• 비파괴검사학회지
• /
• 제7권2호
• /
• pp.42-47
• /
• 1988

이상의 결과를 요약하면 다음과 같다. 1) 초음파 C-scan 법에 의하여 층간분리, 기지균열 등의 손상 정도, 크기 및 형태의 판별이 가능하며 충격손상은 주로 섬유의 주축방향으로 성장한다. 2) 복합재료의 인장파괴시 적층구조에 따라 상이한 AE 양상을 나타내며 이 원인은 파괴 mode의 차이에 기인한다. 3) 섬유의 파단은 기지파단의 경우 보다 강력한 AE activity를 나타내며 peak amplitude의 분포를 분석하여 파괴 mode의 해석이 가능하다. 4) 복합재료의 파괴강도는 적층구조, 충격 손상 등에 영향을 받으며 응력파 계수(SWF)의 측정에 의해 정성적 평가가 가능하다.

• 한국구조물진단유지관리공학회 논문집
• /
• 제10권6호
• /
• pp.183-190
• /
• 2006

본 연구는 철근콘크리트 보에 대해 선가력 후 보강재료별로 보강 효과를 파악하기 위하여 휨 실험한 결과, 다음과 같은 결론을 얻었다. 실험결과, CB 보강 실험체가 콘크리트 내부에 매입되어 일체 거동함으로써 휨내력 향상 및 연성능력 면에서 가장 우수한 것으로 나타났으며, 섬유계 보강재인 CFS와 GFS 보강 실험체 또한 우수한 내력을 가지는 것으로 나타났다. GSP 보강실험체의 경우 다른 보강 실험체에 비해 보강재 자체의 내력은 큰데 반해 콘크리트와 부착성이 떨어져 상대적으로 낮은 보강효과를 보였으며 실제 구조체에서는 콘크리트와 부착성이 개선 되어 보다 큰 보강효과를 발휘할 것으로 사료된다.

• 예술인문사회 융합 멀티미디어 논문지
• /
• 제7권11호
• /
• pp.925-932
• /
• 2017

본 연구에서는 복합재료들 중 단방향성 탄소섬유강화플라스틱(UD CFRP)에서의 적층각도에 따른 비틀림을 받는 판의 해석을 수행하였다. UD CFRP의 경우에는 적층각도에 따른 물성치가 달라진다. 그리고 연구 모델들에서 탄소 섬유의 적층각도는 15°, 30°, 45°, 60°, 75°, 90° 로 지정하였다. 중앙부에는 리벳이나 볼트가 사용될 것으로 가정하여 노치홀을 적용하였다. ISO 15310에서의 실험 방식을 적용하여 해석 방법을 사용했다. 하부에서 2개의 지그를 고정하고 상부에서 2개의 지그를 하강한다. 본 연구에서의 해석 결과값을 보았을 때, 적층각도가 45°일 경우가 파단 부위에 나타나는 전단응력이 254.74MPa로 가장 작은 값으로 나타남을 보였다. 따라서 비틀림이 작용할 때, 45°의 적층각도의 경우가 다른 적층각도에 비하여 더 높은 구조안전성과 내구성을 가졌음을 알 수 있었다. 이러한 결과는 CFRP 판에 비틀림이 작용할 때 그 내구성에 기여할 수 있는 기반 데이터로 적용될 수 있다고 사료된다.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2002년도 춘계학술대회 논문집
• /
• pp.812-815
• /
• 2002

This paper deals with the buckling and vibration analysis of plate with a hole. We knew that in this paper, as aspect ratio rises in design parameter, the buckling strength and the natural frequency of laminated composite plate decrease and as diameter of hole for width of plate rises, the buckling strength decrease but the natural frequency increase. Also this paper compared the CFRP laminated composit plate with the hybrid composite plate, and proposed that the hybrid composite plate is stronger than the CFRP composite plate.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2003년도 춘계학술대회 논문집
• /
• pp.1362-1365
• /
• 2003

On this study. we improved the efficiency applying algorithm that is repeatedly using orthogonal array in discrete design space and filling a defect of gradient method in continuous design space. we showed optimal ply angle that maximized buckling strength of CFRP laminated composite plate without a hole and with a hole by each aspect ratio. In the case of CFRP laminated composite plate without a hole, we confirmed the reliance and efficiency of algorithm in comparison with the result optimization achievement repeatedly using statistical orthogonal array of experimental design.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2003년도 추계학술대회
• /
• pp.1660-1665
• /
• 2003

On this study, we improved the efficiency applying algorithm that is repeatedly using orthogonal array in discrete design space and filling a defect of gradient method in continuous design space. we showed optimal ply angle that maximized 1st natural frequency of CFRP laminated composite cantilever plate by each aspect ratio. A finite element analysis on the CFRP laminated composite cantilever plate using orthogonal array is carried out, and the results are compared with those obtained by modal testing.

