• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.6
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• pp.484-491
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• 2016

The purpose of this development is weight reduction of hollow type steel torque bar by changing the material from steel to composite. Structure analysis is executed by the finite element model generated by the structural load condition and geometric structure requirement. According to this analysis result, optimized ply sequence and wall thickness are defined. To simulate analysis result, torsion test for composite torque bar was performed. Throughout the test result, the stiffness and strength requirement of composite torque bar was verified.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.37 no.5
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• pp.309-316
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• 2024

In this paper, additive manufacturing (AM)-structural coupled analysis was proposed to accurately predict the mechanical behavior of 3D printed short-fiber reinforced composite structures. Tensile specimens were printed using a composite 3D printer (Mark Two, Markforged), and tensile tests were conducted on specimens manufactured with various nozzle paths. In addition, a reverse engineering scheme was applied to the experimental data to reasonably derive local anisotropic material properties according to the nozzle paths. Consequently, AM-structural coupled analysis was performed using the enhanced finite element model with mapped local materials properties, and the mechanical behavior of the 3D printed short-fiber reinforced composite was accurately described. To demonstrate the effectiveness of the proposed AM-structural coupled analysis model, the computational results obtained were compared with experimental results.

• Journal of the Korea institute for structural maintenance and inspection
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• v.15 no.2
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• pp.61-69
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• 2011

Fiber Reinforced Plastic (FRP) sheets have been widely used to retrofit and rehabilitate RC structures, while in case of retrofitting steel structures, there are no codes and researches. It stems from configuration of member and characteristics of bonding behavior. This study focused on the static behavior of steel beams reinforcement by AFRP sheets. The main objective of the experimental programme was the evaluation of the force transfer mechanism, the increment of the beam load carrying capacity and the bending stiffness. A bending test was conducted on a H-shaped steel beam, with aramid FRP sheets bonded to its flanges. The mid-span deflection and the strain from three points along AFRP sheets were recorded Test results exhibit that the increment of the load-carrying capacity with reference to a mid-span deflection level of 15 mm(1/125mm of the clear span) was equal to 9.4% and for the two layers case, an elastic stiffness increment is slightly higher than one layer case.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.37 no.5
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• pp.317-326
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• 2024

In this paper, compression molding-structural coupled analysis was proposed to accurately consider the effect of initial compression molding conditions on the mechanical behavior of short-fiber reinforced composite structures. To this end, local short-fiber orientations depending on the initial charge conditions were investigated using compression molding analysis, and a mean-field homogenization scheme was employed to efficiently derive equivalent orthotropic material properties determined by short-fiber orientations. Furthermore, based on the refined finite element model with short-fiber orientation, compression molding-structural coupled analysis precisely described the locally independent mechanical behavior induced by initial molding conditions. Consequently, it could be confirmed that the proposed analysis model provides a reasonable solution in the design process of short-fiber reinforced composite structures manufactured by compression molding.

• Composites Research
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• v.36 no.2
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• pp.117-125
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• 2023

This paper proposes a new finite element formulation based on enhanced first-order shear deformation theory including the transverse normal strain effect via the mixed formulation (EFSDTM-TN) for the effective thermo-mechanical analysis of laminated composite structures. The main objective of the EFSDTM-TN is to provide an accurate and efficient solution in describing the thermo-mechanical behavior of laminated composite structures by systematically establishing the relationship between two independent fields (displacement and transverse stress fields) via the mixed formulation. Another key feature is to consider the thermal strain effect without additional unknown variables by introducing a refined transverse displacement field. In the finite element formulation, an eight-node isoparametric plate element is newly developed to implement the advantage of the EFSDTM-TN. Numerical solutions for the thermo-mechanical behavior of laminated composite structures are compared with those available in the open literature to demonstrate the numerical performance of the proposed finite element model.

