Failure load evaluation and prediction of hybrid composite double lap joints

Composite Structures

Volumn 92, Issue 12, 2010, Pages 2916-2926

  Lee, Young Hwan ^a   Lim, Do Wan ^b   Choi, Jin Ho ^b   Kweon, Jin Hwe ^b   Yoon, Myung Keun ^c  

^a Hanyang University   (South Korea)

^b Gyeongsang National University   (South Korea)

^c South Dakota School of Mines Technology   (United States)

Author keywords

Damage zone theory; Failure Area Index (FAI); Hybrid composite joint

Indexed keywords

ADHESIVE BONDING; AREA INDEX; DAMAGE ZONES; DOUBLE LAP JOINT; FAILURE LOAD; HYBRID COMPOSITES; HYBRID JOINTS; JOINT TYPE; MECHANICAL FASTENING; MECHANICAL JOINTS; THEORETICAL PREDICTION;

ADHESIVE JOINTS;

ADHESION; BONDING; COMPOSITE; DAMAGE; FAILURE ANALYSIS; STRENGTH;

EID: 77954142393     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2010.05.002     Document Type: Article

References (22)

1. Mallick P.K. Fiber-reinforced composite 1988, Marcel Dekker Inc., p. 418.
2. Choi J.H., Lee D.G. An experimental study of the static torque capacity of the adhesively-bonded tubular single lap joint. J Adhes 1996, 55:245-260.
3. Adams R.D., Peppiatt N.A. Stress analysis of adhesive bonded tubular lap joints. J Adhes 1977, 9:1-18.
4. Kim K.S., Yoo J.S., Yi Y.M., Kim C.G. Failure mode and strength of uni-directional composite single lap bonded joints with different bonding methods. Compos Struct 2006, 72:477-485.
5. Owens James F.P., Lee-Sullivan Pearl Stiffness behaviour due to fracture in adhesively bonded composite-to-aluminum joints. I. Theoretical model. Int J Adhes Adhes 2000, 20:39-45.
6. Owens James F.P., Lee-Sullivan Pearl Stiffness behaviour due to fracture in adhesively bonded composite-to-aluminum joints. II. Experimental. Int J Adhes Adhes 2000, 20:47-58.
7. Choi J.H., Lee D.G. The torque transmission capabilities of the adhesively-bonded tubular single lap joint and the double lap joint. J Adhes 1994, 44:197-212.
8. Hart-Smith L.J. Designing to minimize peel stresses in adhesive bonded joints. Delamination and debonding of materials 1985, 238-266. ASTM STP 876. W.S. Johnson (Ed.).
9. Groth H.L. A method to predict fracture in an adhesively bonded joint. Int J Adhes Adhes 1985, 5:19-22.
10. Sheppard A., Kelly D., Tong L. A damage zone model for the failure analysis of adhesively bonded joints. Int J Adhes Adhes 1998, 18:385-400.
11. Ban C.S., Lee Y.H., Choi J.H., Kweon J.H. Strength prediction of adhesive joints using the modified damage zone theory. Compos Struct 2008, 86:96-100.
12. Hart-Smith L.J. Mechanically fastened joints for advanced composites, phenomenological considerations and simple analysis. Fibrous composite in structural design 1980, Plenum Press, p. 543-74.
13. Ireman T. Three-dimensional stress analysis of bolted single-lap composite joints. Compos Struct 1998, 43:195-216.
14. Whitney J.M., Nuismer R.J. Stress fracture criteria for laminated composites containing stress concentrations. J Compos Mater 1974, 8:253-265.
15. Whitney J.M., Nuismer R.J. Uniaxial failure of composite laminated containing stress concentrations. Fracture mechanics of composites 1975, ASTM STP 593, p. 117-42.
16. Chang F.K., Scott R.A. Strength of mechanically fastened composite joints. J Compos Mater 1982, 16:470-494.
17. Chang F.K., Scott R.A. Failure of composite laminates containing pin loaded holes-method of solution. J Compos Mater 1984, 18:255-278.
18. Choi J.H., Chun Y.J. Failure load prediction of mechanically fastened composite joint. J Compos Mater 2003, 37(24):2163-2177.
19. Ryu C.O., Choi J.H., Kweon J.H. Failure load prediction of composite joints using linear analysis. J Compos Mater 2007, 41(7):865-878.
20. Hart-Smith L.J. Design methodology for boned-bolted composite joint. Technical Report AFWAL-TR-81-3154 1982, Douglas Aircraft Company.
21. Fu M., Mallick P.K. Fatigue of hybrid (adhesive/bolted) joints in SRIM. Int J Adhes Adhes 2001, 21:145-159.
22. Kelly G. Load transfer in hybrid (bonded/bolted) composite single-lap joints. J Compos Struct 2005, 69(1):35-43.