Analysis of composite laminates with multiple fasteners

International Journal of Solids and Structures

Volumn 35, Issue 15, 1998, Pages 1793-1811

  Madenci, E ^a   Shkarayev, S ^a   Sergeev, B ^a   Oplinger, D W ^b   Shyprykevich, P ^b  

^a University of Arizona   (United States)

^b NONE

Author keywords

[No Author keywords available]

Indexed keywords

BOLTED JOINTS; BOUNDARY CONDITIONS; STRESS INTENSITY FACTORS; STRUCTURAL ANALYSIS;

BOUNDARY COLLOCATION TECHNIQUE; MULTIPLE-FASTENER JOINTS;

LAMINATED COMPOSITES;

EID: 0032064766     PISSN: 00207683     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0020-7683(97)00152-2     Document Type: Article

References (14)

1. Bowie, O. L. (1956) Analysis of an infinite plate containing radial crack originating at the boundary of an internal circular hole. Journal of Mathematics and Physics 35, 60-71.
2. Bowie, O. L. and Neal, D. M. (1970) A modified mapping-collocation technique for accurate calculation of stress intensity factors. International Journal of Fracture Mechanics 6, 199-206.
3. Chiang, Y. J. and Rowlards, R. E. (1991) Finite element analysis of mixed-mode fracture of bolted composite joints. Journal of Composites Technology and Research 13, 227-235.
4. Eriksson, L. I., Backlund, J. and Moller, P. (1995) Design of multiple-row bolted composite joints under general in-plane loading. Composites Engineering 5, 1051-1068.
5. Griffin, O. H., Jr, Hyer, M. W., Cohen, D., Shuart, M. J., Yalamanchili, S. R. and Prasad, C. B. (1994) Analysis of multifastener composite joints. Journal of Spacecraft and Rockets 31, 278-284.
6. Hilton, P. D. and Wilmarth, D. D. (1982) PAPST - revision 2.0; revised documentation and theoretical manual, Report to DTNSRDC.
7. Hyer, M. W. and Liu, D. (1984) Stresses in pin-loaded plates: photoelastic results. Journal of Composite Materials 19, 138-153.
8. Lekhnitskii, S. G. (1968) Anisotropic Plates. Gordon and Breach Science Publishers, New York.
9. Madenci, E., Shkarayev, S. and Sergeev, B. (1996) Analysis of composite joints with multiple fasteners. Final Report to Federal Aviation Administration, Contract no. 94-G-029, The University of Arizona, Tucson.
10. Oplinger, D. W. (1978) On the structural behavior of mechanically fastened joints in composite structures. Proceedings of a Conference on Fibrous Composites in Structural Design, San Diego, California, pp. 575-602.
11. Oplinger, D. W. and Gandhi, K. R. (1974) Stresses in mechanically fastened orthotropic laminates. Proceedings of the Second Conference on Fibrous Composites in Flight Vehicle Design, Dayton, Ohio, pp. 813-841.
12. Rowlands, R. E., Rahman, T. L., Wilkinson, T. L. and Chang, Y. I. (1982) Single-and multiple-bolted joints in orthotropic materials. Composites 13, 273-279.
13. Sih, G. C., Paris, P. C. and Irwin, G. R. (1965) On cracks in rectilinearly anisotropic bodies. International Journal of Fracture Mechanics 1, 189-203.
14. Xiong, Y. and Poon, C. (1994) A design model for composite joints with multiple fasteners. Aeronautical Note IAR-AN080, National Research Council, Canada, NRC no. 32165.