BEGIN:VCALENDAR
VERSION:2.0
PRODID:-//DTU.dk//NONSGML DTU.dk//EN
CALSCALE:GREGORIAN
BEGIN:VEVENT
DTSTART:20171120T140000
DTEND:20171120T150000
SUMMARY:DCAMM Seminar - Simulation of Delamination in 3D Composite Structures under Fatigue Loading
DESCRIPTION:<p style="text-align: left;">A DCAMM seminar&nbsp;will be presented by </p>\n<p align="center" style="margin: 0cm 0cm 10pt; text-align: center;"><strong><span>Associate Professor Albert Turon<br>\nDepartment of Mechanical Engineering and Industrial Construction<br>\nUniversity of Girona, Spain</span></strong></p>\n<p align="center" style="text-align: center; margin-bottom: 0pt;"><strong><span> <br>\n</span></strong></p>\n<br>\n<p align="center" style="text-align: center; margin-bottom: 0pt;"><strong><span>\n</span></strong>\n<strong style="text-align: justify;"></strong></p>\n<p align="center" style="text-align: justify; margin-bottom: 0pt;"><strong style="text-align: justify;">Abstract</strong><span style="text-align: justify;">:&nbsp;</span><strong>&nbsp;<br>\n</strong><span style="text-align: left;">The use of numerical tools to account for fatigue-driven delamination in the safety assessment of 3D composite structures still remains challenging. The accuracy and predictive capabilities of most of the existing simulation methods for fatigue delamination are improvable and/or limited to two-dimensional models. In this work, the method presented in [1] has been enhanced for 3D structures where the crack&nbsp;</span><span style="text-align: left;">front shape can change during propagation. A criterion to identify the crack propagation direction, as well as a new expression for the&nbsp;</span><span style="text-align: left;">three-mode decomposed J-integral, have been developed to this end. The resulting formulation has been implemented in ABAQUS to simulate the fatigue behavior of a reinforced composite plate which exhibits changing shape of the delamination front along the loading history. The method is capable to reproduce the change in crack front shape and the delamination growth rate registered during the experimental testing.</span></p>\n<p style="margin: 0cm 0cm 0.0001pt 1cm;"><span> <br>\n</span></p>\n<p align="center" style="text-align: justify; margin-bottom: 0pt;"><span style="text-align: left;"> [1] Bak B.L.V., Turon A., Lindgaard E., Lund E (2016) A Simulation Method for High- Cycle Fatigue-Driven Delamination Using a Cohesive Zone Model. International Journal for Numerical Methods in Engineering, 106, 163-191.<br>\n</span><span>&nbsp;<br>\n</span></p>\n<p style="text-align: justify;"><span></span><span style="text-align: left;">Danish pastry, coffee and tea will be served 15 minutes before the seminar starts.<br>\n</span><span>&nbsp;&nbsp;</span><br>\nAll interested persons are invited</p>
X-ALT-DESC;FMTTYPE=text/html:<p style="text-align: left;">A DCAMM seminar&nbsp;will be presented by </p>\n<p align="center" style="margin: 0cm 0cm 10pt; text-align: center;"><strong><span>Associate Professor Albert Turon<br>\nDepartment of Mechanical Engineering and Industrial Construction<br>\nUniversity of Girona, Spain</span></strong></p>\n<p align="center" style="text-align: center; margin-bottom: 0pt;"><strong><span> <br>\n</span></strong></p>\n<br>\n<p align="center" style="text-align: center; margin-bottom: 0pt;"><strong><span>\n</span></strong>\n<strong style="text-align: justify;"></strong></p>\n<p align="center" style="text-align: justify; margin-bottom: 0pt;"><strong style="text-align: justify;">Abstract</strong><span style="text-align: justify;">:&nbsp;</span><strong>&nbsp;<br>\n</strong><span style="text-align: left;">The use of numerical tools to account for fatigue-driven delamination in the safety assessment of 3D composite structures still remains challenging. The accuracy and predictive capabilities of most of the existing simulation methods for fatigue delamination are improvable and/or limited to two-dimensional models. In this work, the method presented in [1] has been enhanced for 3D structures where the crack&nbsp;</span><span style="text-align: left;">front shape can change during propagation. A criterion to identify the crack propagation direction, as well as a new expression for the&nbsp;</span><span style="text-align: left;">three-mode decomposed J-integral, have been developed to this end. The resulting formulation has been implemented in ABAQUS to simulate the fatigue behavior of a reinforced composite plate which exhibits changing shape of the delamination front along the loading history. The method is capable to reproduce the change in crack front shape and the delamination growth rate registered during the experimental testing.</span></p>\n<p style="margin: 0cm 0cm 0.0001pt 1cm;"><span> <br>\n</span></p>\n<p align="center" style="text-align: justify; margin-bottom: 0pt;"><span style="text-align: left;"> [1] Bak B.L.V., Turon A., Lindgaard E., Lund E (2016) A Simulation Method for High- Cycle Fatigue-Driven Delamination Using a Cohesive Zone Model. International Journal for Numerical Methods in Engineering, 106, 163-191.<br>\n</span><span>&nbsp;<br>\n</span></p>\n<p style="text-align: justify;"><span></span><span style="text-align: left;">Danish pastry, coffee and tea will be served 15 minutes before the seminar starts.<br>\n</span><span>&nbsp;&nbsp;</span><br>\nAll interested persons are invited</p>

URL:http://www.dcamm.dk/da/Kalender/2017/11/Seminar_No_715
DTSTAMP:20260918T060300Z
UID:{72B9A33F-6862-47BE-8C19-CFECB760A16C}-20171120T140000-20171120T140000
LOCATION: Room 1.101, Aalborg University, Fibigerstræde 16, 9220  Aalborg East
END:VEVENT
END:VCALENDAR