Permanent indentation and damage creation of laminates with different composite systems: An experimental investigation
Source abstract
Abstract
Quasi‐static indentation (QSI) and low‐velocity impact tests have been conducted to laminated composite specimens made from different composite systems. C‐scan and thermal deply techniques were used to observe the internal damage characteristics of the laminates. The test results show the effect of fibers and matrices on the permanent indentation and damage behaviors of composite laminates. Fiber breakage plays an important role in the formation of permanent indentation and the match between the fiber and matrix also has a significant influence on the permanent indentation and damage behaviors. A comparison shows the correlation between the peak load energy of the QSI tests and the knee point energy of the impact tests, based on which a condition for the prominent indentation formation was proposed for the impact tests. POLYM. COMPOS., 35:872–883, 2014. © 2013 Society of Plastics Engineers
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Mechanical Behavior of Composites · Metal and Thin Film Mechanics · Tribology and Wear Analysis
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
School of Aeronautic Science and Engineering Beihang University Beijing China
Funding
National Basic Research and Development Program of China
References (36)
Show source-provided references
1. AC 20–107B Subject: Composite aircraft structures Advisory Circular Federal Aviation Administration US Department of transportation (2009).
2. 10.1177/00219983920260140810.1177/002199839202601408 ↗
3. 10.1115/1.312970510.1115/1.3129705 ↗
4. 10.1016/S0266-3538(96)00071-110.1016/S0266-3538(96)00071-1 ↗
5. 10.1016/j.compositesa.2006.04.01310.1016/j.compositesa.2006.04.013 ↗
6. H.SuemasuandY.Aoki Proceedings of the 42nd AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics and Materials Conference and Exhibit American Institute of Aeronautics and Astronautics Seattle Washington(2001).
7. 10.1016/j.compositesb.2011.08.02810.1016/j.compositesb.2011.08.028 ↗
8. 10.1016/S0263-8223(03)00157-010.1016/S0263-8223(03)00157-0 ↗
9. 10.1016/j.compstruct.2008.02.00310.1016/j.compstruct.2008.02.003 ↗
10. Yang S.H. · ASTM STP · 1982 · 787 · 425
11. 10.1115/1.290142110.1115/1.2901421 ↗
12. 10.1016/j.mechmat.2007.07.00310.1016/j.mechmat.2007.07.003 ↗
13. 10.1016/S1359-835X(00)00061-010.1016/S1359-835X(00)00061-0 ↗
14. 10.1016/S0263-8223(00)00138-010.1016/S0263-8223(00)00138-0 ↗
15. 10.1016/j.compscitech.2009.11.00410.1016/j.compscitech.2009.11.004 ↗
16. Shen Z. · Acta Mater. Compos. Sin. · 2008 · 25 · 125
17. 10.1016/j.compstruct.2006.04.08710.1016/j.compstruct.2006.04.087 ↗
18. 10.1016/j.compscitech.2009.02.02910.1016/j.compscitech.2009.02.029 ↗
19. 10.1016/j.ijsolstr.2009.03.01010.1016/j.ijsolstr.2009.03.010 ↗
20. C.Bouvet S.Rivallant andJ.J.Barrau Proceedings of the 14th European Conference on Composite Materials Budapest Hungary(2010).
21. 10.1016/j.compscitech.2012.08.01910.1016/j.compscitech.2012.08.019 ↗
22. 10.1016/j.compositesa.2011.10.00410.1016/j.compositesa.2011.10.004 ↗
23. 10.1016/j.proeng.2011.04.38010.1016/j.proeng.2011.04.380 ↗
24. D.Liu J.Gao andZ.Guan Proceedings of the 9th China‐Japan Joint Conference on Composite Materials 124(2010).
25. Ye Q. · Acta Mater. Compos. Sin. · 2012 · 29 · 144
26. H.Kondo Y.Aoki K.Hiraoka andH.Hatta Proceedings of the 16th International Conference on Composite Materials Kyoto Japan(2007).
27. 10.1016/j.compositesa.2010.02.00510.1016/j.compositesa.2010.02.005 ↗
28. 10.1016/j.compstruct.2012.03.03910.1016/j.compstruct.2012.03.039 ↗
29. Z.Guan Y.Guo Q.Meng andD.Liu Proceedings of the 17th International Conference on Composite Materials Edinburgh Scotland UK(2009).
30. Zheng X. · Acta Aeronaut. Astronaut. Sin. · 2010 · 31 · 929
31. 10.1016/j.compstruct.2008.04.00910.1016/j.compstruct.2008.04.009 ↗
32. 10.1177/073168440504661310.1177/0731684405046613 ↗
33. ASTM D7136/D7136M‐07 Standard test method for measuring the damage resistance of a fiber‐reinforced polymer matrix composite to a drop‐weight impact event. In: ASTM International. (2007).
34. ASTM D6264‐98(04) Standard test method for measuring the damage resistance of fiber‐reinforced polymer matrix composite to concentrated quasi‐static indentation force. In: ASTM International. (2007).
35. 10.1016/j.compscitech.2005.09.00910.1016/j.compscitech.2005.09.009 ↗
36. Li D. · New Carbon Mater. · 2007 · 22 · 59