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. T...
Saved in:
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Gruppo Italiano Frattura
2018-10-01
|
| Series: | Fracture and Structural Integrity |
| Subjects: | |
| Online Access: | http://www.gruppofrattura.it/pdf/rivista/numero46/numero_46_art_14.pdf |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832544376886132736 |
|---|---|
| author | Nour Chafak Mohamed Ibrahim Serier Boualem, Mechab Belad |
| author_facet | Nour Chafak Mohamed Ibrahim Serier Boualem, Mechab Belad |
| author_sort | Nour Chafak Mohamed Ibrahim |
| collection | DOAJ |
| description | 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. The criterion of rupture retained for this study is the factor of intensity of constraints. We show that this factor increases considerably and reaches a critical threshold when the two cracks develop towards each other. The repair of such damage using a composite patch ensures the stability of this structure during the commissioning process. The sharp fall in the stress intensity factor is characteristic of this stability |
| format | Article |
| id | doaj-art-f509cedfb5b74bc2acdcfa7a09244bff |
| institution | Kabale University |
| issn | 1971-8993 |
| language | English |
| publishDate | 2018-10-01 |
| publisher | Gruppo Italiano Frattura |
| record_format | Article |
| series | Fracture and Structural Integrity |
| spelling | doaj-art-f509cedfb5b74bc2acdcfa7a09244bff2025-02-03T10:38:28ZengGruppo Italiano FratturaFracture and Structural Integrity1971-89932018-10-01124614014910.3221/IGF-ESIS.46.1410.3221/IGF-ESIS.46.14Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patchNour Chafak Mohamed IbrahimSerier Boualem,Mechab BeladIn 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. The criterion of rupture retained for this study is the factor of intensity of constraints. We show that this factor increases considerably and reaches a critical threshold when the two cracks develop towards each other. The repair of such damage using a composite patch ensures the stability of this structure during the commissioning process. The sharp fall in the stress intensity factor is characteristic of this stabilityhttp://www.gruppofrattura.it/pdf/rivista/numero46/numero_46_art_14.pdfPlate Repair Adhesive Patch Composite materials Crack Finite elements Stress intensity factor |
| spellingShingle | Nour Chafak Mohamed Ibrahim Serier Boualem, Mechab Belad Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch Fracture and Structural Integrity Plate Repair Adhesive Patch Composite materials Crack Finite elements Stress intensity factor |
| title | Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch |
| title_full | Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch |
| title_fullStr | Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch |
| title_full_unstemmed | Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch |
| title_short | Analysis of the crack-crack interaction effect initiated in aeronautical structures and repaired by composite patch |
| title_sort | analysis of the crack crack interaction effect initiated in aeronautical structures and repaired by composite patch |
| topic | Plate Repair Adhesive Patch Composite materials Crack Finite elements Stress intensity factor |
| url | http://www.gruppofrattura.it/pdf/rivista/numero46/numero_46_art_14.pdf |
| work_keys_str_mv | AT nourchafakmohamedibrahim analysisofthecrackcrackinteractioneffectinitiatedinaeronauticalstructuresandrepairedbycompositepatch AT serierboualem analysisofthecrackcrackinteractioneffectinitiatedinaeronauticalstructuresandrepairedbycompositepatch AT mechabbelad analysisofthecrackcrackinteractioneffectinitiatedinaeronauticalstructuresandrepairedbycompositepatch |