Work

Evaluation of Residual Strength Under Impact Damage in Woven CFRP Composites

Year: 2012

Type: article

Abstract: Damage induced by low velocity impact loading in aircraft composite is the form of failure which is frequently occurred in aircraft. As the consequences of impact loading in composite laminates, matrix cracking, delamination and eventually fiber breakage for higher impact energies can be occurred. Even when no visible impact damage is observed, damage can exist inside of composite laminates and carrying load of the composite laminates is considerably reduced. The objective of this study is to evaluate and predict residual strength behavior of composite laminates by impact loading and for this, tensile test after impact was carried out on composite laminates made of woven CFRP.

Source: Journal of the Korean Society for Precision Engineering

DOI: 10.7736/kspe.2012.29.6.654

Authors: Jung-Hun Choi, Min-Sung Kang, Jae-Mean Koo, Chang-Sung Seok

Institution: Sungkyunkwan University

Language: English

Topic: Mechanical Behavior of Composites

Subfield: Mechanics of Materials

Field: Engineering

Domain: Physical Sciences

Open Access status: diamond

OpenAlex ID: W1781097331

FWCI: 0.422

Cites: 16

Cited by: 1

Related to: 10