Analysis of a Buffer Strip Laminate with Fiber and Matrix Damage and Interlaminar Debonding
A shear lag solution for a hybrid buffer strip laminate containing initial damage in the form of a rectilinear notch, matrix splitting and interlaminar debonding is presented. The model is a unidirectional monolayer with two symmetric constraint layers that represent angle plies. The intent of the analysis is to estimate the remote strain required to propagate the initial damage and/or to fail the laminate catastrophically. The analytical solution has a set of integral equations in which material and geometric parameters appear explicitly. Some typical results are presented for a graphite/epoxy panel having either high strength and low modulus or low strength and low modulus buffer strips. Matrix damage, angle plies, and interlaminar debonding are shown to affect the damage tolerance capability of buffer strip laminates. © 1987.
L. R. Dharani and C. P. Seaton, "Analysis of a Buffer Strip Laminate with Fiber and Matrix Damage and Interlaminar Debonding," Composite Structures, Elsevier, Jan 1987.
The definitive version is available at https://doi.org/10.1016/0263-8223(87)90004-3
Mechanical and Aerospace Engineering
International Standard Serial Number (ISSN)
Article - Journal
© 1987 Elsevier, All rights reserved.
01 Jan 1987