The impact behaviour of carbon fiber-epoxy composite leading edge using finite element method

• Main Authors: Nurihan, O., Aminanda, b,, Y., Ali, J. S. M., Rasid, Z. A., Hafizal, Y.
• Format: Article
• Language: English
• Published: Blue Eyes Intelligence Engineering and Sciences Publication 2019
• Subjects: T Technology (General)
• Online Access: http://eprints.utm.my/id/eprint/90766/1/ONurihan2019_TheImpactBehaviourofCarbon.pdf; http://eprints.utm.my/id/eprint/90766/; http://dx.doi.org/10.35940/ijrte.B3013.078219

Composite material has been widely used in aircrafts due to its high strength to weight ratio that leads to weight saving of the aircrafts. Equally important, aircraft material should be tough i.e. it should have the ability to absorb high energy and thus resist fracture. The aircraft’s wing design...