Effects of constitutive parameters on the accuracy of measured fracture energy using the DCB-specimen

Engineering Fracture Mechanics

Volumn 75, Issue 10, 2008, Pages 2968-2983

  Biel, A ^a   Stigh, U ^a  

^a UNIVERSITY OF SKÖVDE   (Sweden)

Author keywords

Adhesive; DCB specimen; Fracture energy; Test standards; Toughness testing

Indexed keywords

ADHESIVE JOINTS; CANTILEVER BEAMS; COMPUTER SIMULATION; CONSTITUTIVE EQUATIONS; CONVERGENCE OF NUMERICAL METHODS; FRACTURE MECHANICS;

EXACT SOLUTION; LINEAR ELASTIC FRACTURE MECHANICS;

FRACTURE ENERGY;

ADHESIVE JOINTS; CANTILEVER BEAMS; COMPUTER SIMULATION; CONSTITUTIVE EQUATIONS; CONVERGENCE OF NUMERICAL METHODS; FRACTURE ENERGY; FRACTURE MECHANICS;

EID: 40849083441     PISSN: 00137944     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfracmech.2008.01.002     Document Type: Article

References (23)

1. Irwin G.R., and Kies J.A. Critical energy rate analysis of fracture strength. Weld J, Weld Res Suppl 33 (1954) 193-198
2. Berry J.P. Determination of fracture surface energies by the cleavage technique. J Appl Phys 34 (1963) 62-68
3. Mostovoy S., Crosley P.B., and Ripling E.J. Use of crack-line-loaded specimens for measuring plane-strain fracture toughness. J Mater 2 (1967) 661-668
4. ASTM D 3433. Fracture strength in cleavage of adhesives in bonded joints. Philadelphia, USA: American Society for Testing and Materials; 1999.
5. IC of structure adhesives using the double cantilever beam (DCB) and tapered double cantilever beam (TDCB) specimens. London, Great Britain: British Standard Institution; 2001.
6. IC, of structural adhesive joints: the results of an international round-robin. Int J Adhes Adhes 23 (2003) 293-305
7. Tamuzs V., Tarasovs S., and Vilks U. Delamination properties of translaminar-reinforced composites. Compos Sci Technol. 63 (2003) 1423-1431
8. Biel A., and Stigh U. An analysis of the evaluation of the fracture energy using the DCB-specimen. Arch Mech 59 (2007) 311-327
9. Andersson T., and Stigh U. The stress-elongation relation for an adhesive layer loaded in modus I using equilibrium of energetic forces. Int J Solid Struct 41 (2004) 413-434
10. Andersson T., and Biel A. On the effective constitutive properties of a thin adhesive layer loaded in peel. Int J Fracture 141 (2006) 227-246
11. Olsson P., and Stigh U. On the determination of the constitutive properties of the interphase layers - an exact solution. Int J Fracture 41 (1989) R71-R76
12. Paris A.J., and Paris P.C. Instantaneous evaluation of J and C*. Int J Fracture 38 (1988) R19-R21
13. Rice J.R. A path independent integral and the approximation analysis of the concentration by notches and cracks. J Appl Mech 35 (1968) 379-386
14. Stigh U., and Andersson T. An experimental method to determine the complete stress-elongation relation for a structural adhesive layer loaded in peel. In: Williams J.G., and Pavan A. (Eds). Fracture of polymers. Composites and adhesives vol. 27 (2000), ESIS Publication 297-306
15. Schmidt P. Computational models of adhesively bonded joints. PhD thesis, Linköping University, Institute of Technology, Linköping, Sweden; 2007.
16. ASTM D 3762. Standard test method for adhesive-bonded surface durability of aluminum (wedge test). Philadelphia, USA: American Society for Testing and Materials; 1998.
17. Williams J.G. The fracture mechanics of delamination tests. J Strain Anal 24 4 (1989) 207-214
18. Tada H., Paris P.C., and Irwin G.R. The stress analysis of cracks handbook (2000), ASME Press, New York
19. Eshelby J.D. The force on an elastic singularity. Philos Trans R Soc Lond A244 (1951) 87-112
20. Nilsson F. Large displacement aspects on fracture testing with double cantilever beam specimens. Int J Fracture 139 (2006) 305-311
21. Stigh U. Damage and crack growth analysis of the double cantilever beam specimen. Int J Fracture 37 (1988) R13-R18
22. Kinloch A.J. Adhesion and adhesives, science and technology (1987), Chapman and Hall, London
23. Sargent J.P. Durability studies for aerospace applications using modus I and wedge tests. Int J Adhes Adhes 25 (2005) 247-256