This paper studies the matrix cracking sequence in [02/90 2]s graphite epoxy laminates that contain a small central hole. Experiment was performed first using specimens loaded in uniaxial, quasi-static tension, followed by inspections of the speci men at several prescribed loading increments by means of x-radiography. The inspection provides a quantitative measurement and a physical analysis of matrix cracking patterns near the hole.
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References
1.
Wang, A S. D. and F.W. Crossman "Initiation and Growth of Transverse Cracks and Edge Delamination in Composite Laminates, Part 1, An Energy Method ," J Composite Materials, 14:71-87 (1980)
2.
Crossman, F.W. , W.J. Warren, A. S D Wang and G.E. Law "Initiation and Growth of Transverse Cracks and Edge Delamination in Composite Laminates, Part 2, Experimental Correlation," J. Composite Materials, 1488-106 (1980).
3.
Wang, A S. D , N.N. Kishore and C.A. Li "Crack Development in Graphite-Epoxy Cross-Ply Laminates under Uniaxial Tension," Composites Science and Technology, 241-31 (1985)
4.
Wang, A. S. D , E.S. Reddy and Y. Zhong "Three Dimensional Simulation of Crack Growth in Notched Laminates ," Joint Symposium on Composite Materials Science and Engineering, American Society for Composites—University of Delaware Center for Composite Materials, September 23-25, University of Delaware, Newark, DE (1987)
5.
Rybicki, E.F. and D.W. Schmueser "Effect of Stacking Sequence and Lay-Up Angle on Free Edge Stresses around a Hole in a Laminated Plate under Tension ," J Composite Materials, 12300-313 (1978)
6.
Daniel, I.M. , R.E. Rowlands and J.B. Whiteside "Effects of Materials and Stacking Sequence on the Behavior of Composite Plates with Holes ," Experimental Mechanics, 141-9 (1974)
7.
O'Brien, T.K. and I.S. Raju. "Strain Energy Release Rate Analysis of Delamination around an Open Hole in Composite Laminates," Paper No. AIAA-84-0961, AIAA/ASME/ASCE/AHS 25th Structures, Structural Dynamics and Materials Conference, May 14-16, Palm Springs, CA (1984).
8.
Raju, I.S. and J.H. Crews "Three Dimensional Analysis of [0/90]s and [90/0]s Laminates with a Central Circular Hole," Composite Technology Review, 4(4):116-124 (1982)
9.
Carlsson, L. "Interlaminar Stresses at a Hole in a Composite Member Subjected to an In-Plane Loading," J. Composite Materials , 17.241 (1983).
10.
Encson, K. , M. Persson, L. Carlsson and A. Gustavsson "On the Prediction of the Initiation of Delamination in a [0/90] s Laminate with a Circular Hole," Journal of Composite Materials, 18495-506 (1984).
11.
Wang, A.S.D., W. Binienda, Y. Zhong and E.S. Reddy "Mixed Mode Fracture of Umaxial Fiber Reinforced Composites," NADC-TR-87133-60, Naval Air Development Center, War-minster, PA 18974 (April 1987).
12.
Reddy, E.S. , N.N. Kishore and A S. D. Wang "A Three Dimensional Finite Element Code and Users' Manual for Matrix Cracking in Laminates," Drexel University Technical Report (September 1987)