Impacts of Volume of Carbon Nanotubes on Bending for Carbon-‎Kevlar Hybrid Fabrics

Publish Year: 1400
نوع سند: مقاله ژورنالی
زبان: English
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شناسه ملی سند علمی:

JR_JACM-7-2_040

تاریخ نمایه سازی: 9 خرداد 1400

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 (۰-degree), ۱۰-degree, ۲۰-degree, ۳۰-degree, and ۴۰-degree) with the different volume of CNT% (۰, ۰.۱, ۰.۳, ۰.۵, ۰.۷, ۱, and ۱.۵) after attempting six successful ballistic impacts, at various targets’ angles: normal impact (۰-degree), ۱۰-degree, ۲۰-degree, ۳۰-degree, and ۴۰-degree) with the different volume of CNT% (۰, ۰.۱, ۰.۳, ۰.۵, ۰.۷, ۱, and ۱.۵). Each sample was fabricated by the same curing unit and then evaluated by the three‐point bending universal testing machine model (INSTRON-۳۳۶۹). Flexural Stress-Strain curves under ۳-points bending in CNT epoxy composite laminates calculated flexural modulus of elasticity and bending toughness at room temperature.

Authors

Elias Randjbaran

Department of Aerospace Engineering, Faculty of Engineering, Serdang, Selangor, ۴۳۴۰۰, Malaysia

Dayang L. Majid

Department of Aerospace Engineering, Faculty of Engineering, Serdang, Selangor, ۴۳۴۰۰, Malaysia

Rizal Zahari

Systems Engineering Department, Military Technological College, Ministry of Defence, Muscat, PO-Box ۲۶۲ PC ۱۱۱, Sultanate of Oman

Mohamed T. H. Sultan

Department of Aerospace Engineering, Faculty of Engineering, Serdang, Selangor, ۴۳۴۰۰, Malaysia

Norkhairunnisa Mazlan

Department of Aerospace Engineering, Faculty of Engineering, Serdang, Selangor, ۴۳۴۰۰, Malaysia

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