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    일방향 CFRP 적층판의 모드 2 동적 층간파괴인성 평가 = Evaluation of Mode 2 Dynamic Interlaminar Fracture Toughness of Unidirectional CFRP Laminates

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    https://www.riss.kr/link?id=A3082180

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    In this paper, an investigation was performed on the Mode II dynamic interlaminar fracture toughness of unidirectional CFRP laminates. The stacking sequences used in this experiment are two kinds of [0˙_(20)] and [0˙_(10)/F₂/0˙_(10)]. In the experiments, Split Hopkinson's Bar test was applied to dynamic and notched flexure test. The Mode Ⅱ fracture toughness of each unidirectional CFRP was estimated by the analyzed deflection of the specimen and J-Integral with the measured impulsive load and reactions at the supported points. As an experimental results, the specimen [0˙_(10)/F₂/0˙_(10)] appears greater than that of [0˙_(20)] for the J^-integral and displacement velocity at a measuring point within the range of experiment.
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    In this paper, an investigation was performed on the Mode II dynamic interlaminar fracture toughness of unidirectional CFRP laminates. The stacking sequences used in this experiment are two kinds of [0˙_(20)] and [0˙_(10)/F₂/0˙_(10)]. In the expe...

    In this paper, an investigation was performed on the Mode II dynamic interlaminar fracture toughness of unidirectional CFRP laminates. The stacking sequences used in this experiment are two kinds of [0˙_(20)] and [0˙_(10)/F₂/0˙_(10)]. In the experiments, Split Hopkinson's Bar test was applied to dynamic and notched flexure test. The Mode Ⅱ fracture toughness of each unidirectional CFRP was estimated by the analyzed deflection of the specimen and J-Integral with the measured impulsive load and reactions at the supported points. As an experimental results, the specimen [0˙_(10)/F₂/0˙_(10)] appears greater than that of [0˙_(20)] for the J^-integral and displacement velocity at a measuring point within the range of experiment.

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