Jute/Carbon Fiber로 강화된 Epoxy-based Hybrid 복합재료의 Drop Weight Impact 및 Tension-Tension Loading Fatigue 거동

Zamurrad Arshad; Muhammad Ali Nasir; Yasir Baig; Muhammad Zeeshan; Rizwan Ahmed Malik; Khubab Shaker; Azhar Hussain; M. Latif; Maryam Sattar; Hussein Alrobei

Polymer(Korea), Vol.44, No.5, 610-617, September, 2020

DOI10.7317/pk.2020.44.5.610 Export Citation

Jute/Carbon Fiber로 강화된 Epoxy-based Hybrid 복합재료의 Drop Weight Impact 및 Tension-Tension Loading Fatigue 거동

Drop Weight Impact and Tension-Tension Loading Fatigue Behaviour of Jute/Carbon Fibers Reinforced Epoxy-based Hybrid Composites

Zamurrad Arshad, Muhammad Ali Nasir, Yasir Baig¹, Muhammad Zeeshan², Rizwan Ahmed Malik³, Khubab Shaker², Azhar Hussain³, M. Latif⁴, Maryam Sattar⁵, and Hussein Alrobei^{6, †}

Department of Mechanical Engineering, University of Engineering and Technology, Taxila, Pakistan
¹Beijing University of Aeronautics and Astronautics, No. 37 Xueyuan Road, Beijing, CN 100191, China
²National Textile University, Faisalabad, Pakistan
³Department of Metallurgy and Material Engineering, University of Engineering and Technology, Taxila, Pakistan
⁴Department of Mechanical Engineering, Inha University, Incheon, Korea
⁵Department of Mechanical Engineering, Institute of Space Technology, Islamabad, Pakistan
⁶Department of Mechanical Engineering, College of Engineering, Prince Sattam bin Abdul aziz University, AlKharj, Saudi Arabia

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This work focuses on the synthesis of a novel hybrid composite, fabricated by utilizing jute and carbon fibers reinforced epoxy composites through hand layup technique to replace pure carbon-epoxy fiber composites. The mechanical properties were evaluated by drop weight impact and tension-tension fatigue tests. The tension-tension fatigue test was conducted to monitor the dynamic stiffness and fatigue life degradation of hybrid composite materials by varying the layers of jute fiber. The maximum peak load during the impact test was observed as 1081.7 N in case of carbon/jute/carbon/jute/carbon (CJCJC) stacking sequence composite materials. Finally, the surface morphology of hybrid composite materials was studied with scanning electron microscopy (SEM) after mechanical tests to check the delamination, fiber pull-out and matrix cracks. It can be concluded from the obtained mechanical results that the newly developed composite with 15% jute/carbon-epoxy hybrid materials has the potential to swap carbon-epoxy composite without much loss of fatigue life along with relatively enhanced ductility as well as impact strength.

Keywords:carbon;jute;hybrid composites;fatigue test;impact test;SEM morphology

[References]

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[Referenced By]

[1] Dhakal HN, Zhang ZY, Guthrie R, MacMullen J, Bennett N, Carbohydr. Polym., 96, 1 (2013)

[2] Vijayan R, Krishnamoorthy A, Mater. Today Proc., 16, 897 (2019)

[3] Latif M, Prabhakar MN, Nam GB, Lee DW, Song JI, Compos. Res., 30, 303 (2017)

[4] Gholampour A, Ozbakkaloglu T, J. Mater. Sci., 55(3), 829 (2020)

[5] Sana R, Foued K, Yosser BM, Mounir J, Slah M, Bernard D, Fiber Polym., 16, 2451 (2015)

[6] Zaman HU, Beg MDH, Fiber Polym., 15, 831 (2014)

[7] Jha K, Samantaray BB, Tamrakar P, Mater. Today Proc., 5, 5601 (2019)

[8] Singh H, Singh JP, Singh S, Dhawan V, Tiwari SK, Mater. Today Proc., 5, 28427 (2018)

[9] Ahsan M, Zwawi M, Taqi M, Kanthasamy R, Bahadar A, Fibers, 7, 77 (2019)

[10] Khalil HPSA, Kang CW, J. Reinf. Plast. Compos., 28, 1123 (2009)

[11] Braga RA, Magalhaes PAA, Mater. Sci. Eng. C-Biomimetic Supramol. Syst., 56, 269 (2015)

[12] Santulli C, Janssen M, Jeronimidis G, J. Mater. Sci., 40(13), 3581 (2005)

[13] Shamsuyeva M, Winkelmann J, Endres HJ, J. Compos. Sci., 3, 43 (2019)

[14] Latif M, Prabahakr MN, Song J, J. Appl. Polym. Sci., 136, 47695 (2019)

[15] Latif M, Kumar CN, Prabahakr MN, Song J, Fiber Polym., 20, 413 (2019)

[16] Sanjay MR, Arpitha GR, Yogesha B, Mater. Today Proc., 2, 2959 (2015)

[17] Thwe MM, Liao K, J. Mater. Sci. Lett., 19(20), 1873 (2000)

[18] Velmurugan R, Manikandan V, Compos. Part A - Appl. Sci. Manuf., 38, 2216 (2007)

[19] Pothan LA, George CN, John MJ, Thomas S, J. Reinf. Plast. Compos., 29, 1131 (2010)

[20] Basiji F, Safdari V, Nourbaksh A, Pilla S, Turk. J. Agric. For., 34, 191 (2010)

[21] Vilay V, Mariatti M, Taib RM, Todo M, Compos. Sci. Technol., 68, 631 (2008)

[22] Alamri H, Low IM, Polym. Test., 3, 620 (2012)

[23] Goud G, Rao RN, Bull. Mater. Sci., 35, 595 (2012)

[24] Shima K, Okubo K, Fujii T, WIT Trans. Eng. Sci., 39, 261 (2003)

[25] Bakar NH, Hyie KM, Mardziah CM, Roselina NRN, Masdek NRN, J. Teknol., 76, 25 (2015)

[26] Tang R, Guo YJ, Weitsman YJ, Int. J. Fatigue, 26, 421 (2004)

[27] Ali A, Nasir MA, Khalid MY, Nauman S, Shaker K, Khushnood S, Altaf K, Zeeshan M, Hussain A, J. Mech. Sci. Technol., 33, 4217 (2019)

[28] Cole DP, Henry TC, Gardea F, Haynes RA, Compos. Sci. Technol., 151, 202 (2017)

[29] Padmaraj NH, Chethan KN, Pavan, Onkar A, IOP Conference Series: Mater. Sci. Eng., 225, 012017 (2017)

[30] Salman SD, Sharba MJ, Leman Z, Sultan MTH, Ishak MR, Cardona F, BioResources, 11, 3575 (2016)

[31] Sarasini F, Tirillo J, Ferrante L, Valente M, Valente T, Lampani L, Gaudenzi P, Cioffi S, Iannace S, Sorrentino L, Compos. Part B-Eng., 59, 204 (2014)

[32] Ramana MV, Ramprasad S, Mater. Today Proc., 4, 8654 (2017)

[33] Isa M, Ahmed A, Aderemi B, Taib RM, Akil HM, Dabo IAM, Leonardo EI. J. Pract. Technol., 13, 97 (2014)