• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 춘계학술발표대회 논문집
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• pp.143.1-146
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• 1999

• 한국염색가공학회지
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• 제28권4호
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• pp.246-252
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• 2016

In comparison to metal alloys, braided composite features a high impact resistance and crash energy absorption potential, and also it still remained competitive stiffness and strength properties. Braiding angle is one of the most important parameters which affect the mechanical behaviors of braided composite. This paper presents transverse low velocity impact failure behavior analysis on the carbon 3D triaxial braided composite tube with the braiding angle of $20^{\circ}$, $50^{\circ}$ and $80^{\circ}$. The flexural behaviour of 3D triaxial braided composite tube under bending loads was studied by conducting quasistatic three point bending test. Also, the low velocity impact responses of the braided composite tubes were also tested to obtain load-displacement curves and energy absorption. Consequently, the increase of the braided angle, the peak load also increases owing to the bigger bending stiffness.

• Composites Research
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• 제32권5호
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• pp.249-257
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• 2019

In this paper, the buckling behavior of triaxially braided circular arch with monosymmetric open section subjected to three-point bending was studied experimentally and numerically. First, test specimens were manufactured using vacuum assisted resin transfer molding (VARTM). Then the specimen was tested under three-point bending to determine the ultimate buckling strength. Before performing the numerical analysis, effective material properties of the braided composite were obtained through micro-meso scale analysis virtual testing validated with available test results. Then linear buckling analysis and geometrically non-linear post buckling analysis, established to simulate the test setup, were performed to study the buckling behavior of the composite frame. Analysis results were compared with experimentally obtained ones for verification. The effect of manufacturing defects of tow misalignment, irregular surface and resin rich region, and uncertainties during test setup were studied using numerical models. From the numerical analyses performed it was observed that both manufacturing defect and uncertainties had effect on the buckling behavior and strength.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.939-941
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• 2017

항공우주 구조물은 경량화를 위하여 복합재의 사용이 증가하고 있다. 이러한 구조물 중 추진기관에 해당하는 발사체 동체의 링 프레임 및 부품은 구조적 파손에 덜 취약한 섬유 강화 복합재를 주로 사용한다. 섬유 강화 복합재의 사용이 증가함에 따라 강성 및 강도의 효율적인 설계 방법에 대한 관심이 높아지고 있다. 본 논문에서는 섬유 강화 복합재 중 2차원 3축 브레이딩 복합재의 단위 체적 형상(Repeating Unit Cell, RUC)에 따른 기계적 강도를 예측하였다. 강도 예측 기법으로 섬유다발의 이산화 기법를 통한 섬유조각(Yarn Slice) 정의, 증분 접근법, 강성저하 모델 등을 사용하였다. 마지막으로 예측된 강도와 시험결과를 비교하여 본 논문에서 정의한 예측 기법의 정확도를 검증하였다.