Multi-level experimental and numerical analysis of composite stiffener debonding. Part 1: Non-specific specimen level

A multi-level analysis of skin/stiffener debonding is used for the fuselage design of future aircraft during postbuckling. The specimens composed of a laminate (the skin) to which an over-thickness (the flange) had been added were subjected to four-point bending, which led to interface failure betwe...

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Veröffentlicht in:	Composite structures 2009-10, Vol.90 (4), p.381-391
Hauptverfasser:	Bertolini, Julien, Castanié, Bruno, Barrau, Jean-Jacques, Navarro, Jean-Philippe
Format:	Artikel
Sprache:	eng
Schlagworte:	Buckling Engineering Sciences Exact sciences and technology Finite element analysis Fracture mechanics Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Materials and structures in mechanics Mechanics Physics Skin/stiffener debonding Solid mechanics Structural and continuum mechanics
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