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


Rhead, A. T., Butler, R. and Hunt, G. W., 2009. Post-buckled propagation model for compressive fatigue of impact damaged laminates. International Journal of Solids and Structures, 45 (16), pp. 4349-4361.

Related documents:

This repository does not currently have the full-text of this item.
You may be able to access a copy if URLs are provided below. (Contact Author)

Official URL:

Related URLs:


An analytical model for prediction of compressive fatigue threshold strains in composite plates with barely visible impact damage (BVID) is presented. The model represents the complex damage morphology as a single circular delamination at a critical level and calculates the strain at which thin-film buckling of the circular delaminated region occurs. The threshold strain is defined as the strain at which the strain energy release rate for the fracture of post-buckled delaminated plies along the delamination is equal to the critical Mode I value (G1C) for the resin. The model predicts the critical through-thickness level for delamination, the stability of delamination growth and also the sensitivity to experimental error in geometric measurements of the damage area. Results obtained using the model show an agreement of fatigue strain to within 4% of experimental values for four sets of data reported in the literature.


Item Type Articles
CreatorsRhead, A. T., Butler, R. and Hunt, G. W.
Related URLs
Uncontrolled Keywordscomposite materials,fatigue,energy release rate,propagation,delamination,post-buckling,laminate
DepartmentsFaculty of Engineering & Design > Mechanical Engineering
Research CentresAerospace Engineering Research Centre
ID Code15177


Actions (login required)

View Item