Difference between revisions of "Composite analysis"

From CAELinuxWiki
Jump to: navigation, search
m (Reverted edit of Atywehacyg, changed back to last version by Jose francisco)
 
(One intermediate revision by one other user not shown)
(No difference)

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