The determination of Mode III fracture toughness in thick composite laminates (Record no. 45245)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 01804nam a2200241Ia 4500 |
| 003 - CONTROL NUMBER IDENTIFIER | |
| control field | MX-MdCICY |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20250625140642.0 |
| 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-11018 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 250602s9999 xx |||||s2 |||| ||und|d |
| 245 10 - TITLE STATEMENT | |
| Title | The determination of Mode III fracture toughness in thick composite laminates |
| 490 0# - SERIES STATEMENT | |
| Volume/sequential designation | Composites Science and Technology, 56, p.489-499, 1996 |
| 520 3# - SUMMARY, ETC. | |
| Summary, etc. | In this paper we propose a method of determining the Mode ZZZ interlaminar fracture toughness in thick composite laminates. Previous finite element results show that when an edge-cracked composite specimen is subjected to torsion loading, the fracture behavior is dominated by Mode III. In order to simplify the calculation of strain energy release rate, an analytical series solution employing effective moduli is derived to study the fracture behavior of edge-cracked multilayer laminates. This analytical tool is applied for angle-ply laminates to characterize the critical strain energy release rates. Several angle-ply laminates with artificial damage located at arbitrary interfaces have been tested to find the interlaminar fracture toughness under torsion loading. Experimental results show that Gut, ranges from 650 to 850 J/m2 for most cases. Test results reveal that this theory and experimental method can be used to find interlaminar Gmc values for angle-ply composites. |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | MODE III FRACTURE TOUGHNESS |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | THICK COMPOSITE LAMINATE |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | TORSION |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | EFFECTIVE SHEAR MODULI |
| 650 14 - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | SHEAR ANISOTROPY FACTOR |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Liao, W.C. |
| 700 12 - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Sun, C.T. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="https://drive.google.com/file/d/1ASEGKos0txX5_n8CVuskTHoXtqEtYaPe/view?usp=drivesdk">https://drive.google.com/file/d/1ASEGKos0txX5_n8CVuskTHoXtqEtYaPe/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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Clasificación local | Ref1 | CICY | CICY | Documento préstamo interbibliotecario | 25.06.2025 | B-11018 | 25.06.2025 | 25.06.2025 | Documentos solicitados |