Prediction of the post-crushing compressive response of progressively crushable sandwich foam cores
File(s)Post_crushing_foam_Gigliotti.pdf (1.98 MB)
Accepted version
Author(s)
Gigliotti, L
Pinho, ST
Type
Journal Article
Abstract
In this paper, a novel analytical model for predicting the post-crushing compressive response of progressively crushable sandwich foam cores is presented. The calibration of the model is performed using experimental measurements obtained exclusively from standard monotonic compressive tests. Therefore, the need for performing time-consuming compressive tests including multiple unloading–reloading cycles is avoided. Model predictions have been validated against experimental measurements available for three different foam materials. The model is shown to accurately predict the thickness of the crushed material layer during progressive crushing and the residual after-crushing strain (with a maximum error of 12.1%). The proposed model is capable of predicting the residual after-crushing strain with a significantly smaller error (error-reduction over 56%) than existing models, whose calibrations require the same experimental measurements as the present model. The results presented in this work demonstrate the relevance of the proposed model for a damage-tolerant design of foam-cored composite sandwich structures.
Date Issued
2016-01
Date Acceptance
2015-10-06
Citation
Composites Part A - Applied Science and Manufacturing, 2016, 80, pp.148-158
ISSN
1359-835X
Publisher
Elsevier
Start Page
148
End Page
158
Journal / Book Title
Composites Part A - Applied Science and Manufacturing
Volume
80
Copyright Statement
© 2016, Elsevier. Licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/
Sponsor
Airbus
Grant Number
PO 1100081421
Subjects
Science & Technology
Technology
Engineering, Manufacturing
Materials Science, Composites
Engineering
Materials Science
Foams
Sandwich structures
Damage tolerance
Analytical modelling
CELL POLYOLEFIN FOAMS
UNIAXIAL COMPRESSION
POLYMERIC FOAMS
IMPACT BEHAVIOR
PANELS
INDENTATION
DAMAGE
TRAIN
BEAMS
Materials
0912 Materials Engineering
0913 Mechanical Engineering
0901 Aerospace Engineering
Publication Status
Published
Date Publish Online
2015-10-23