A methodology that uses multi-axial testing and dissipated energy (DE) to characterise the mechanical behaviour of laminated composite materials has been further extended to make use of intuitive relationships between material stiffness and DE. The methodology is able to accurately predict the initiation and early progression of damage providing valuable information on the location, intensity and behaviour of damage in a composite specimen. A constitutive relationship was implemented in which the material stiffness was degraded based upon the total work and dissipated energy. The resultant material behaviour demonstrated that response characterisation of composites with complex failure modes using DE is possible, even when employing a simplistic relationship. This suggests a more detailed constitutive relationship will lead to a more accurate prediction of load response and damage behaviour of composite materials.
History
Start page
1
End page
10
Total pages
10
Outlet
Third Asia-Pacific International Symposium on Aerospace Technology (APISAT 2011)