The plane strain fracture toughness of a high strength low alloy steel, En 25, tempered from the as-quenched state to 650°C, and a high strength aluminium alloy, 7075-T6, have been determined using compact tension specimens of varying thicknesses from 4 to 25mm. The size of the shear lips, BSL, measured at the free surfaces of the specimens was found to be independent of the specimen thickness and to be related to the true plane strain fracture toughness, KIC, through the expression BSL = 0.41(KIC/σ ys)2.02, where σys is the 0.2% proof stress of the material. A rationale for this behaviour is that BSL is approximately equal to the size of the plane stress plastic zone, ry, at the surfaces of a plate specimen, which from theoretical analysis, has been shown to be rY = Π/8(KIC/σYS)2. The ASTM standard plane strain fracture toughness test method has been proven to be insensitive to detect excess yielding in the specimens tempered at temperatures higher than 450°C. At high tempers, yielding fracture mechanics approaches were used to determine the true KIC values. The fracture toughness versus shear lip size relationship is believed to have considerable importance in the analysis of service failures and in the preliminary study of specimen size effect in plane strain fracture toughness determination.
| Identifer | oai:union.ndltd.org:ADTP/275337 |
| Date | January 1977 |
| Creators | Lai, M. O. (Man On), 1947- |
| Publisher | ResearchSpace@Auckland |
| Source Sets | Australiasian Digital Theses Program |
| Language | English |
| Detected Language | English |
| Rights | Items in ResearchSpace are protected by copyright, with all rights reserved, unless otherwise indicated., http://researchspace.auckland.ac.nz/docs/uoa-docs/rights.htm, Copyright: The author |
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