A methodology that uses multi-axial testing and dissipated energy (DE) to characterise the mechanical behaviour of laminated composite materials has been implemented into an analysis approach. The goal of this approach is to quantify the damage development on a continuum basis and eventually relate this damage to the constitutive behaviour of the material. The approach was implemented into a commercial finite element package with a custom user subroutine. Doublenotch characterisation specimens and open hole tension coupons were assessed. DE was predicted well in tension and in-plane rotation cases apart from a pure shear case where DE was excessive. DE magnitude was satisfactory in the open hole case and damage propagation well represented. Future work will involve advancing the technique to include DEdependent constitutive modelling.
History
Start page
1
End page
10
Total pages
10
Outlet
ICAS 2010 CD-ROM Proceedings
Editors
Ian Grant
Name of conference
27th Congress of International Council of the Aeronautical Sciences