Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch

In this work, we analyze three - dimensionally, by the finite element method, the performance of the repair of aeronautical structures damaged by cracking and repaired by patch of composite materials. The effect of crack-crack interaction according to their position and interdistance was analyzed....

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Bibliographic Details
Main Authors: Nour Chafak Ibrahim, Serier Boualem, Mechab Belaïd
Format: Article
Language:English
Published: Gruppo Italiano Frattura 2018-09-01
Series:Frattura ed Integrità Strutturale
Subjects:
Online Access:https://www.fracturae.com/index.php/fis/article/view/2128