• 한국소음진동공학회논문집
• /
• 제13권6호
• /
• pp.423-429
• /
• 2003

On this study. we improved the efficiency applying algorithm that is repeatedly using table of orthogonal array in discrete design space and filling a defect of gradient method in continuous design space. we showed optimal ply angle that maximized 1st natural frequency of CFRP laminated composite plate without a hole and with a hole by each aspect ratio. In the case of CFRP laminated composite plate without a hole, we confirmed the reliance and efficiency of algorithm in comparison with the result of optimization achievement repeatedly using statistical table of orthogonal array of experimental design and the BFGS optimal design method.

• 한국재료학회지
• /
• 제34권2호
• /
• pp.72-78
• /
• 2024

The lightweight and high strength characteristics of aluminum alloy materials make them have promising prospects in the field of construction engineering. This paper primarily focuses on aluminum alloy materials. Aluminum alloy was combined with concrete, wood and carbon fiber reinforced plastic (CFRP) cloth to create a composite column. The axial compression test was then conducted to understand the mechanical properties of different composite structures. It was found that the pure aluminum tube exhibited poor performance in the axial compression test, with an ultimate load of only 302.56 kN. However, the performance of the various composite columns showed varying degrees of improvement. With the increase of the load, the displacement and strain of each specimen rapidly increased, and after reaching the ultimate load, both load and strain gradually decreased. In comparison, the aluminum alloy-concrete composite column performed better than the aluminum alloy-wood composite column, while the aluminum alloy-wood-CFRP cloth composite column demonstrated superior performance. These results highlight excellent performance potential for aluminum alloy-wood-CFRP composite columns in practical applications.

• Structural Engineering and Mechanics
• /
• 제44권6호
• /
• pp.705-733
• /
• 2012

In this work, an experimental examination was carried out to study interfacial stresses developed at the junction zones between carbon fiber reinforced plastic (CFRP) fabrics (~1 mm thickness) and tensile concrete portion in CFRP retrofitted RC beams. In this respect, initially six similar RC beams of $150{\times}150{\times}1000mm$ dimensions were prepared. Three of which were strengthened with CFRP fabrics at the tensile side of the beams. Furthermore, a notch was cut at the center of the bottom surface for all of the studied beams. The notch was 15 mm deep and ran across the full width of tension side of the beams. The mentioned interfacial stresses could be calculated from strains measured using strain gauges mounted on the interface zone of the tensile concrete and the CFRP sheet. Based on the results obtained, it is shown that interfacial stresses developed between CFRP fabrics and RC beam had a noticeable effect on debonding failure mode of the latter. The load carrying capacity of CFRP strengthened RC specimens increased ~75% compared to that of the control RC beams. This was attributed to the enhancement of flexural mode of the former. Finally, finite element analysis was also utilized to verify the measured experimental results.

• Computers and Concrete
• /
• 제18권6호
• /
• pp.1083-1096
• /
• 2016

Beam-column joints are recognized as the weak points of reinforcement concrete frames. The ductility of reinforced concrete (RC) frames during severe earthquakes can be measured through the dissipation of large energy in beam-column joint. Retrofitting and rehabilitating structures through proper methods, such as carbon fiber reinforced polymer (CFRP), are required to prevent casualties that result from the collapse of earthquake-damaged structures. The main challenge of this issue is identifying the effect of CFRP on the occurrence of failure in the joint of a cross section with normal ductility. The present study evaluates the retrofitting method for a normal ductile beam-column joint using CFRP under monotonic and cyclic loads. Thus, the finite element model of a cross section with normal ductility and made of RC is developed, and CFRP is used to retrofit the joints. This study considers three beam-column joints: one with partial CFRP wrapping, one with full CFRP wrapping, and one with normal ductility. The two cases with partial and full CFRP wrapping in the beam-column joints are used to determine the effect of retrofitting with CFRP wrapping sheets on the behavior of the beam-column joint confined by such sheets. All the models are subjected to monotonic and cyclic loading. The final capacity and hysteretic results of the dynamic analysis are investigated. A comparison of the dissipation energy graphs of the three connections shows significant enhancement in the models with partial and full CFRP wrapping. An analysis of the load-displacement curves indicates that the stiffness of the specimens is enhanced by CFRP sheets. However, the models with both partial and full CFRP wrapping exhibited no considerable improvement in terms of energy dissipation and stiffness.