Experimental investigation on dynamic and static transverse behaviour of thin woven Carbon/Aramid hybrid laminates

被引：12

作者：

Andrews Zachariah S. ^{[1
]}

Satish Shenoy B. ^{[1
]}

Jayan J. ^{[1
]}

Pai K.D. ^{[1
]}

机构：

[1] Department of Aeronautical and Automobile Engineering, Manipal Institute of Technology, Manipal Academy of Higher Education, Manipal

来源：

Journal of King Saud University - Engineering Sciences | 2022年 / 34卷 / 04期

关键词：

Aramid fibre; Hybrid composites; Impact behaviour; Static behaviour;

D O I：

10.1016/j.jksues.2020.09.015

中图分类号：

学科分类号：

摘要：

Trends in the development of lightweight micro/mini Unmanned Aerial Vehicles (UAVs) demand thin composite laminates for their structural applications. As these structures experience impact loading during their life cycle, the performance enhancement in the through-the-thickness direction is deemed mandatory. This study investigates the application of Aramid/Carbon fibre reinforced polymer hybrid thin laminate in enhancing static and dynamic transverse loading behaviour. Laminates are fabricated by Vacuum-Assisted Resin Infusion Moulding (VARIM) process. A three-point bending and the Charpy impact tests were conducted to analyse the static and the dynamic transverse loading behaviour of the hybrid laminates, respectively. The effect of location and stacking sequence of the woven aramid layers on low-velocity impact and the static transverse flexural loading has been investigated in this study. The results have revealed that the location and the stacking sequences of the Aramid fabric in laminated CFRP play an essential role in their impact strength with a compromise in the flexural properties. The laminates with two layers of Aramid fabric at (0/90) and (±45) orientation each on their outer surface displayed a better impact behaviour in terms of the average impact strength and the absorbed energy. The images obtained from optical micrography conclude that the delamination and fibre breakage as the significant damages due to through-the -thickness loading. © 2020 The Authors

引用

页码：273 / 281

页数：8

共 53 条

[31]

Nayak S.Y., Heckadka, Sathish Rao, pp. 30-36, (2015)

[32]

Nugroho G., Pranoto I., Rohmana N.Z., Effect of breather type and vacuum pressure on the manufacturing of an unmanned aerial vehicle fuselage using vacuum bagging method, AIP Conf. Proc., 1983, (2018)

[33]

Mangalgiri P.D., Composite materials for aerospace applications, Bull. Mater. Sci, 22, pp. 657-664, (1999)

[34]

Mallick P.K., Fiber-reinforced Composites, (2007)

[35]

Padmaraj N.H., Vijaya K.M., Dayananda P., Experimental study on the tension-tension fatigue behaviour of glass/epoxy quasi-isotropic composites, J. King Saud Univ. – Eng. Sci., 32, pp. 396-401, (2020)

[36]

Razali N., Sultan M.T.H., Mustapha F., Yidris N., (2014)

[37]

Richardson M.O.W., Wisheart M.J., Review of low-velocity impact properties of composite materials, Compos. Part A: Appl. Sci. Manuf., 27, pp. 1123-1131, (1996)

[38]

Shin M.K., Lee B., Kim S.H., Lee J.A., Spinks G.M., Gambhir S., Wallace G.G., Kozlov M.E., Baughman R.H., Kim S.J., Synergistic toughening of composite fibres by self-alignment of reduced graphene oxide and carbon nanotubes, Nat. Commun., 3, pp. 650-658, (2012)

[39]

Singh T.J., Samanta S., Characterization of Kevlar fiber and its composites: a review, Mater. Today: Proc., 2, pp. 1381-1387, (2015)

[40]

Soetanto M.F., pp. 178-185, (2016)

← 1 2 3 4 5 6 →