Numerical model of critical thrust force
Delamination during the drilling of a carbon-epoxy composite
Research and innovation REF: RE227 V1
Numerical model of critical thrust force
Delamination during the drilling of a carbon-epoxy composite

Author : Dr. Redouane ZITOUNE

Publication date: April 10, 2013 | Lire en français

Logo Techniques de l'Ingenieur You do not have access to this resource.
Request your free trial access! Free trial

Already subscribed?

3. Numerical model of critical thrust force

In order to determine the thrust force responsible for delamination at the hole exit, an original numerical model is used to predict the critical thrust forces responsible for delamination at the hole exit, for a different number of plies under the drill.

This numerical model is based on the analytical models previously developed by

You do not have access to this resource.
Logo Techniques de l'Ingenieur

Exclusive to subscribers. 97% yet to be discovered!

You do not have access to this resource. Click here to request your free trial access!

Already subscribed?

Article included in this offer

"Plastics and composites"

( 329 articles )

Complete knowledge base

Updated and enriched with articles validated by our scientific committees

Services

A set of exclusive tools to complement the resources

View offer details
Contact us
Contact our team FAQ