O. Ranestad et al., An engineering method for constraint based fracture assessment of welded structural components with surface cracks, ENG FRACT M, 63(6), 1999, pp. 653-674
In this study it has been shown that accurate descriptions of crack-tip str
ess-fields in surface cracked welded plates can be obtained without large 3
D FEA models. When a fracture mechanics FE analysis is required in a large
construction, existing shell models can be used in combination with a plane
strain submodel. The 2D plane strain model is driven by displacements from
the global shell model. This technique has been used to simulate crack-tip
stress-fields in a surface cracked plate. The crack-tip stress fields are
characterised with the J-integral and the constraint parameter, Q. The crac
k in the global shell model was simulated with line-spring elements. The gl
obal behaviour as well as the crack-tip stress-fields of the plane strain s
ubmodel have been compared to a 3D solid model. Initially, the crack-tip st
ress-fields in the plane strain model and the 3D model with surface crack w
ere compared, using the same inplane mesh and element type. It was found th
at when first order elements were used, the constraint was higher in 3D tha
n in plane strain. For second order elements, however, the trend was the op
posite. By using a correction factor for the load, the load vs. J behaviour
and the crack-tip stress-fields of a surface cracked plate can be predicte
d from a shell analysis with line-spring elements and a plane strain model.
Accurate predictions of J and Q were obtained using the shell + submodel t
echnique for homogeneous material and for a weldment with fusion line crack
. The shell + submodelling technique was used to assess brittle fracture in
two steel weldments with a surface crack using the RKR failure criterion b
y Ritchie et al. [16]. For the investigated case, the toughness requirement
s could be relaxed significantly based on the two parameter analysis compar
ed to conventional fracture mechanics analyses. (C) 1999 Elsevier Science L
td. All rights reserved.