An experimental and numerical study on omega stringer debonding

Omega stringers offer interesting structural capabilities and are expected on future aircraft fuselages. In postbuckling mode, the final failure of these structures may occur by stringer debonding between stringer flanges and the skin of the fuselage. In this study, it is demonstrated that the use o...

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Veröffentlicht in:	Composite structures 2008-11, Vol.86 (1), p.233-242
Hauptverfasser:	Bertolini, Julien, Castanié, Bruno, Barrau, Jean-Jacques, Navarro, Jean-Philippe
Format:	Artikel
Sprache:	eng
Schlagworte:	Buckling Engineering Sciences Exact sciences and technology Fracture mechanics Fracture mechanics (crack, fatigue, damage...) Fundamental areas of phenomenology (including applications) Materials and structures in mechanics Mechanics Omega Physics Resin fillets Skin/stiffener debonding Solid mechanics Structural and continuum mechanics
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