The influence of the constituent properties on the residual strength of glare

Applied Composite Materials

Volumn 8, Issue 4, 2001, Pages 263-277

  De Vries, T J ^a   Vlot, A ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; ALUMINUM ALLOYS; FRACTURE; GLASS FIBERS; STIFFNESS; STRAIN; STRENGTH OF MATERIALS;

CONSTITUENT PROPERTIES; FIBRE METAL LAMINATE GLARE; RESIDUAL STRENGTH;

LAMINATED COMPOSITES;

EID: 0034926712     PISSN: 0929189X     EISSN: None     Source Type: Journal    
DOI: 10.1023/A:1011256202539     Document Type: Article

References (9)

1. Towards application of fibre metal laminates in large aircraft
2. Influences of metal layer properties on the residual strength of glare
3. The application of Fx-fiber in fiber metal laminate
4. Towards Fx FML
5. Test procedures for fiber metal laminates
6. The application of the R-curve concept for the prediction of the residual strength of fiber metal laminates