Quasi-static behavior of three-dimensional integrated core sandwich composites under compression loading
Source abstract
Abstract
In the current study, the effect of the thickness and the foam density in three-dimensional integrated woven sandwich composites on quasi-static properties was investigated. For this purpose, produced samples were subjected to uniaxial flatwise compression tests and their compression strength and moduli were determined. Obtained results were optimized by taking core thickness, foam density and panel weights into consideration. Damages that occurred on the tested samples were reported. When compared to conventional foam core sandwich composites, it was found that three-dimensional integrated sandwich composites have better compression properties and due to the fact that the pile yarns in the core and the foam support each other.
Source: crossref · Quality: baseline
Research context
OpenAlex topics: Cellular and Composite Structures · Mechanical Behavior of Composites · Polymer Foaming and Composites
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
Affiliations
University of Uludag Vocational School of Technical Sciences, Gorukle Bursa, Turkey
University of Leuven, Department of Metallurgy and Materials Engineering, Leuven, Belgıum
University of Leuven – Thomas More, Department of Engineering Technology, Sint-Katelijne-Waver, Belgıum
References (43)
Show source-provided references
1. 10.1016/S1359-835X(96)00098-X10.1016/S1359-835X(96)00098-X ↗
2. Zenkert D. The handbook of sandwich construction , London: Engineering Materials Advisory Chameleon Press, 1997, pp. 165–167.
3. 10.1016/S0263-8223(02)00087-910.1016/S0263-8223(02)00087-9 ↗
4. 10.1016/S0734-743X(98)00037-210.1016/S0734-743X(98)00037-2 ↗
5. 10.1016/j.compscitech.2005.09.00510.1016/j.compscitech.2005.09.005 ↗
6. 10.1016/j.compositesa.2009.03.01210.1016/j.compositesa.2009.03.012 ↗
7. 10.1016/j.compositesa.2009.04.03210.1016/j.compositesa.2009.04.032 ↗
8. 10.1177/004051750934644110.1177/0040517509346441 ↗
9. Karahan M · Mater Sci (Medziagotyra)
10. Barrett DJ. A micromechanical model for the analysis of Z-fiber reinforcement. In: AIAA/ASCE/ASME/AHS SDM Conference , Salt Lake City, Utah, 1996, AIAA-96-1329-CP, pp.62–67.
11. ZCL Composites Inc. Company Literature. ST. Edmonton, AB. Canada, 1998.
12. 10.1016/S1359-835X(00)00025-710.1016/S1359-835X(00)00025-7 ↗
13. 10.1016/S0266-3538(00)00070-110.1016/S0266-3538(00)00070-1 ↗
14. 10.1179/14658019910154062810.1179/146580199101540628 ↗
15. Van Vuure AW, Ivens J and Verpoest I. Sandwich panels produced from sandwich-fabric preforms. In: Proceeding of the International Symposium on Advanced Materials for Lightweight Structures'94 , ESA_ESTEC Noordwijk Netherlands, 22–25 March 1994, pp.609–12.
16. Van Vuure AW, Ivens J and Verpoest I. Sandwich-fabric panels. In: Proceedings of the 40th International SAMPE Symposium and Exhibition . Anaheim convention center, Anaheim California, 8–11 May 1995, pp.996-76.
17. Verpoest I, Wevers M, Ivens J, et al. 3D fabrics for ompression and ımpact resistant composite sandwich structures. In: Proceedings of the 35th International SAMPE Symposium . Anaheim convention center, Anaheim California, 2–5 April 1990, pp.296–305.
18. 10.1080/0040500900865872310.1080/00405009008658723 ↗
19. Nakatani T, Nakai A, Fujita A, et al. Mechanical behaviour in glass 3D woven fabric composites. In: Proceedings of the Fourth Japan International SAMPE Symposium , Tokyo, Japan, 24–28 September 1995, pp.1473–1478.
20. 10.1016/S0263-8223(00)00035-010.1016/S0263-8223(00)00035-0 ↗
21. 10.1177/089270570403541010.1177/0892705704035410 ↗
22. 10.1177/073168440810069710.1177/0731684408100697 ↗
23. 10.1016/j.matdes.2009.06.03910.1016/j.matdes.2009.06.039 ↗
24. 10.1016/0266-3538(95)00135-210.1016/0266-3538(95)00135-2 ↗
25. 10.1016/S1359-835X(00)00017-810.1016/S1359-835X(00)00017-8 ↗
26. 10.1016/S1359-8368(00)00041-X10.1016/S1359-8368(00)00041-X ↗
27. 10.1016/S0263-8223(98)00093-210.1016/S0263-8223(98)00093-2 ↗
28. 10.1016/S1359-835X(00)00025-710.1016/S1359-835X(00)00025-7 ↗
29. 10.1177/004051751243683210.1177/0040517512436832 ↗
30. Zhou GM · J Nanjing Univ Aeronaut Astronaut · 2007 · 39 · 11
31. 10.12989/sem.2001.12.2.16910.12989/sem.2001.12.2.169 ↗
32. 10.1016/S0020-7683(00)00025-110.1016/S0020-7683(00)00025-1 ↗
33. 10.1016/j.compositesa.2010.05.01410.1016/j.compositesa.2010.05.014 ↗
34. Throne JL, Progelhof RC. Impact stress-strain behaviour of low density closed-cell foam. In: Antec 85, Conference Proceedings for the Society of Plastics Engineers, Inc. 43rd Annual Technical Conference . Washington D.C., USA, April 29–May 2, 1985, pp.442–446.
35. 10.1016/0010-4361(94)90004-310.1016/0010-4361(94)90004-3 ↗
36. 10.1016/S0020-7683(98)00048-110.1016/S0020-7683(98)00048-1 ↗
37. 10.1016/S0020-7683(99)00277-210.1016/S0020-7683(99)00277-2 ↗
38. Koissin V and Shipsa A. Mechanical properties of pre-compressed and undamaged Divinycell H-grade foam core. Report C2001-5, Department of Aeronautics, Royal Institute of Technology, Stockholm, 2001.
39. Gibson LJ · 1988
40. 10.1016/0020-7403(92)90013-710.1016/0020-7403(92)90013-7 ↗
41. Koissin V and Shipsha A. Deformation of foam cores uniaxial compression-tension cycle. In: Proceedings of the 7th International Conference Sandwich Structures , Aalborg University, Aalborg, Denmark, 29–31 August 2005.
42. Zhou GM · J Nanjing Univ Dept Aeronaut Astronaut · 2007 · 39 · 11
43. 10.1007/s00419-006-0032-x10.1007/s00419-006-0032-x ↗