Titlebook: ICAF 2019 – Structural Integrity in the Age of Additive Manufacturing; Proceedings of the 3 Antoni Niepokolczycki,Jerzy Komorowski Conferen

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Damage Mechanisms and Mechanical Properties of Directly Bonded CFRTP and Aluminium with Nano-Structuicantly compared to two other considered bonding cases. Furthermore, the measured traction-separation behaviour is seen to be difference for each case. Nevertheless, the applied calculation method shows some challenges related to thermal stresses and plastic deformation that should to be taken into account in future studies.

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Ply Curving Termination to Suppress Delamination in Composite Ply Drop-Offs significantly low stiffness and thus the stress concentration at the ply edge is suppressed. This paper reports the numerical analysis and experiment to validate the effectiveness of this new concept. In addition, suppression of edge delamination by PCT is also demonstrated.

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膽小鬼

2195-4356 ents innovative fatigue life enhancement methods and repair .This book gathers papers presented at the 36.th. conference and 30.th. Symposium of the International Committee on Aeronautical Fatigue and Structural integrity. Focusing on the main theme of “Structural Integrity in the Age of Additive Ma

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表示向前

Fatigue in Additive Manufactured Aircraft: The Long Way to Make It FlyAdditive Manufacturing (AM) or, more colloquially, 3D-printing..As opposed to the conventional subtractive manufacturing methodologies, AM is able to create net-shaped products by means of the addition, layer by layer, of the needed material..The biggest benefit of the AM in respect to the conventio

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NOTCH

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The Optimization and Design of Complicated-Surface Panel Based on Automate Fiber Placementure criteria are screened and perfected. Iso-parametric shell element is used to simulate skin and stiffener. A specific interface element is used to simulate between skin and stiffener. During the analysis process of the buckling, post-buckling and failure of the structure under complex loads, the

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