Please use this identifier to cite or link to this item:
http://localhost:8080/xmlui/handle/123456789/2910Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Rambabu, P. | - |
| dc.contributor.author | Narasayya, Ch.V.A. | - |
| dc.contributor.author | Mohan, M.K. | - |
| dc.contributor.author | Prasad, N. Eswara | - |
| dc.date.accessioned | 2025-01-24T05:45:26Z | - |
| dc.date.available | 2025-01-24T05:45:26Z | - |
| dc.date.issued | 2015 | - |
| dc.identifier.citation | 10.1016/j.matpr.2015.07.008 | en_US |
| dc.identifier.uri | http://localhost:8080/xmlui/handle/123456789/2910 | - |
| dc.description | NITW | en_US |
| dc.description.abstract | The effect of ageing on the mixed mode fracture toughness (I/III) was evaluated for the aluminium alloy AA2219 in limited underaged (LUA), underaged (UA) peakaged (PA) and overaged (OA) conditions. Opening mode fracture toughness (Mode I) test was conducted. Sheet tensile samples were prepared and tested in all the ageing conditions. Optical microscopy has been carried out and fractographic studies have been conducted to study and determine the mode of failure. | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | Materials Today: Proceedings | en_US |
| dc.subject | Mixed Mode Fracture Toughness (I/III) | en_US |
| dc.subject | Over aged (OA) | en_US |
| dc.title | Mixed Mode (I/III) Fracture Behaviour of an Aerospace Grade Aluminium Alloy in Different Ageing Conditions | en_US |
| dc.type | Other | en_US |
| Appears in Collections: | Metallurgical and Materials Engineering | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 1-s2.0-S2214785315002539-main.pdf | 812.1 kB | Adobe PDF | View/Open |
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