Development of fibre metal laminates for advanced aerospace structures

Journal of Materials Processing Technology

Volumn 103, Issue 1, 2000, Pages 1-5

  Vogelesang, L B ^a   Vlot, A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; CORROSION RESISTANCE; COST EFFECTIVENESS; FATIGUE OF MATERIALS; FLAME RESISTANCE; FUSELAGES; IMPACT RESISTANCE; LAMINATED COMPOSITES; STRENGTH OF MATERIALS;

DAMAGE TOLERANCE; FIBRE METAL LAMINATES; WEIGHT REDUCTION;

FIBER REINFORCED METALS;

EID: 0033742467     PISSN: 09240136     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0924-0136(00)00411-8     Document Type: Article

References (2)

1. L.B. Vogelesang, J.W. Gunnink, G.H.J.J. Roebroeks, R.P.G. Müller, Toward the supportable and durable aircraft fuselage structure, in: J.M. Grandage, G.S. Jost (Eds.), Proceedings of the 18th Symposium of the International Committee on Aeronautical Fatigue, Melbourne, Australia, 3-5 May, 1995, pp. 257-272.
2. L.B. Vogelesang, J. Schijve, Fibre metal laminates: damage tolerant aerospace materials, in: Case Studies in Manufacturing with Advanced Materials, Vol. 2, pp. 259-260, 1995, Elsevier, ISBN: 0-444-88934-5.