Delamination Fracture Analysis of Composite Laminates Caused by Local Buckling and Postbuckling

911986

09/01/1991

Event
International Pacific Air & Space Technolgy Conference
Authors Abstract
Content
Localized buckling of delaminated sublaminates in composite plates creates high interlaminar stresses around the delamination boundary, and then often causes rapid extensive delamination growth. This delamination growth reduces the global stiffness and thereby lowers the buckling load of the laminate significantly. With use of the VCCTS technique proposed by the authors, quantitative multiple parametric analyses of embedded elliptically-shaped delamination growth are provided in detail for the first time in this paper. The new results in this paper show that whether a delamination grows or not is determined by both the geometrical and physical parameters and their relations, and therefore they can be used to predict the growth of delaminations with varied kind of parameters.
Meta TagsDetails
DOI
https://doi.org/10.4271/911986
Pages
10
Citation
Tsao, D., Duan, D., and Ji, W., "Delamination Fracture Analysis of Composite Laminates Caused by Local Buckling and Postbuckling," SAE Technical Paper 911986, 1991, https://doi.org/10.4271/911986.
Additional Details
Publisher
Published
Sep 1, 1991
Product Code
911986
Content Type
Technical Paper
Language
English