Conclusion
Delamination during the drilling of a carbon-epoxy composite
Research and innovation REF: RE227 V1
Conclusion
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?

6. Conclusion

The results of the proposed numerical model for predicting the critical thrust forces responsible for delamination at the hole exit were compared with the measured critical thrust forces and those obtained by analytical models based on the assumption of an orthotropic material and a circular crack. The critical forces predicted by this numerical model are driven by the energy restitution rates in Mode I and Mode II, and not only by Mode I as assumed by the analytical models

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?


Ongoing reading
Conclusion

Article included in this offer

"Material processing - Assembly"

( 161 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