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- W118964144 abstract "The results of an anlytical and experimental study of graphite-epoxy stiffened panels with impact-damaged stringer terminations are presented. Five stitched graphite-epoxy panels with stiffeners with a gradual reduction in either thickness or height were examined. Panels were analyzed using finite element analysis and tested by loading them in axial compression to a predetermined load. The panels were then subjected to impact damage and loaded to failure. Axial midplane strains, surface strains, interlaminar strains and failure results are discussed." @default.
- W118964144 created "2016-06-24" @default.
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- W118964144 date "1998-04-20" @default.
- W118964144 modified "2023-09-27" @default.
- W118964144 title "Behavior of Compression-Loaded Composite Panels With Stringer Runouts and With Impact Damage" @default.
- W118964144 hasPublicationYear "1998" @default.
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