Post-buckled propagation model for compressive fatigue of impact damaged laminates

DOI10.1016/j.ijsolstr.2008.03.014zbMath1169.74407OpenAlexW2058183219MaRDI QIDQ837422

Andrew T. Rhead, Richard J. Butler, Giles W. Hunt

Publication date: 10 September 2009

Published in: International Journal of Solids and Structures (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.ijsolstr.2008.03.014

zbMATH Keywords

propagationcomposite materialsdelaminationenergy release ratepost-bucklingfatiguelaminate

Mathematics Subject Classification ID

Plates (74K20) Composite and mixture properties (74E30) Bifurcation and buckling (74G60)

Uses Software

• VICONOPT

Cites Work

• Unnamed Item
• Unnamed Item
• Buckling and vibration of any prismatic assembly of shear and compression loaded anisotropic plates with an arbitrary supporting structure
• One dimensional modelling of failure in laminated plates by delamination buckling
• Buckling and vibration of anisotropic or isotropic plate assemblies under combined loadings
• Transverse shear deformation in exact buckling and vibration of composite plate assemblies