Finite Element Modeling of Fatigue in Fiber–Metal Laminates

Innovative hybrid materials developed at Delft University of Technology (e.g., ARALL and GLARE) dramatically reduce life-cycle costs and offer a great opportunity for service life extension of legacy aircraft. Replacement or repair of damaged aircraft components requires high-strength composite mate...

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Veröffentlicht in:	AIAA journal 2015-08, Vol.53 (8), p.2228-2236
Hauptverfasser:	Woelke, Pawel B, Rutner, Marcus P, Shields, Michael D, Rans, Calvin, Alderliesten, René
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft Aircraft components Aluminum Calibration Cohesion Composite materials Computer simulation Configurations Crack propagation Exact solutions Fatigue failure Fatigue life Fatigue tests Fiber-metal laminates Finite element method Fracture mechanics Hybrid structures Impact damage Impact resistance Laminates Life cycle costs Life extension Mathematical models Metal fatigue Methodology Service life Simulation Strain energy release rate Stress concentration
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