Properties Comparison of Open Hole and Non-Hole Carbon UD-Lycal Composite with Vacuum Bagging Manufacturing Method

Lathifa Rusita Isna, Afid Nugroho, Rezky Agung Pratomo, Redha Akbar Ramadhan

Abstract

Carbon fiber reinforce polymer is one of some composite materials that has the high strength with light weight material. To apply this composite to the amphibious airplane structure, it should through the experimental tensile test to know the tensile strength and modulus of elasticity of the composite. In this experiment, we use Carbon UD fiber and Lycal resin as the composite material that manufactured with Vacuum Bagging Method. Specimens and testing process refer to ASTM D3039 for non-hole specimen, and ASTM D5766 for open hole specimen of tensile test standard for composite matrix polymers. The result of the experimental test shows that the tensile modulus of elasticity for non-hole composite is 34.92 ± 0.13 GPa, with the Ultimate Tensile Strength of this composite is 1081± 0.03 MPa, and the modulus of elasticity for open hole composite is 41.87± 0.02 GPa, with the Ultimate Tensile Strength of this composite is 899.04± 0.02 MPa. The simulation yields nearly same stress-strain graph with the result of experiment. The result shows that, the open hole composite has the ultimate tensile strength lower than non-hole composite, it’s due to the open hole composite has a trigger failure that may decreasing the tensile strength value.

Keywords

composite, carbon fiber, vacuum bagging, tensile testing, hole specimen.

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References

- ASTM International, “D3039/D3039M-17 Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials.” ASTM International, 100 Barr Harbor Drive, PO Box C700, West Conshohocken, PA 19428-2959. United States, pp. 1–13, 2017.

- ASTM International, “D5766/D5766M-02a Standard Test Method for Open Hole Tensile Strength of Polymer Matrix Composite Laminates,” in ASTM Book of Standards, vol. 15.03, 2002, pp. 1–6.

- B.G. Green, M. R. Wisnom, and S. R. Hallett, “An experimental investigation into the tensile strength scaling of notched composites,” Compos. Part A Appl. Sci. Manuf., vol. 38, no. 3, pp. 867–878, 2007, doi: 10.1016/j.compositesa.2006.07.008

- G Padhi, C.T.Mccarthy, M.A. Mccarthy. “Experimental and Numerical Study of the Open-Hole Tensile Strength of Carbon / Epoxy Composites”. Mechanics of Composite Materials · 2004.DOI:10.1023/B:MOCM.0000039744 .98869.0d.

- G. Yamamoto, K. Koizumi, and T. Okabe, “Tensile Strength of Unidirectional Carbon Fiber-Reinforced Plastic Composites,” in Intech Open, Sendai, Japan: Intech Open, 2019.

- MIL-HDBK-17-F, Composite Materials Handbook, US DOD, published by ASTM International, Pennsylvania, USA.

- M. S. Ismail, T. K. Kwan, M. I. Hussain, and Z. M. Zain, “Automatic compaction device for composite panel production at layup process: A case study,” Univers. J. Electr. Electron. Eng., vol. 6, no. 5, pp. 68–74, 2019, doi: 10.13189/ujeee.2019.061508.

- R. M. O’Higgins, M. A. McCarthy, and C. T. McCarthy, “Comparison of open hole tension characteristics of high strength glass and carbon fibre-reinforced composite materials,” Compos. Sci. Technol., vol. 68, no. 13, pp. 2770–2778, 2008, doi: 10.1016/j.compscitech.2008.06.003.

- W. H. Alhazmi et al., “Notch tensile strength of carbon fiber/epoxy composite plate with a center hole under static and cyclic loading,” Procedia Struct. Integr., vol. 17, pp. 292–299, 2019, doi: 10.1016/j.prostr.2019.08.039

- X. Huang, “Fabrication and properties of carbon fibers,” Materials (Basel)., vol. 2, pp. 2369–2403, 2009, doi: 10.3390/ma2042369.

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