作者: Tomas Rodriguez Hernandez , Alberto Arana Hidalgo
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摘要: A stringer made of composite material for reinforcing aircraft skin panels. Plies are introduced at 90° in a segment close to the run-out, and progressively reducing number plies 0°, such that majority is an adjacent so stiffness run-out reduced, load it supports also therefore reduced. This alternative solution solutions already existing getting run-outs support smaller load, thereby both risk peeling off separation between panel. method manufacturing said provided.