Development of fibre metal laminates: Concurrent multi-scale modeling and testing

Journal of Materials Science

Volumn 41, Issue 20, 2006, Pages 6777-6788

  Sinke, J ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; ANISOTROPY; EPOXY RESINS; FIBER REINFORCED MATERIALS; FRACTURE MECHANICS; GLASS FIBERS; MATHEMATICAL MODELS; RESEARCH AND DEVELOPMENT MANAGEMENT;

ARAMID FIBRES; CRACK BRIDGING EFFECT; FIBRE METAL LAMINATES (FML); FRACTURE ENERGY; MULTI-SCALE MODELING;

LAMINATES;

EID: 33845677638     PISSN: 00222461     EISSN: 15734803     Source Type: Journal    
DOI: 10.1007/s10853-006-0206-5     Document Type: Article

References (11)

1. Vlot A, Glare (2001) History of the development of a new aircraft material. Kluwer Academic Publishers, The Netherlands
2. Alderliesten RC (1998) Development of an empirical crack growth model for Fibre Metal Laminates. Preliminary MSc Thesis, Delft University of Technology
3. Vermeulen B, van Tooren MJL, Peeters LJB (September 2005) Knowledge-based design method for fibre metal laminate fuselage panels. Int DETC conference, Long Beach, CA, USA
4. Alderliesten RC (2005) Fatigue crack propagation and delamination growth in glare. PhD Thesis, The Netherlands
5. Suiker ASJ, Fleck NA (2004) J Fatigue 125:1
6. de Jong TJ (2004) Forming of Laminates. PhD Thesis, The Netherlands
7. Hagenbeek M (2005) Characterization of FML under thermomechanical loadings, PhD thesis, The Netherlands
8. van Rooijen RGJ (2006) Bearing strength characteristics of standard and steel reinforced GLARE,PhD thesis, The Netherlands
9. Roebroeks GHJJ (2000) The metal volume fraction approach, TD-R-00-003. SLI, Delft
10. DIALFAST (2004) Development of innovative and advanced laminates for future aircraft structures. CEC 6th Framework Program, Specific, Targeted, Research Project, No, 502846
11. Middendorf P, Linde P, de Boer H, Sinke J (2005) Micromechanical modelling approach for Fibre Metal Laminates. NAFEMS Conference