Extrusion4
Meshing
how
tria -quad?
linear vs quadratic elements