Experimental and Numerical Failure Analysis of Adhesive Composite Joints
In the first section of this work, a suitable data reduction scheme is developed to measure the adhesive joints strain energy release rate under pure mode-I loading, and in the second section, three types of adhesive hybrid lap-joints, that is, Aluminum-GFRP (Glass Fiber Reinforced Plastic), GFRP-GF...
Saved in:
| Main Author: | |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Wiley
2012-01-01
|
| Series: | International Journal of Aerospace Engineering |
| Online Access: | http://dx.doi.org/10.1155/2012/925340 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| _version_ | 1832548473796296704 |
|---|---|
| author | Farhad Asgari Mehrabadi |
| author_facet | Farhad Asgari Mehrabadi |
| author_sort | Farhad Asgari Mehrabadi |
| collection | DOAJ |
| description | In the first section of this work, a suitable data reduction scheme is developed to measure the adhesive joints strain energy release rate under pure mode-I loading, and in the second section, three types of adhesive hybrid lap-joints, that is, Aluminum-GFRP (Glass Fiber Reinforced Plastic), GFRP-GFRP, and Steel-GFRP were employed in the determination of adhesive hybrid joints strengths and failures that occur at these assemblies under tension loading. To achieve the aims, Double Cantilever Beam (DCB) was used to evaluate the fracture state under the mode-I loading (opening mode) and also hybrid lap-joint was employed to investigate the failure load and strength of bonded joints. The finite-element study was carried out to understand the stress intensity factors in DCB test to account fracture toughness using J-integral method as a useful tool for predicting crack failures. In the case of hybrid lap-joint tests, a numerical modeling was also performed to determine the adhesive stress distribution and stress concentrations in the side of lap-joint. Results are discussed in terms of their relationship with adhesively bonded joints and thus can be used to develop appropriate approaches aimed at using adhesive bonding and extending the lives of adhesively bonded repairs for aerospace structures. |
| format | Article |
| id | doaj-art-884cd7a8f09e4a0ab088083c9c228760 |
| institution | Kabale University |
| issn | 1687-5966 1687-5974 |
| language | English |
| publishDate | 2012-01-01 |
| publisher | Wiley |
| record_format | Article |
| series | International Journal of Aerospace Engineering |
| spelling | doaj-art-884cd7a8f09e4a0ab088083c9c2287602025-02-03T06:14:04ZengWileyInternational Journal of Aerospace Engineering1687-59661687-59742012-01-01201210.1155/2012/925340925340Experimental and Numerical Failure Analysis of Adhesive Composite JointsFarhad Asgari Mehrabadi0Department of Mechanical Engineering, Islamic Azad University, Arak Branch, Arak 567-38135, IranIn the first section of this work, a suitable data reduction scheme is developed to measure the adhesive joints strain energy release rate under pure mode-I loading, and in the second section, three types of adhesive hybrid lap-joints, that is, Aluminum-GFRP (Glass Fiber Reinforced Plastic), GFRP-GFRP, and Steel-GFRP were employed in the determination of adhesive hybrid joints strengths and failures that occur at these assemblies under tension loading. To achieve the aims, Double Cantilever Beam (DCB) was used to evaluate the fracture state under the mode-I loading (opening mode) and also hybrid lap-joint was employed to investigate the failure load and strength of bonded joints. The finite-element study was carried out to understand the stress intensity factors in DCB test to account fracture toughness using J-integral method as a useful tool for predicting crack failures. In the case of hybrid lap-joint tests, a numerical modeling was also performed to determine the adhesive stress distribution and stress concentrations in the side of lap-joint. Results are discussed in terms of their relationship with adhesively bonded joints and thus can be used to develop appropriate approaches aimed at using adhesive bonding and extending the lives of adhesively bonded repairs for aerospace structures.http://dx.doi.org/10.1155/2012/925340 |
| spellingShingle | Farhad Asgari Mehrabadi Experimental and Numerical Failure Analysis of Adhesive Composite Joints International Journal of Aerospace Engineering |
| title | Experimental and Numerical Failure Analysis of Adhesive Composite Joints |
| title_full | Experimental and Numerical Failure Analysis of Adhesive Composite Joints |
| title_fullStr | Experimental and Numerical Failure Analysis of Adhesive Composite Joints |
| title_full_unstemmed | Experimental and Numerical Failure Analysis of Adhesive Composite Joints |
| title_short | Experimental and Numerical Failure Analysis of Adhesive Composite Joints |
| title_sort | experimental and numerical failure analysis of adhesive composite joints |
| url | http://dx.doi.org/10.1155/2012/925340 |
| work_keys_str_mv | AT farhadasgarimehrabadi experimentalandnumericalfailureanalysisofadhesivecompositejoints |