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AIMS Materials Science, 2016, 3(4): 1577-1586. doi: 10.3934/matersci.2016.4.1577
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Multiple crack propagation by DBEM in a riveted lap-joint
Department of Industrial Engineering, University of Salerno, Fisciano (SA), Italy
Received: , Accepted: , Published:
References
1. Citarella R (2015) Residual strength evaluation by DBEM for a cracked lap joint. Frattura ed Integrità Strutturale 35: 523–533.
2. Citarella R (2016) Multiple crack propagation by DBEM in a riveted butt-joint: a simplified bidimensional approach. Frattura ed Integrità Strutturale 36: 160–167.
3. Citarella R (2011) MSD Crack propagation on a repaired aeronautic panel by DBEM. Adv Eng Softw 42: 887–901.
4. Citarella R, Cricrì G, Armentani E (2013) Multiple crack propagation with Dual Boundary Element Method in stiffened and reinforced full scale aeronautic panels. Key Eng Mater 560: 129–155.
5. Sepe R, Armentani E, Lascio PD, et al. (2015) Crack Growth Behavior of Welded Stiffened Panel. Procedia Eng 109: 473–483.
6. Silva LFM, Gonçalves JPM, Oliveira FMF, et al. (2000) Multiple-site damage in riveted lap-joints: experimental simulation and finite element prediction. Int J Fatigue 22: 319–338.
7. Citarella R, Carlone P, Sepe R, et al. (2016) DBEM crack propagation in friction stir welded aluminum joints. Adv Eng Softw 101: 50–59.
8. Lamanna G, Sepe R, Pozzi A (2014) Tensile testing of hybrid composite joints. Appl Mech Mater 575: 452–456.
9. Hong HK, Chen JT (1988) Derivations of Integral Equations of Elasticity. ASCE J Eng Mech 114: 1028–1044.
10. Chen JT, Hong HK (1999) Review of dual boundary element methods with emphasis on hypersingular integrals and divergent series. ASME Appl Mech Rev 52: 17–33.
11. Citarella R, Carlone P, Lepore M, et al. (2016) Hybrid technique to assess the fatigue performance of multiple cracked FSW joints. Eng Fract Mech 162: 38–50.
12. C M BEASY Ltd (2011) BEASY V10r14 Documentation.
13. Calì C, Citarella R (2004) Residual strength assessment for a butt joint in MSD condition. Adv Eng Softw 35: 373–382.
14. Citarella R, Cricrì G, Lepore M, et al. (2014) Assessment of Crack Growth from a Cold Worked Hole by Coupled FEM-DBEM Approach. Key Eng Mater 577–578: 669–672.
15. Cavallini G, Lazzeri R (2003) Report on Experimental Fatigue Crack Growth in medium and complex components. ADMIRE project report: ADMIRE-TR-3.0-67-3.1/UP. Dipartimento di Ingegneria Aerospaziale, Università di Pisa.
16. De Castro PMST, De Matos PFP, Moreira PMGP, et al. (2007) An overview on fatigue analysis of aeronautical structural details: open hole, single rivet lap-joint, and lap-joint panel. Mater Sci Eng 468–470: 144–157.
17. Armentani E, Citarella R (2006) DBEM and FEM analysis on non-linear multiple crack propagation in an aeronautic doubler-skin assembly. Int J Fatigue 28: 598–608.
18. Citarella R (2009) Non Linear MSD crack growth by DBEM for a riveted aeronautic reinforcement. Adv Eng Softw 40: 253–259.
19. Rigby RH, Aliabadi MH (1993) Mixed-mode J-integral method for analysis of 3D fracture problems using DBEM. Eng Anal Bound Elem 11: 239–256.
20. Rigby RH, Aliabadi MH (1998) Decomposition of the mixed-mode J-integral—revisited. Int J Solids Struct 35: 2073–2099.
21. Yu DZ (2013) A Numerical Analysis of Riveted Lap Joint Containing Multiple-site Damage. Appl Math Inf Sci 7: 699–704
22. Erdogan F, Sih GC (1963) On the crack extension in plates under plane loading and transverse shear. J Basic Eng 85: 519–527.
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