Post-buckling Progressive Failure Analysis of Composite Panels Using a Two-Way Global-Local Coupling Approach Including Intralaminar Failure and Debonding

M. Akterskaia, E. Jansen, S. R. Hallet, P. M. Weaver, R. Rolfes

Research output: Chapter in Book/Report/Conference proceedingChapterpeer-review

Abstract

A novel two-way global-local coupling approach to model progressive separation of skin and stringer in combination with intralaminar damage in stiffened CFRP panels under compression is presented. The methodology makes it possible to examine the damage at two levels of accuracy, taking advantage of fast calculations at the global level and assessing in detail the damage propagation at the local level. The required appropriate information exchange between the global and local level in both directions has been attained. This chapter presents an overview of this efficient approach for progressive failure analysis of composite panels and illustrates the approach on the basis of a one-stringer panel, in particular for the case of skin-stringer debonding.

Original languageEnglish
Title of host publicationPoliTO Springer Series
PublisherSpringer
Pages83-102
Number of pages20
DOIs
Publication statusPublished - 2019

Publication series

NamePoliTO Springer Series
ISSN (Print)2509-6796
ISSN (Electronic)2509-7024

Fingerprint

Dive into the research topics of 'Post-buckling Progressive Failure Analysis of Composite Panels Using a Two-Way Global-Local Coupling Approach Including Intralaminar Failure and Debonding'. Together they form a unique fingerprint.

Cite this