Difference between revisions of "Composite analysis"

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This page will be a place to share information involving composite analysis.
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This page will be a place to share information involving composite analysis with ''code_aster''. Any help and experience will be wellcame. Please, write comments, ideas, tips, ... in the discussion page. josefrancisco.lopezmarin@gmail.com
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==Specimen==
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[[Image:example2.png]]
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==Orthotropic materials==
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Fiber glass:
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* <tex>E_{11}=35 GPa</tex>, <tex>E_{22}=10 GPa=E_{33}=10 GPa</tex>
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* <tex>G_{12}=G_{23}=G_{13}=3.5 GPa</tex>
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* <tex>\nu_{12}=0.35</tex>, <tex>\nu_{23}=\nu_{13}=0.05</tex>
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Foam:
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==Creating the mesh==
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===GMSH===
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cs=60;
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Point(1)={0,0,0,cs};
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Point(2)={1000/3,0,100,cs};
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Point(3)={2000/3,0,100,cs};
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Point(4)={1000,0,0,cs};
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Spline(1)={1:4};
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Extrude {0, 2000, 0} {
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Line{1}; Layers{20}; Recombine;
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}
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[[Image:specimen2.png]]
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===Salome===
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==Boundary conditions==
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==Loads==
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==Failure criteria==

Latest revision as of 12:52, 18 November 2010

This page will be a place to share information involving composite analysis with code_aster. Any help and experience will be wellcame. Please, write comments, ideas, tips, ... in the discussion page. josefrancisco.lopezmarin@gmail.com


Specimen

Example2.png

Orthotropic materials

Fiber glass:

  • E_{11}=35 GPa, E_{22}=10 GPa=E_{33}=10 GPa
  • G_{12}=G_{23}=G_{13}=3.5 GPa
  • \nu_{12}=0.35, \nu_{23}=\nu_{13}=0.05

Foam:

Creating the mesh

GMSH

cs=60;
Point(1)={0,0,0,cs};
Point(2)={1000/3,0,100,cs};
Point(3)={2000/3,0,100,cs};
Point(4)={1000,0,0,cs};
Spline(1)={1:4};
Extrude {0, 2000, 0} {
Line{1}; Layers{20}; Recombine;
}


Specimen2.png


Salome

Boundary conditions

Loads

Failure criteria