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....
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 |
Similar Items
-
Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch
by: Nour Chafak Mohamed Ibrahim, et al.
Published: (2018-10-01) -
Modeling of a cracked and repaired Al 2024T3 aircraft plate: effect of the composite patch shape on the repair performance
by: Baghdadi Mohammed, et al.
Published: (2019-10-01) -
Full Analysis of All Composite Patch Repairing Design Parameters
by: A. Ait Yala, et al.
Published: (2018-12-01) -
Modeling of a cracked and repaired Al 2024T3 aircraft plate: effect of the composite patch shape on the repair performance
by: Mohammed Baghdadi, et al.
Published: (2019-07-01) -
Fatigue crack growth of composite patch repaired Al-alloy plates under variable amplitude loading
by: Fatima Zohra Seriari, et al.
Published: (2017-12-01)