Studies in the matrix dominated failures of composite joints

Composite Structures

Volumn 44, Issue 1, 1999, Pages 1-16

  Jones, R ^a   Sawyer, J P G ^a   Chiu, W K ^a  

^a MONASH UNIVERSITY   (Australia)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; FAILURE ANALYSIS; JOINTS (STRUCTURAL COMPONENTS); STIFFNESS; STRUCTURAL ANALYSIS;

DAMAGE TOLERANCE; IN-PLANE LOADING;

COMPOSITE STRUCTURES;

COMPOSITE; DAMAGE; FIBER REINFORCED COMPOSITE; MATHEMATICAL ANALYSIS;

EID: 0033006894     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0263-8223(98)00107-X     Document Type: Article

References (26)

1. [1] Composite Aircraft Structure, Federal Aviation Administration Advisory Circular, 20-107A, 1984.
2. [2] Damage Tolerance and Fatigue Evaluation of Structure, Federal Aviation Administration Advisory Circular, 25.571-1A, 1986.
3. [3] Molent L, Callinan RJ, Jones R, Design of an all boron epoxy doubler for the F-111C wing pivot fitting: structural aspects, Journal of Composite Structures 1989;11:57-83.
4. [4] Jones R, Chiu WK, Smith R. Airworthiness of composite repairs, Engineering Failure Analysis 1995;2:117-128.
5. [5] Gates S. Matrix dominated stress/strain behavior in polymeric composites: effect of hold time, non-linearities and rate dependent stress-strain behavior of advanced polymer matrix composites. NASA Technical Memorandum 104070, 1991.
6. [6] Wang J, Kelly D. Strength and failure modes of adhesively bonded joints at different loading rates. Co-operative Research Centre for Advanced Composite Structures, CRC-ACA EP 97013, Melbourne, Australia, also published in Journal of Adhesion (in press).
7. [7] van Blaricum TJ, Bates B, Jones R. An experimental investigation into the effect of impact damage on the compressive strength of step lap joints, Journal of Engineering Fracture Mechanics 1989;32:667-674.
8. [8] Wang SS, Srinivasan S, Hu HT, Halaji R. Visco-elastic and non-linear adherend effects in bonded composite joints, Journal of Composite Structures 1995;33:7-16.
9. [9] Chiu WK, Chalkley PD, Jones R. Effects of temperature on the shear stress-strain behaviour of structural adhesives (FM73), Journal of Computers and Structures 1994;53:483-489.
10. [10] Chiu WK, Galea SC, Jones R. The role of material non-linearities in composite structures. Time dependent response of carbon fibre/ epoxy composites, Journal of Composite Structures 1997;38:71-81.
11. [11] Gates S. Rate dependent stress-strain behaviour of advanced polymer matrix composites. NASA Technical Memorandum 104070, 1991.
12. [12] Jones R, Alesi H, Chiu WK, Galea S. A preliminary study into the matrix dominated non-linear behaviour of graphite epoxy laminates, Journal of Composite Structures 1995;30:193-199.
13. [13] Hart-Smith LJ. Adhesively bonded double lap joints, NASA Langley Research Center Report NASA CR-112235, January 1973.
14. [14] Jones R, Trippit B, Chiu WK, Tomas J. Lap joint theory revisited, Journal of Polymers and Polymer Composites 1995;3:11-19.
15. [15] Chiu WK, Jones R. The role of rate effects in adhesives and graphite epoxy in structural design, Journal of Polymers and Polymer Composites 1996;4:1-12.
16. [16] Glinka G. Energy density approach to calculation of inelastic stress-strain near notches and cracks, Engineering Fracture Mechanics 1985;22:485-508.
17. [17] Chao M, Chiu WK, Jones R, Wang J, Kelly D. The analysis of bonded lap joints. In: Proceedings ICCM-11, 14-18 July 1997, Scott ML, editor. Melbourne, Australian Composite Society, 1997:119-127.
18. [18] Mignery LA, Schapery RA. Visco-elastic and non-linear adherend effects in bonded composite joints, Journal of Adhesion 1991; 343:17-40.
19. [19] Alesi H, Nguyen VM, Jones R, Mileshkin N, Kelly D. Postbuckling failure analysis of carbon/epoxy compression panel. In: Proceedings ICCM-11, 14-18 July 1997, Scott ML, editor. Melbourne, Australian Composite Society, 1997:707-722.
20. [20] Sawyer JPG. Modelling the inelastic behaviour of paper structures. PhD thesis, Monash University, Melbourne, 1997.
21. [21] Jones RM. Mechanics of composite materials, New York: McGraw-Hill, 1995:339-342.
22. [22] Alesi H. Postbuckling analysis of 3D composite structures. PhD thesis, Royal Melbourne Institute of Technology, 1996:121-153.
23. [23] Ramaswamy VG, Stouffer DC, Laflen JH. A constitutive model for the inelastic multi-axial response of René 80 at 871°C and 982°C, Journal of Engineering and Materials Technology, ASME 1990;112:281-286.
24. [24] Gates TS. Effect of elevated temperature on the visco-plastic modelling of graphite/polymeric composites, ASTM STP 1174, Harris CE, Gates TS, editors, 1993:201-221.
25. [25] Weeks CA, Sun CT. Non-linear rate dependent response of thick section composite laminates. In: High Strain Rate Effects on Polymeric, Metal and Ceramic Matrix Composites and Other Advanced Materials, Rajapaske DS, Vinson JR, editors. ASME, 1995;48:81-95.
26. [26] Kaye RH, Jones R, Hayes P. Orion P3C horizontal stabiliser strain survey and corrosion repair development. Defence Science and Technology Technical Report, DSTO-TR-0196, November 1995. Composite Structures 44 (1999) 17-29