Damage progression and failure of single-lap thin-ply laminated composite bolted joints under quasi-static loading (Record no. 54923)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 02546nam a2200277Ia 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | MX-MdCICY |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20250625162456.0 |
| 040 ## - CATALOGING SOURCE | |
| Transcribing agency | CICY |
| 090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN) | |
| Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) | B-20843 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 250602s9999 xx |||||s2 |||| ||und|d |
| 245 10 - TITLE STATEMENT | |
| Title | Damage progression and failure of single-lap thin-ply laminated composite bolted joints under quasi-static loading |
| 490 0# - SERIES STATEMENT | |
| Volume/sequential designation | International Journal of Mechanical Sciences, 170, p.105360, 2020 |
| 520 3# - SUMMARY, ETC. | |
| Summary, etc. | Composite bolted joints are widely used on primary and secondary load-bearing structures of aircrafts. However, investigating the damage progression and failure of composite bolted joints under high bearing loads is challenging due to the geometric, contact and material nonlinearities. In this work, an extensive experimental study has been carried out to investigate and understand the damage evolution and failure of single-lap thin-ply laminated composites bolted joints under quasi-static loading. Quasi-isotropic carbon/epoxy laminates with stacking sequence [45/0/-45/90]4s were selected for fabricating the test specimen. The specimens were observed using X-ray computed tomography (CT)scanning and SEM imaging at different stages of the loading process to evaluate internal damage and deformation characteristics. The results indicate that the bearing failure of composite bolted joints can be interpreted as an accumulated damage process with local compressing, and mainly includes four stages: damage initiation, damage evolution, non-linear softening and catastrophic failure. The major failure modes of the thin-ply laminates are found to be similar to those of traditional thickness composite, including fiber breakage, matrix cracking, delamination, fiber kinking and fiber-matrix splitting. However, the major difference is that the delamination growth in the bearing area in thin-ply composites is suppressed compared with the traditional thickness composites. Therefore, the obtained experimental data provides valuable information for developing mechanism-based failure models of single-lap thin-ply composite bolted joints. |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | LAMINATED COMPOSITES |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | BOLTED JOINTS |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | THIN-PLY |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | DAMAGE PROGRESSION |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | FAILURE |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Cao, Y. |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Cao, Z. |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Zhao, Y. |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Zuo, D. |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Tay, T. E. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://drive.google.com/file/d/1ez3qZYljPFISOThX5BUYelVbzhsuUc9-/view?usp=drivesdk">https://drive.google.com/file/d/1ez3qZYljPFISOThX5BUYelVbzhsuUc9-/view?usp=drivesdk</a> |
| Public note | Para ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | Clasificación local |
| Koha item type | Documentos solicitados |
| Lost status | Source of classification or shelving scheme | Damaged status | Not for loan | Collection | Home library | Current library | Shelving location | Date acquired | Total checkouts | Full call number | Date last seen | Price effective from | Koha item type |
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| Clasificación local | Ref1 | CICY | CICY | Documento préstamo interbibliotecario | 25.06.2025 | B-20843 | 25.06.2025 | 25.06.2025 | Documentos solicitados |