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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-Structunforced thermoplastic (CFRTP) and aluminium. A nanostructure is manufactured on the aluminium surface and is directly bonded to the CFRTP by applying heat and pressure. Double cantilever beam (DCB) testing is carried out to evaluate the bonding properties and the initial results of a method for dire
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Analytical and Numerical Investigation of the Effect of Secondary Bending in Hard-Point Jointss of mechanical fasteners. Upon cabin pressurization, membrane stresses are induced in the skin sheets every flight. Fastened attachments include inherent eccentricity with respect to the load path, which induces out of plane deflections of the skin sheets. This is referred to as ‘secondary bending’
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Demonstration of an Airframe Digital Twin Framework Using a CF-188 Full-Scale Component Testlow proactive and cost-effective decisions on an individual aircraft basis. The National Research Council of Canada is currently demonstrating the ADT framework using a CF–188 full-scale component test to assess the adaptability of this approach for Royal Canadian Air Force (RCAF) fleets. An in-hous
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