Delamination behavior of spliced Fiber Metal Laminates. Part 2. Numerical investigation

Composite Structures

Volumn 46, Issue 2, 1999, Pages 147-162

  Hashagen, F ^a   De Borst, R ^a   De Vries, T ^a  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

Author keywords

Delamination behavior; Fiber Metal Laminates; Splicing

Indexed keywords

ALUMINUM; DEFORMATION; DELAMINATION; FRACTURE TOUGHNESS; GLASS FIBERS; INTERFACES (MATERIALS); MATHEMATICAL MODELS; PLASTICITY; STRENGTH OF MATERIALS; STRESSES;

FIBER METAL LAMINATES; GLASS FIBER REINFORCED PREPREG LAYERS; HOFFMAN LIKE YIELD FUNCTION; INELASTIC DEFORMATION; INTERFACE ELEMENTS; SOLID LIKE SHELL ELEMENTS; VON MISSES YIELD CRITERION;

FIBER REINFORCED METALS;

ALUMINUM FIBER; DELAMINATION; FIBER REINFORCED COMPOSITE; LAMINATE; METAL FIBER; SPLICING;

EID: 0032824650     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(99)00050-1     Document Type: Article

References (22)

1. Lange R. The AIRBUS AXX, A presentation to the Nederlandse Vereniging voor Luchtvaarttechniek, Hand-out, Delft, 1997.
2. Vries T. de, Vlot A, Hashagen F. Delamination behavior of spliced Fiber Metal Laminates. Part 1. Experimental results. Comp Struct 1999;46:131-145.
3. Parisch H. A continuum based shell theory for nonlinear applications. Int J Numer Meth Engng 1995;38(11):1855-83.
4. Hashagen F, Schellekens JCJ, Borst R. de, Parisch H. Finite Element Procedures for Modelling Fiber Metal Laminates. Comp Struct 1995;32:255-64.
5. Schellekens JCJ, de Borst R. On the integration of interface elements. Int J Numer Meth Engng 1993;36:43-66.
6. Corigliano A. Formulation, identification and use of interface models in numerical analysis of composite delamination. Int J Solids and Struct 1993;30(20):2779-811.
7. Allix O, Ladevéze P. Interlaminar interface modelling for the prediction of delamination. Comp Struct 1992;22:235-42.
8. Allix O. Identification and validation of an interface damage model for delamination prediction. In: Owen DRJ, Õnate E, Hinton E. editors. Proceedings of Computer Plast, COMPLAS/5. 1997:1139-47.
9. König M, Krüger R. Computation of energy release rates: a tool for predicting delamination growth in carbon fiber reinforced epoxy laminates. In: Owen DRJ, Õnate E, Hinton E. editors. Proceedings of Computer Plast. COMPLAS/4. 1995:1167-78.
10. Schellekens JCJ, de Borst R. Free edge delamination in carbon-epoxy laminates: A novel numerical/experimental approach. Comp Struct 1994;28:357-73.
11. Rybicki EF, Kanninen MF. A finite element calculation of stress intensity factors by a modified crack closure integral. Eng Fract Mech 1977;9:931-38.
12. Bathe K-J. Finite Element Procedures in Engineering Analysis, Englewood Cliffs, NJ: Prentice-Hall, 1982.
13. de Borst R, Feenstra PH. Studies in anisotropic plasticity with reference to the hill criterion. Int J Numer Meth Engng 1990;29:315-36.
14. Simo JC, Taylor RL. Consistent tangent operators for rate-independent elasto-plasticity. Comp Meth Appl Mech Engng 1985;48:101-18.
15. Groen AE. Three-dimensional elasto-plastic analysis of solids. Dissertation TU Delft, Delft University of Technology, 1997.
16. Allix O, Ladevéze P. Corigliano A. damage analysis of interlaminar fracture specimens, Comp Struct 1995;31:61-74.
17. Feenstra PH, Schellekens JCJ. Self-adaptive solution algorithm for a constrained Newton-Raphson method. TU-Delft Report nr.: 25-2-91-2-13, Delft University of Technology, 1991.
18. Hitchings D, Robinson P, Javidrad F. A finite element model for delamination propagation in composites. Comput and Structures 1996;60:1093-104.
19. Structural Laminates Company - Customer Data Sheet, No.: 2,200, Delft, 1994.
20. de Vries T. Various parameters concerning the residual strength of aircraft materials, Part II, Test data and charts. Graduation Thesis, Delft University of Technology, 1993.
21. ASTM - Standard test method for strength properties of adhesives in shear by tension loading of laminated assemblies, ASTM D3165-73, Annual book of ASTM Standards, 1979.
22. ASTM - Standard test method for strength properties of double lap shear adhesive joints by tension loading, ASTM D3528-76, Annual book of ASTM Standards, 1981.