Two-parameter fracture assessment of surface cracked cylindrical shells during collapse
The present study addresses the use of CTOD and T-stress in fracture assessments of surface cracked shell structures. A new software is developed for this purpose, denoted LINK pipe. It is based on a combination of a quadrilateral assumed natural deviatoric strain thin shell finite element and an im...
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Veröffentlicht in: | Engineering fracture mechanics 2006, Vol.73 (2), p.264-282 |
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Sprache: | eng |
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Zusammenfassung: | The present study addresses the use of CTOD and
T-stress in fracture assessments of surface cracked shell structures. A new software is developed for this purpose, denoted LINK
pipe. It is based on a combination of a quadrilateral assumed natural deviatoric strain thin shell finite element and an improved linespring finite element. Plasticity is accounted for using stress resultants. A power law hardening model is used for shell and linespring materials. A co-rotational formulation is employed to represent nonlinear geometry effects. With this, one can carry out nonlinear fracture mechanics assessments in structures that show instabilities due buckling (local/global), ovalisation and large rigid body motion. Many constraint-measuring parameters have been proposed, with the
Q-parameter or the
T-stress being the most popular ones. Solid finite element meshing for complex structures such as pipes containing semi-elliptical surface cracks in order to compute
Q is at present not a feasible approach. However, shell structures are most conveniently meshed with shell finite elements, and the linespring finite element is a natural way of accounting for surface cracks. The
T-stress is readily obtained from the linespring membrane force and bending moment along the surface crack. In this study we present a new approach to analyse cracked shell structures subjected to large geometric changes. By numerical examples it is shown how geometric instabilities and fracture compete as governing failure mode. |
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ISSN: | 0013-7944 1873-7315 |
DOI: | 10.1016/j.engfracmech.2005.03.012 |