Structural behaviour modelling of bolted joints in composite laminates subjected to cyclic loading

The structural behaviour of bolted joints of composite laminates for aerospace applications was modelled comparing the shape, amplitude and phase of stress–strain cycles. This study proposes a model for the bolted joints resulting in a typical load–displacement curve, under cyclic loading, significa...

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Veröffentlicht in:	Aerospace science and technology 2015-06, Vol.43, p.89-95
Hauptverfasser:	Scarselli, G., Castorini, E., Panella, F.W., Nobile, R., Maffezzoli, A.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft components Bolted joints Cyclic loads Damping modelling Fatigue (materials) Fatigue of composite laminates Hysteresis Laminates Phase (cyclic) Slack behaviour Stress-strain relationships
Online-Zugang:	Volltext
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