Titlebook: Damage Growth in Aerospace Composites; Aniello Riccio Book 2015 Springer International Publishing Switzerland 2015 Aerospace Composite Mat

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Delamination and Debonding Growth in Composite Structurespace is developing reliable simulation techniques for composites structural behaviour in the presence of damages such as interlaminar delaminations and debondings. These are able to perform Progressive Failure Analysis (PFA), are efficient from a computational point of view, and correct mesh size ef

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Influence of Intralaminar Damage on the Delamination Crack Evolutionchapter is to investigate the influence of the intralaminar damage (transverse matrix cracks and their associated local delaminations) on the interlaminar damage (delamination) evolution in composite laminate materials. Using specific device setups and coupons, this influence on the delamination ons

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A Fast Numerical Methodology for Delamination Growth Initiation Simulationerospace composite structures, it is mandatory to account for the effects of delaminations and their evolution even in the earlier stages of the design process. In order to achieve this goal, newer and faster numerical procedures representing the main phenomenological features governing the structur

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Seda Uğurlu,Başar Öztayşi,Cengiz Kahramanpace is developing reliable simulation techniques for composites structural behaviour in the presence of damages such as interlaminar delaminations and debondings. These are able to perform Progressive Failure Analysis (PFA), are efficient from a computational point of view, and correct mesh size ef

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Introduction,, arising after impact with foreign objects or caused by manufacturing defects, makes designing with composites a challenging task. In recent years, the inability to predict the damage onset and its evolution in aerospace composite structures, has led to over-conservative designs, not fully realizin

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Detailed Methodologies for Integrated Delamination Growth and Fiber-Matrix Damage Progression Simulatrix breakage. Delaminations, which can arise during the manufacturing process or as a consequence of impacts from foreign objects, are probably the most investigated mode of failure in composite laminates. However, others damages such as matrix cracks, fiber–-matrix debonding, and fiber fractures c