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عدد المساهمات : 18994 التقييم : 35488 تاريخ التسجيل : 01/07/2009 الدولة : مصر العمل : مدير منتدى هندسة الإنتاج والتصميم الميكانيكى
| موضوع: بحث بعنوان Modeling of fracture processes in laminate composite plates with embedded delamination الإثنين 11 يناير 2021, 10:24 pm | |
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أخوانى فى الله أحضرت لكم بحث بعنوان Modeling of fracture processes in laminate composite plates with embedded delamination Mikhail A. Tashkinov Perm National Research Polytechnic University, Russia
و المحتوى كما يلي :
ABSTRACT. This work is devoted to research and development of models for the processes of nucleation and growth of delamination in laminated composite materials. Possibilities of fracture mechanics approaches using virtual crack closure technique as well as progressive failure analysis based on the failure criteria are demonstrated. Influence of the initial delamination size on the rate of growth of the defect is studied. A comparative analysis of the applicability of fracture criteria to modeling of samples with delamination were performed, including implementation of element deletion algorithm. The numerical results obtained with the studied methods were compared. KEYWORDS. Composite laminates; Delamination; VCCT; Progressive failure analysis; Fracture criteria; Element deletion. CONCLUSIONS Several methods of simulation of the delamination in composite materials samples have been investigated. The effect of defect size on the parameters of deformation and failure of the sample was established. Computational experiments were performed to explore the possibility of the delamination simulation using progressive failure models, applying various criteria. It can be stated that a defect in the form of delamination has a significant influence on the strength of the samples and its presence can be modeled using both methods of fracture mechanics and methods based on failure criteria. The energy approaches for modeling the growth of the delamination seem more promising, however, because the methods using the values of stress fields in the failure criteria, in general, impose additional conditions on the model’s geometrical properties. Thus, the appearance of a singularity due to distortion of the geometry or features of the finite-element mesh, can prevent achieving reliable results. At the same time, disadvantage of the energy techniques is that they require a predetermine position of the delamination in the structure. Thus, currently the combined methods are being developed, which utilize failure criteria for locating the start of delamination and the fracture mechanics methods to modeling its subsequent growth [29]. The initial information about the presence of the delamination can be also obtained by experimental approaches. Among them are the non-destructive testing methods such as acoustic emission, ultrasonic examination and others [30-33]. Another promising direction is embedding of the sensor elements, such as piezoelectric sensors and sensors, based on optical fibers [34-36]. Indications of such sensors may be also used for verification of failure models as well as predictions of durability of structures based on them. Another approach to improve the models of delamination in composites is account of a different nature of defects. Thus, in the case of manufacturing-induced defects, the occurrence of delamination is often accompanied by the presence of socalled “resin pockets”. In this case, a more accurate model is required, that considers resin as a separate component with isotropic properties. Also, the temperature factors can affect the rate of growth, the effect of which may be incorporated in the models with the appropriate constitutive relations. Thus, based on the basic principles, including those reflected in this paper, for each specific case of the composite structure the model that most closely simulates the formation and development of the defects can be created.
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