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

doi:10.1007/978-3-030-11969-0_6

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

^*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceeding › Chapter in a book

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 language	English
Title of host publication	PoliTO Springer Series
Publisher	Springer
Pages	83-102
Number of pages	20
DOIs	https://doi.org/10.1007/978-3-030-11969-0_6
Publication status	Published - 2019

Publication series

Name	PoliTO Springer Series
ISSN (Print)	2509-6796
ISSN (Electronic)	2509-7024

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© 2019, Springer Nature Switzerland AG.

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10.1007/978-3-030-11969-0_6

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

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.",

author = "M. Akterskaia and E. Jansen and Hallet, \{S. R.\} and Weaver, \{P. M.\} and R. Rolfes",

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doi = "10.1007/978-3-030-11969-0\_6",

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AU - Akterskaia, M.

AU - Jansen, E.

AU - Hallet, S. R.

AU - Weaver, P. M.

AU - Rolfes, R.

PY - 2019

Y1 - 2019

N2 - 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.

AB - 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.

UR - https://www.scopus.com/pages/publications/85083997522

U2 - 10.1007/978-3-030-11969-0_6

DO - 10.1007/978-3-030-11969-0_6

M3 - Chapter in a book

AN - SCOPUS:85083997522

T3 - PoliTO Springer Series

SP - 83

EP - 102

BT - PoliTO Springer Series

PB - Springer

ER -

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

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