Calculation of hybrid joints used in modern aerospace structures
Journal Title: INCAS BULLETIN - Year 2011, Vol 3, Issue 4
Abstract
The state – of - the art of aeronautical structures show that parts are manufactured and subsequently assembled with the use of fasteners and/ or bonding. Adhesive bonding is a key technology to low weight, high fatigue resistance, robustness and an attractive design for cost structures. The paper results resolve significant problems for two groups of end-users: 1) for the aerospace design office: a robust procedure for the design of the hybrid joint structural components; 2) for the aeronautical repair centres: a useful procedure for structural design and analysis with significant cost savings.
Authors and Affiliations
Marcel STERE, Daniela BARAN
Keywords
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- EP ID EP103067
- DOI 10.13111/2066-8201.2011.3.4.15
- Views 111
- Downloads 0
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