Title of article :
Impacts of Volume of Carbon Nanotubes on Bending for CarbonKevlar Hybrid Fabrics
Author/Authors :
Randjbaran, Elias Department of Aerospace Engineering - Faculty of Engineering, Selangor, Malaysia , Majid, Dayang L. Department of Aerospace Engineering - Faculty of Engineering, Selangor, Malaysia , Zahari, Rizal Systems Engineering Department - Military Technological College Ministry of Defence, Muscat, Sultanate of Oman , Sultan, Mohamed T. H. Department of Aerospace Engineering - Faculty of Engineering, Selangor, Malaysia , Mazlan, Norkhairunnisa Department of Aerospace Engineering - Faculty of Engineering, Selangor, Malaysia
Abstract :
Carbon nanotubes indicate mechanical properties ideally examined for reinforced Carbon/Kevlar hybrid fabrics in the
intact specimens by SEM and EDX observations an Carbon nanotubes indicated mechanical properties that were examined for
reinforced Carbon/Kevlar hybrid fabrics in the intact specimens by SEM and EDX observations and after attempting six successful
ballistic impacts, at various targets’ angles: normal impact (0-degree), 10-degree, 20-degree, 30-degree, and 40-degree) with the
different volume of CNT% (0, 0.1, 0.3, 0.5, 0.7, 1, and 1.5) after attempting six successful ballistic impacts, at various targets’ angles:
normal impact (0-degree), 10-degree, 20-degree, 30-degree, and 40-degree) with the different volume of CNT% (0, 0.1, 0.3, 0.5, 0.7, 1,
and 1.5). Each sample was fabricated by the same curing unit and then evaluated by the three‐point bending universal testing
machine model (INSTRON-3369). Flexural Stress-Strain curves under 3-points bending in CNT epoxy composite laminates
calculated flexural modulus of elasticity and bending toughness at room temperature.
Keywords :
Carbon nanotubes , 3-points bending , Oblique ballistic impact , Kevlar fibre , Carbon fibre , Flexural
Journal title :
Journal of Applied and Computational Mechanics