Experimental studies on compression-after-impact behavior of quasi-isotropic composite laminates

Science and Engineering of Composite Materials

Volumn 6, Issue 1, 1997, Pages 19-35

  Wang, H ^a   Chen, P H ^b   Shen, Z ^b  

^a NATIONAL RESEARCH COUNCIL CANADA   (Canada)

^b AIRCRAFT STRENGTH RESEARCH INSTITUTE OF CHINA   (China)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0344772343     PISSN: 0334181X     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

References (16)

1. Baker, A. A., R. Jones and R. J. Callinan, "Damage Tolerance of Graphite/Epoxy Composites," Composite Structures, 4:15-44(1985).
2. Chai, H., C. D. Babcock and W. G. Knauss, "One Dimensional Modeling of Failure in Laminated Plates by Delamination Buckling," Int. J. Solids & Structures, 17: 1069-1083 (1981).
3. Whitcomb, J. D., "Finite Element Analysis of Instability-Related Delamination Growth," NASA-TM-81964 (1981).
4. Yeh, M.-K. and C.-M. Tan, "Buckling of Elliptically Delaminated Composite Plates," J. Composite Materials, 28:36-52 (1994).
5. Kutlu, Z and F.-K. Chang, "Modeling Compression Failure of Laminated Composites Containing Multiple Through-the-Thickness Delaminations," J. Composite Materials, 26: 350-387 (1992).
6. Wang, S.S., N. M. Zahlan and H. Suemasu, "Compressive Stability of Delaminated Random Short-Fiber Composites, Part 1-Modeling and Methods of Analysis," J. Composite Materials, 19:296-316 (1985).
7. Wang, H., P. H. Chen and Z. Shen, "Barely Visible Impact Damage and its Effects on Compression Behavior of Composite Laminates," (submitted to J. Theor. Appli. Fract. Mech.)
8. Wang, H., P. H. Chen and Z. Shen, "Simulating Impact Damage by Artificial Defects in Composite Laminates under Compression," (to be submitted).
9. Zhao, Q. S., "Preliminary Studies on a Bismaleimide Resin for Carbon Fiber Reinforced Composites," Aviation Technology, No.1, 1988 (in Chinese).
10. Joshi, S. P. and C. T. Sun, "Impact Induced Fracture in a Laminated Composites," J. Composite Materials, 19:51-66(1985).
11. Wang, H. and T. Vu-Khanh, "Damage Extension in Carbon Fiber/PEEK Crossply Laminates under Low Velocity Impact," J. Composite Materials, 28:684-707(1994).
12. Starnes, J. H., Jr., M. D. Rhodes and J. G. Williams, "Failure Characteristics of Graphite/Epoxy Structural Components Loaded in Compression," NASA-TM-84552 (1982).
13. Carlsson, L. A. and R. B. Pipes, Experimental Characterization of Advanced Composite Materials, Prentice-Hall, Inc., Englewood Cliffs, New Jersey (1987).
14. Chatterjee, S. N., W. A. Dick and R. B. Pipes, "Mixed-Mode Delamination Fracture in Laminated Composites," Composites Science & Technology, 25: 49-67 (1986).
15. Chai, H., "Interlaminar Shear Fracture of Laminated Composites," Int. J. Fract. 43:117-131(1990).
16. Li, J., Lee, S. M., Lee, E. W. and O'Brien, T. K., "Evaluation of the Edge Crack Torsion (ECT) Test for Mode III Interlaminar Fracture Toughness of Laminated Composites," NASA-TM-110264, (1996).