The behavior of II/III mixed-mode delamination in laminated composites and potential savings in Aerospace regarding verification processes
Visualitza/Obre
Estadístiques de LA Referencia / Recolecta
Inclou dades d'ús des de 2022
Cita com:
hdl:2117/82178
Realitzat a/ambImperial College of London
Tipus de documentTreball Final de Grau
Data2014
Condicions d'accésAccés obert
Llevat que s'hi indiqui el contrari, els
continguts d'aquesta obra estan subjectes a la llicència de Creative Commons
:
Reconeixement-NoComercial-SenseObraDerivada 3.0 Espanya
Abstract
Delamination is recognised as the most critical damage process in laminated composites:
even a simple, single plane defect can result in multi-plane delamination growth (delamination
migration) which is often associated to other secondary processes such as intralaminar
or translaminar damage. In previous research, the link between the mode III component
and delamination migration was established [9]. However, the exact mode-mixity at which
this migration occurs needs to be investigated further.
This project will determine the effect of load introduction on the migration threshold in
II/III mixed-mode delamination. The test method that will be used is a 6-point bending
plate [10] that relies on bending moments to induce mixed-mode delamination. The tests
will be instrumented with acoustic emission to capture, if possible, the onset of resin microcracking.
The test will then be interrupted for detailed fractographic analysis at the crack
front. These will give an insight of the role of bending on the fracture process of mode II-III
on multi-angled interfaces.
Col·leccions
Fitxers | Descripció | Mida | Format | Visualitza |
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FYP_OSCAR_CANO_IRANZO.compressed (1).pdf | Report | 3,003Mb | Visualitza/Obre |