Fatigue Crack Propagation in Adhesively Bonded Joints

M.M. Abdel Wahab; Ian A. Ashcroft; A.D. Crocombe; P.A. Smith

doi:10.4028/www.scientific.net/KEM.251-252.229

Paper Titles

The Influence of Size Effects on the Fatigue Behaviour of the Aluminium Alloy AIMgSi0.7
p.203

A New Three-Dimensional Fracture Criterion
p.209

Scattering of SH Waves by an Arc-Shaped Crack between a Cylindrical Piezoelectric Inclusion and the Matrix: Near Fields
p.215

Effect of Material Non-Linearity of Adherents on the Behaviour of Interface Cracks
p.221

Fatigue Crack Propagation in Adhesively Bonded Joints
p.229

Effect of Strength of Mismatch Interface on Crack Driving Force
p.235

BEM Analysis of Damaged Superplastic Formed / Diffusion Bonded Structures
p.245

2D- and 3D-Mixed Mode Fracture Criteria
p.251

Approximate Formula for Estimating Stress Concentration Factors for V-Notched Cylindrical Specimens
p.261

HomeKey Engineering MaterialsKey Engineering Materials Vols. 251-252Fatigue Crack Propagation in Adhesively Bonded...

Fatigue Crack Propagation in Adhesively Bonded Joints

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Periodical:

Key Engineering Materials (Volumes 251-252)

Pages:

229-234

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.251-252.229

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Online since:

October 2003

Authors:

M.M. Abdel Wahab, Ian A. Ashcroft, A.D. Crocombe, P.A. Smith

Keywords:

Adhesively Bonded Joint, Composite, Fatigue Crack Propagation

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References

[1] R. Adams and W. Wake, Structural Adhesive Joints in Engineering (Elsevier, 1984).

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[2] M.M. Abdel Wahab, I. A. Ashcroft, A.D. Crocombe and P.A. Smith, International Journal of Fatigue, Vol. 24(6) (2002), pp.705-709.

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[3] M.M. Abdel Wahab, Journal of Adhesion Science and Technology, Vol. 14(6) (2002), pp.851-866.

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[4] C.T. Sun and C.J. Jih, Engineering Fracture Mechanics, Vol. 28(1) (1987), pp.13-20.

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[5] A.D. Crocombe, C.Y. Ong, C.M. Chan, M.M. Abdel Wahab and I.A. Ashcroft, Journal of Adhesion, Vol. 78(9) (2002), pp.745-778.

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[4] 4. 5 3 3. 5 4 4. 5 5 5. 5 6 6. 5 log cycles to failure Maximum load (kN) Experimental (no fillet) Experimental (fillet) nGI nGT.

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[2] [4] [6] [8] [10] [12] 143. 5 4 4. 5 5 5. 5 6 6. 5 log cycles to failure Maximum load (kN) Experimental nGI nGT.

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