Modelling Delamination in an Equivalent Single Layer Model in Explicit Finite Element Analysis

Master Thesis (2017)
Author(s)

Jurrien Koeman (TU Delft - Aerospace Engineering)

Contributor(s)

Christos Kassapoglou – Mentor

Christian Bögle – Mentor

Chiara Bisagni – Graduation committee member

Dimitrios Zarouchas – Graduation committee member

Faculty
Aerospace Engineering
More Info
expand_more
Publication Year
2017
Language
English
Graduation Date
19-12-2017
Awarding Institution
Delft University of Technology
Programme
Aerospace Engineering
Sponsors
BMW AG Forschungs- und Innovationszentrum
Faculty
Aerospace Engineering
Page Views
289
Collections
thesis
Reuse Rights

Other than for strictly personal use, it is not permitted to download, forward or distribute the text or part of it, without the consent of the author(s) and/or copyright holder(s), unless the work is under an open content license such as Creative Commons.

Abstract

Delamination is one of the failure modes of composites prone to happen in the case of a car crash. In the early stages of car design, finite element analysis is used as a tool to analyze structural concepts. In order to model delamination in a newly developed material model, it is analyzed in two parts: detection and effects of delamination. To detect delamination in an equivalent single layer model in explicit finite element analysis, the transverse shear stresses are recovered from the solution of a time step, followed by the application of a stress-based delamination failure criterion. The second part results in the following: to model the effects of delamination in the same framework, each effect has to be treated separately, leading to the use of a delamination damage factor to reduce the bending stiffness and stresses due to delamination.

Files

Koeman_2017_Modelling_Delamina... (pdf)
(pdf | 3.76 Mb)
- Embargo expired in 19-12-2022
License info not available