%0 Journal Article
%T Calculation of hybrid joints used in modern aerospace structures
%A Marcel STERE
%A Daniela BARAN
%J INCAS Bulletin
%D 2011
%I National Institute for Aerospace Research ˇ°Elie Carafoliˇ± - INCAS
%R 10.13111/2066-8201.2011.3.4.15
%X The state ¨C 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.
%K aircraft
%K hybrid joint
%K adhesive bonding
%K strap joint (single and double)
%K FEA
%K ANSYS
%U http://bulletin.incas.ro/files/stere_baran_v3_iss_4_full.pdf