Fatigue crack initiation in fibre-metal laminate GLARE 2

Materials Science and Engineering: A

Volumn 234-236, Issue , 1997, Pages 621-624

  Vasek A ^a   Polak J ^a   Kozak V ^a  

^a INSTITUTE OF PHYSICS OF MATERIALS   (Czech Republic)

Author keywords

Fatigue crack initiation; Finite element calculations; GLARE 2

Indexed keywords

COMPUTATIONAL METHODS; CRACK INITIATION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; LOAD TESTING; OPTICAL MICROSCOPY; SCANNING ELECTRON MICROSCOPY; STRAIN; STRESS ANALYSIS;

FIBER METAL LAMINATE GLARE 2;

LAMINATED COMPOSITES;

FATIGUE CRACK; FIBER; LAMINATED MATERIAL; METAL;

EID: 0031205635     PISSN: 09215093     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0921-5093(97)00294-3     Document Type: Article

References (6)

1. L.B. Vogelesang, J.W. Gunning, Mater. Design 7 (1986) 287-300.
2. A. Beukers et al. (Eds.), Fatigue of Aircraft Materials, Delft University Press, Delft, 1992.
3. R.O. Ritchie, Mat. Sci. Eng. A103 (1988) 15-28.
4. M. Papakyriacou et al., in K.H. Schwalbe and C. Berger (eds.), ECF10 - Structural Integrity: Experiments, Models and Applications, Berlin 1994, Engineering Materials Advisory Services, Warley, Vol. II (1994) 1193-1199.
5. A. Vašek, L.B. Vogelesang, in U. Meier (ed.), SAMPE Europe -Success of Materials by Combination, Basel, 1996, SAMPE Europe, Niederglatt/ZH, (1996) 437-449.
6. A. Vašek et al., in J. Petit (ed.), ECF11 - Mechanism and Mechanics of Damage and Failure, Poitiers 1996, Engineering Materials Advisory Services, Warley, (1996) 1685-1690.