A simple method for computing the stress intensity factors for cracks at notches

Engineering Failure Analysis

Volumn 9, Issue 6, 2002, Pages 683-702

  Jones, R ^a   Peng, D ^a  

^a MONASH UNIVERSITY   (Australia)

Author keywords

Airworthiness; Cracks; Notches; Repairs; Stress intensity factors

Indexed keywords

COMPUTATIONAL METHODS; CRACKS; LOADS (FORCES);

NOTCHES;

STRESS INTENSITY FACTORS;

CRACK; LOADING; STRESS;

EID: 0036900013     PISSN: 13506307     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1350-6307(02)00007-9     Document Type: Article

References (29)

1. A methodology for structural optimisation with damage tolerance constraints
2. Computational schemes for integrity analyses of fuselage panels in aging airplanes
3. Analytical solution for embedded elliptical cracks, and finite element alternating method for elliptical surface cracks, subject to arbitrary loadings
4. Composite repairs to cracked holes under bi-axial loading
5. Fatigue cracks at notches
6. The stress intensity factor of small cracks at notches
7. Estimation of stress intensity factors for small cracks at notches
8. Stress intensity factors of small cracks at notches
9. Asymptotic approximations to crack problems
10. The distribution of stress near the tip of a radial crack at the edge of a circular hole
11. Practical stress expressions for stress concentration regions
12. The infinite sheet with cracked hole under inclined tension or in plane shear
13. The stress intensity factor of a radial crack at the edge of a circular hole under shear loading
14. Bonded composite repair of fatigue cracked primary aircraft structure
15. Composite repair to rib stiffened panels
16. Design of an all boron epoxy doubler for the F-111C wing pivot fitting: Structural aspects
17. Bonded-composite repair of representative multi-site damage in a full-scale fatigue-test article
18. An application of the inclusion analogy for bonded reinforcement
19. A cracked plate repaired by bonded reinforcements
20. A crack bridging model for bonded plates subjected to tension and bending
21. Repair of Mirage iii aircraft using BFRP crack patching technology
22. Uniaxial failure of composite laminates containing stress concentrations
23. Bonded repairs to rib stiffened wing skins
24. Studies in multi-site damage of fuselage lap joints
25. Fatigue cracking in the upper wing pivot fittings in F-111 aircraft