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[학술저널]

  • 학술저널

최정훈(현대기아자동차) 강민성(넥센타이어) 구재민(성균관대학교) 석창성(성균관대학교)

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초록

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.

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1. 서론
2. 충격 및 잔류강도 시험
3. 충격손상을 받은 복합재료의 잔류강도 예측 모델
4. 결론
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