• Composites Research
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• 제22권6호
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• pp.18-22
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• 2009

본 논문에서는 복합적층판의 저속충격실험을 통하여 충격력과 충격거동의 관계를 확인하였다. 또한 육안으로 확인하기 어려운 손상역영을 탐지하기 위하여 비파괴검사인 c-scan을 이용하였다. CAI실험을 통하여 저속충격을 받은 복합적층판의 압축강도를 측정하였다. 저속충격실험, 비파괴검사, CAI실험을 통한 복합적층판의 저속충격거동 특성을 확인하기 위해 몬테카를로 시뮬레이션을 적용하여 가상의 확률분포를 나타냈다. 가시화된 통계적 확률분포를 이용하여 주요변수들을 비교 및 분석하였다.

• 한국안전학회지
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• 제17권1호
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• pp.6-10
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• 2002

This paper presents the impact behavior and damage of laminated composite plates subjected to low-velocity impact. For this purpose, a pendulum impact test for impact behavior and C-scan for impact damage are done. Test materials are carbon/epoxy laminated composite plates and stacking sequences $[0/90_4\;[0/45_2/-45]_s,\;[0/45/-45/90]_s$ and [0/26/51/77/-77/-51/-26/0].

• Steel and Composite Structures
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• 제12권3호
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• pp.207-230
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• 2012

Nowadays CFRP (Carbon Fiber Reinforced Polymer) became widely used materials for the strengthening and retrofitting of structures. Many experimental and analytical studies are encountered at literature about strengthening beams by using this kind of materials against static loads and cyclic loads such as earthquake or wind loading for investigating their behavior. But authors did not found any study about strengthening of RC beams by using CFRP against low velocity impact and investigating their behavior. For these reasons an experimental study is conducted on totally ten strengthened RC beams. Impact loading is applied on to specimens by using an impact loading system that is designed by authors. Investigated parameters were concrete compression strength and drop height. Two different sets of specimens with different concrete compression strength tested under the impact loading that are applied by dropping constant weight hammer from five different heights. The acceleration arises from the impact loading is measured against time. The change of velocity, displacement and energy are calculated for all specimens. The failure modes of the specimens with normal and high concrete compression strength are observed under the loading of constant weight impact hammer that are dropped from different heights. Impact behaviors of beams are positively affected from the strengthening with CFRP. Measured accelerations, the number of drops up to failure and dissipated energy are increased. Finite element analysis that are made by using ABAQUS software is used for the simulation of experiments, and model gave compatible results with experiments.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2002년도 춘계학술발표대회 논문집
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• pp.89-92
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• 2002

Traditionally unidirectional laminated composite which are characterized by high specific stiffness and strength were used for structural application. But theses composites are highly susceptible to impact damage because of lower transverse tensile strength. The main failure modes of laminated composite are fiber breakage, matrix cracking and delamination for low velocity impact. The modified failure criterions are implemented to predict these failure modes with finite element analysis. Failure behavior of the woven fabric laminated composite which is used in forehead part of subway to lighten weigh has been studied. The new failure criterions are in good agreement with experimental results and can predict the failure behavior of the woven fabric composite plate subjected to low velocity impact more accurately.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2000년도 추계학술발표대회 논문집
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• pp.98-101
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• 2000

Recently, composite material which has much excellent mechanical characteristics has been applied in many industries. However, it has a brittle characteristic under impact condition and its invisible characteristics of the damaged area has been the motivation of many engineers investigation. The modified failure criterion is implemented to predict the failure behavior of the composite plate subjected to low velocity impact using commercial finite element analysis code, ABAQUS-Ver. 5.8. The new criterion is in good agreement with experimental results and can predict the failure behavior of the composite plate subjected to low velocity impact more accurately.

• Composites Research
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• 제20권5호
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• pp.1-6
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• 2007

본 연구에서는 탄소/에폭시 복합재 적층판과 강철평판의 저속충격 거동에 관한 비교 연구를 수행하였다. 각각의 평판의 해석을 위한 판의 충격거동의 타당성을 검증하기 위해 Karas 모델을 사용하여 해석 검증을 하였다. 충격거동 비교연구를 위한 모델은 Karas 모델과 동일한 두께의 강철평판을 모사하였고, 같은 두께의 복합재 적층판을 모사하기 위하여 $[0/90/45/-45/-45/45/90/0]_{8S}$ 적층각을 이용하여 모델링 하였다. 각각의 판에 대한 저속충격 거동을 비교하기 위해 일정한 속도로 낙하하는 충격체 무게별 해석과 일정한 무게를 가진 충격체의 속도변화에 따른 해석 결과를 비교 연구하였다. 연구결과 복합재 적층판과 강철평판의 물성치로 인하여 접촉하중과 판의 변위에서는 결과값의 차이를 보였으나 복합재 적층판의 경우가 판의 유연한 특성으로 충격완화 효과가 보였으며 강철평판 보다 무게비와 충격손상에 대한 우수성을 확인하여 볼 수 있었다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2012년도 춘계학술대회 논문집
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• pp.987-988
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• 2012

• International Journal of Precision Engineering and Manufacturing
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• 제6권1호
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• pp.36-41
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• 2005

• 한국정밀공학회지
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• 제14권6호
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• pp.135-141
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• 1997

Low velocity impact test and compressive residual strength test after impact were performed by using Hercules AS4/3501-6[45/0/-45/90]$_{2s}$ laminated plate to investigate the low velocity impact damage behavior and the post-impact strength degradation on orthotropic composite laminate plate. Due to the lateral impact losd, the load path showed "" shape according to the laminate central deflection. Damage in a laminate occurs by inclined matrix crack at the damage initiation load stage and vertical matrix crack, occurs on the outer surface. Evaluating the compressive residual strength after the low velocty impact test, it could be found that there is a transient range where the compressive residual strength drop suddenly in the initial damage which is in the matrix crack range and the initial delamination area. is in the matrix crack range and the initial delamination area.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2012년도 추계학술대회 논문집
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• pp.757-758
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• 2012