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Naji, M. |
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Motta, Antonella |
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Aletan, Dirar |
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Mohamed, Tarek |
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Ertürk, Emre |
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Taccardi, Nicola |
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Kononenko, Denys |
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Petrov, R. H. | Madrid |
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Alshaaer, Mazen | Brussels |
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Bih, L. |
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Casati, R. |
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Muller, Hermance |
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Kočí, Jan | Prague |
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Šuljagić, Marija |
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Kalteremidou, Kalliopi-Artemi | Brussels |
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Azam, Siraj |
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Ospanova, Alyiya |
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Blanpain, Bart |
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Ali, M. A. |
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Popa, V. |
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Rančić, M. |
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Ollier, Nadège |
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Azevedo, Nuno Monteiro |
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Landes, Michael |
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Rignanese, Gian-Marco |
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Shterenlikht, Anton
Alfsen og Gunderson (Norway)
in Cooperation with on an Cooperation-Score of 37%
Topics
Publications (23/23 displayed)
- 2019Fatigue of thin periodic triangular lattice platescitations
- 2019Fracture of three-dimensional lattices manufactured by selective laser meltingcitations
- 2018Modelling fracture in heterogeneous materials on HPC systems using a hybrid MPI/Fortran coarray multi-scale CAFE frameworkcitations
- 2018Multiscale CAFE for fracture in heterogeneous materials under dynamic loading conditions
- 2018Fabrication of micro-scale fracture specimens for nuclear applications by direct laser writing
- 2017Multi-scale CAFE framework for simulating fracture in heterogeneous materials implemented in fortran co-arrays and MPIcitations
- 2017Measurement of assembly stress in composite structures using the deep-hole drilling techniquecitations
- 2017Fortran coarray/MPIMulti-scale CAFE for fracture in heterogeneous materialscitations
- 2016On stability of a new side cut destructive method for measuring non-uniform residual stress in thin platescitations
- 2015Advances in the deep hole drilling technique for the residual stress measurement in composite laminates
- 2015Advances in the deep hole drilling technique for the residual stress measurement in composite laminates
- 2015Measurement of in-plane residual stresses in an AS4/8552 composite laminate using the deep-hole drilling method
- 2015Measurement of in-plane residual stresses in an AS4/8552 composite laminate using the deep-hole drilling method
- 2014Prediction of crack propagation and arrest in X100 natural gas transmission pipelines with a strain rate dependent damage model (SRDD). Part 2citations
- 2013Prediction of crack propagation and arrest in X100 natural gas transmission pipelines with the strain rate dependent damage model (SRDD). Part 1citations
- 2013The Role of Grain Size on Deformation of 316H Austenitic Stainless Steel
- 2010The evolution of crack-tip stresses during a fatigue overload eventcitations
- 2010Influence of gas depressurisation on the ductile fracture propagation of X80 and X100 steel pipelines
- 2006The CAFE model of fracture - application to a TMCR steelcitations
- 2006A general method for coupling microstructural response with structural performancecitations
- 2005Modeling the ductile-brittle transition behavior in thermomechanically controlled rolled steelscitations
- 2005Assessment of an instrumented Charpy impact machinecitations
- 20043D CAFE modelling of transitional ductile fracture in steels
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article
Prediction of crack propagation and arrest in X100 natural gas transmission pipelines with a strain rate dependent damage model (SRDD). Part 2
Abstract
<p>Part 1 of this paper described a specimen for the measurement of high strain rate flow and fracture properties of pipe material and for tuning a strain rate dependent damage model (SRDD). In part 2 the tuned SRDD model is used for the simulation of axial crack propagation and arrest in X100 natural gas pipelines. Linear pressure drop model was adopted behind the crack tip, and an exponential gas depressurisation model was used ahead of the crack tip. The model correctly predicted the crack initiation (burst) pressure, the crack speed and the crack arrest length. Strain rates between 1000s<sup>-1</sup> and 3000s<sup>-1</sup> immediately ahead of the crack tip are predicted, giving a strong indication that a strain rate material model is required for the structural integrity assessment of the natural gas pipelines. The models predict the stress triaxiality of about 0.65 for at least 1m ahead of the crack tip, gradually dropping to 0.5 at distances of about 5-7m ahead of the crack tip. Finally, the models predicted a linear drop in crack tip opening angle (CTOA) from about 11-12° at the onset of crack propagation down to 7-8° at crack arrest. Only the lower of these values agree with those reported in the literature for quasi-static measurements. This discrepancy might indicate substantial strain rate dependence in CTOA.</p>