Development of a calibration for a fatigue damage model used for composite materials.
Rodríguez López, Pablo
Promotor(s) :
Bruyneel, Michaël
;
Lequesne, Cédric
Date of defense : 26-Jun-2019/27-Jun-2019 • Permalink : http://hdl.handle.net/2268.2/6577
Details
Title : | Development of a calibration for a fatigue damage model used for composite materials. |
Author : | Rodríguez López, Pablo ![]() |
Date of defense : | 26-Jun-2019/27-Jun-2019 |
Advisor(s) : | Bruyneel, Michaël ![]() Lequesne, Cédric |
Committee's member(s) : | Noels, Ludovic ![]() Ponthot, Jean-Philippe ![]() Bruyneel, Michaël ![]() Deliège, Geoffrey |
Language : | English |
Number of pages : | 50-100 |
Keywords : | [en] Composite [en] Materials [en] Finite Element Method [en] Damage [en] Mechanics [en] Implementation [en] Interlaminar [en] Simcenter |
Discipline(s) : | Engineering, computing & technology > Aerospace & aeronautics engineering |
Research unit : | Siemens PLM Software Company |
Target public : | Researchers Professionals of domain Student |
Institution(s) : | Université de Liège, Liège, Belgique |
Degree: | Cours supplémentaires destinés aux étudiants d'échange (Erasmus, ...) |
Faculty: | Master thesis of the Faculté des Sciences appliquées |
Abstract
[en] More and more manufacturing society (aeronautic, automobile or wind turbine) would like to assess the life of their composite structures. For such aim, Siemens PLM Software has developed a finite element solver to tackle the behavior of such composites under different scenarios. The most common fail under damage in composites is due to delamination between plies. In this thesis, the implementation of the interlaminar model describing the bi-triangular relation that comprises both onset and propagation relating the traction against the displacement will be implemented in the subroutine of Simcenter solver.
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