Experiments have been made to investigate the effect of mean stress on fatigue crack propagation in +in. (12.7mm) thick specimens of six aluminium alloys of high and low fracture toughness. The resuits are presented in terms of the stress intensity factor range, AK and the R value where R is the rat
Effect of specimen thickness on fracture toughness
โ Scribed by M.O. Lai; W.G. Ferguson
- Publisher
- Elsevier Science
- Year
- 1986
- Tongue
- English
- Weight
- 703 KB
- Volume
- 23
- Category
- Article
- ISSN
- 0013-7944
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โฆ Synopsis
The variation of fracture toughness with specimen thickness for Comsteel En25 compact tension specimens ranging in thickness from 4 mm to 25 mm and tempered from the asquenched state to 600ยฐC is predicted reasonably well using the models proposed by Bluhm Proc. ASTM 61, 1324 (1961) and by Hahn er al. Met. Trans. 5, 475 (1974). Both models made use of data from two specimens of any thicknesses in the mixed mode region. The fit of the models suggested by Krafft et al. Proc. Crack Propagation Symp. p. 8, Cranfield (1961) and Tetelman et al. Fracture of Structural Materials, Wiley, New York (1967), was however less accurate. For Krafft's model, the discrepancy was attributed to the difficulty in determining an accurate G, n,il, value for thin specimens as a result of buckling. Tetelman's model implied the assumption that formation of shear lip was a surFAce phenomenon rather than one formed by a volume sensitive mechanism. This assumption did not appear reasonable for the material used in the investigation.
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