Subject of the paper concerns the special joints used in aeronautical structures for concentrated force introduction into the CFRP-shells. Such a kind joints were used already in the GFRP gliders designed in the WUT. They properties in CFRP application are still unknown. The joints cause the discontinuity of the shells and have the influence on the shell shear stiffnes. Therefore it is necessary to investigate the influence of the technological parameters of the joint into its strength properties.
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