The energy release rate in the general delamination problem of anisotropic laminates under thermomechanical loads

Journal of Applied Mechanics, Transactions ASME

Volumn 65, Issue 1, 1998, Pages 85-92

  Yin, Wan Lee ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0040011306     PISSN: 00218936     EISSN: 15289036     Source Type: Journal    
DOI: 10.1115/1.2789051     Document Type: Article

References (20)

1. Chai, H., Babcock, C. D., and Knauss, W. G., 1981, “One-dimensional modeling of failure in laminated plates by de lamination buckling,”Int. J. Solids Struc., Vol. 17, pp. 1069-1083.
2. Chen, H. P., 1991, “Shear deformation theory for compressive de lamination buckling and growth,”AIAA J., Vol. 29, pp. 813-819.
3. Davidson, B. D., 1994, “Energy release rate determination for edge de lamination under combined in-plane, bending and hydrothermal loading. Part I-De lamination at a single interface,”J. Composite Materials, Vol. 28, pp. 1009-1031.
4. Jane, K. C., 1989, “Buckling, Post buckling Deformation and Vibration of a Delaminated Plate,” Ph.D. dissertation, Georgia Institute of Technology, Atlanta, GA.
5. Jane, K. C., and Yin, W.-L., 1992, “Refined buckling and pos tbuckling analysis of two-dimensional de laminations-II. Results for anisotropic laminates and conclusion,”Int. J. Solids Struc., Vol. 29, pp. 611-639.
6. Kachanov, L. M. 1976, “Separation failure of composite materials,”Poly. Meek, Vol. 12, pp. 811-815.
7. Kardomateas, G. A., and Schmueser, D. W., 1988, “Buckling and post buckling of delaminated composites under compressive loads including transverse shear effects,”AIAA J., Vol. 26, pp. 337-343.
8. O’Brien, T. K., 1984, “Mixed-mode strain-energy-release-rate effects on edge de lamination of composites,”Effects of Defects in Composite Materials, ASTM STP 836, American Society for Testing of Materials, Philadelphia, PA, pp. 125-142.
9. Storakers, B., and Anderson, B., 1988, “Nonlinear plate theory applied to de lamination in composites,”J. Mech. Phys. Solids, Vol. 36, pp. 689-718.
10. Nilsson, K.-F., and Storakers, B., 1992, “On Interface Crack Growth in Composite Plates,” ASMEJournal of Applied Mechanics, Vol. 59, pp. 530-538.
11. Yin, W.-L., 1985, “Ax symmetric buckling and growth of a circular de lamination in a compressed laminate,”Int. J. Solids Struc., Vol. 21, pp. 503-514.
12. Yin, W.-L., 1986, “Cylindrical buckling of laminated and delaminated plates,”Proc. AIAA/ASME/ASCE/AHS 27th SDM Conference, San Antonio, TX, pp. 165-179.
13. Yin, W.-L., 1993, “Thermal stresses in anisotropic multilayered structures,”Thermal Stress and Strain in Microelectronics Packaging, J. H. Lau, ed., van No strand Reinhold, New York, pp. 95-138.
14. Yin, W.-L., 1995, Thermal buckling of composite plates with a strip de lamination,”Proc. AIAA/ASME/ASCE/AHS/ASC 36th SDM Conference, Apr., 10-13, New Orleans, LA, pp. 1389-1397, revised version to appear inInt. J. Solids Struc.
15. Yin, W.-L., 1997, “A general analysis method for singularities in composite structures,”Proc. AIAA/ASME/ASCE/AHS/ASC 38th SDM Conference, Orlando, FL, pp. 2238-2245.
16. Yin, W.-L., and Jane, K. C., 1992, “Refined buckling and post buckling analysisof two-dimensional de laminations-I. Analysis and validation,”Int. J. Solids Struc., Vol. 29, pp. 591-610.
17. Yin, W.-L., and Wang, J. T. S., 1984, “The Energy Release Rate in the Growth of a One-Dimensional De lamination,” ASMEJournal of Applied Mechanics, Vol. 51, pp. 939-941.
18. Yin, W.-L., Sallam, S. N., and Simitses, G. J., 1986, “Ultimate axial load capacity of a delaminated beam-plate,”AIAA J., Vol. 23, pp. 1437-1444.
19. Yin, W.-L., Jane, K.-C., and Lin, C.-C., 1997, “Singular solutions of multi material wedges under thermo mechanical loading,”Analysis and Design Issues for Modern Aerospace Vehicles-1977, G. J. Simitses, ed., ASME, New York, pp. 159-166.
20. Bottega, W. J., 1983, “A growth law for propagation of arbitrary shaped de lamination in layered plates,”Int. J. Solids Struc., Vol. 19, pp. 1009-1017.