Finite element procedures were used to generate stress intensity, crack mouth compliance, and load point compliance for a segment from a cylindrical shell. Stress intensity and crack mouth compliance were found to be independent of span length for a large range of crack lengths when suitably nommhxe
A comparison of various fracture toughness testing methods
β Scribed by Susil K. Putatunda
- Publisher
- Elsevier Science
- Year
- 1986
- Tongue
- English
- Weight
- 971 KB
- Volume
- 25
- Category
- Article
- ISSN
- 0013-7944
No coin nor oath required. For personal study only.
β¦ Synopsis
comparative study of the various fracture toughness test methods and estimation procedures has been carried out. The fracture toughness of AISI 4340 steel has been determined by several methods, i.e. (i) JR curve, (ii) 6, curve, (iii) K, curve, (iv) stretch zone size measurements (v) non-linear energy method of Poulose et al. and by (vi) a new procedure proposed recently by Banerjee. Compact tension specimens with TL orientation have been used. All the specimens used satisfied the ASTM E813 test size requirements. Applicability of various fracture toughness estimation procedures like (i) Hanhn and Rosenfield, (ii) Rolfe and Barsom and (iii) equivalent energy rate method of Bucci et al. have been examined. These values have been compared with true fracture toughness of the material obtained by ASTM E399 test procedure. Comparison of various conventional test methods indicate multiple specimen 6, curve method gives most consistent results and these values are within + 15% of the true fracture toughness value. Out of all estimation procedures
Rolfe and Barsom's method appears to be best, giving &. number within +8% of the true fracture toughness value. Non-linear energy method was found to give a fracture toughness value consistent with true fracture toughness of the material.
π SIMILAR VOLUMES
Ahstraet--A modified criterion is developed on an empirical basis for the minimum thickness Brain of a plane strain fracture toughness test specimen: B.,. = 400 g~o Ecq. where K~, is the plane strain fracture toughness, E is the Young's modulus and ~r~, is the yield stress of the material. The modi
hharaet--A compact form of C-shape fracture toughness test specimen is investigated. The specimen can be taken from thick-walled cylinders with greater material economy than the proposed ASTM C-shape, but is more difficult to manufacture. The K-calibration is identical with the ASTM compact tension
The dynamic fatigue life equation is appfied to uniaxial tensile test. The resultant equations for the surface energy and fracture toughness are calculated with the data from the tensile test and compared with the ones from ASTM E399 test. During the crack propagation under model loading, the materi