• Composites Research
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• v.29 no.6
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• pp.363-368
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• 2016

This study performed a nonlinear finite element crash analysis of guardrail structures using supports made of composite materials. In this study, we used a new [0/90/90/0] laminated Boron fiber composite for resisting the crash effects. Based on the improved ground-structure interaction model, appropriate ground properties to the support were determined. In particular, the complex crash mechanism of guardrails was studied using various parameters. The parametric studies are focused on the various effects of car crash on the structural performance and thickness of supports. The numerical results for various parameters are verified by comparing those using existing steel materials.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.19 no.7
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• pp.474-480
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• 2018

FRP is a new material that is lightweight, has high strength and high durability, and is emerging as a third construction material in many countries. The composite material panel targeted in this study was a curved member and is the most frequently used arch-shaped member of a structures, such as tunnels. Composite curved panels can be produced in high quality and large quantities through automation operations. On the other hand, the frequency of application is low, and the design criteria and experimental data are lacking. Therefore, this study examined the mechanical performance of the member unit first to verify its performance as structural members of the FRP curved panel. For this purpose, tensile, compression, and connection performance tests were carried out. The tensile tests showed greater tensile strength of specimens with larger curvature, and the compression tests showed that the composite section of a composite material has greater compressive strength than the concrete section. Finally, the test of the performance of the connection showed that the attachment performance of the connection was more than equal to that of the FRP composite material panel.

• Journal of the Society of Disaster Information
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• v.11 no.2
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• pp.235-243
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• 2015

The methods to improve the protection and explosion-proof performance of concrete structures include the backside reinforcement or concrete material property improvement and the addition of structural members or supports to increase the resistance performance, but they are inefficient in terms of economics and structural characteristics. This study is about the basic study on the fiber composite panel cover, and the nano-composite material and adhesive as the filler, to maximize the specific performance of each layer and the protection and explosion-proof performance as the composite panel component by improving the tensile strength, light weight, adhesion and fire-proof performances. The fiber composite panel cover (aramid-polyester ratios of 6:4 and 6.5:3.5) had a 2,348 MPa maximum tensile strength and a 1.8% maximum elongation. The filler that contained the nano-composite material and adhesive had a 4 MPa maximum tensile shear adhesive strength. In addition, the nano-composite filler was 30% lighter than the normal portland cement

• Proceedings of the Korean Society For Composite Materials Conference
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• 2002.10a
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• pp.228-232
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• 2002

본 연구에서는 다목적 실용위성 2호기에 적용된 금속 구조물 중 알루미늄 샌드위치 패널 구조인 탑재체 플랫폼과 튜브 스트럿(tube strut) 구조에 복합재료 응용기술을 적용하였다. 복합재료 구조로의 대체 설계에서도 관성하중 및 음향진동등과 같은 극심한 발사환경과 더불어 운용하게 될 우주 열환경을 고려하였다. 연구의 목적은 금속소재보다 비강도, 비강성이 우수한 복합재료를 위성 구조물에 사용함으로써 무게를 경량화함에 있다.

• Proceedings of the Korean Society of Dyers and Finishers Conference
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• 2011.11a
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• pp.51-51
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• 2011

Acetate 섬유는 고감성 제품의 대표적 핵심소재로서 실크와 같은 우아한 광택과 청량감을 주어 고가의 의류제품으로 사용되지만 편직 및 염색가공 공정이 까다롭고 비교적 저분자량의 분산염료로 염색되어 내열성, 염색견뢰도 및 물에 대한 형태안정성이 떨어진다. 특히, Acetate 편직물은 이태리나 일본 등 섬유선진국에서도 제조가 까다로운 기술적 난이도가 매우 높은 제품군이다. 반면 Tri-Acetate는 Acetate의 장점을 가지면서 내열성, 내세탁성, 원상회복력(resilience)등이 우수하여 기존 Acetate 시장의 고급제품 용도로의 전개가 가능할 뿐만 아니라 PET 등의 물성 및 형태가 다른 복수의 소재성분을 직물 사이에 공존시킴으로써 새로운 태, 기능, 외관, 광택의 부여가 가능하며 이를 활용한 차별화된 고부가가치 시장의 창출이 기대된다. Acetate와 Tri-Acetate 모두 셀룰로오스의 친수기가 아세틸화된 구조를 가지는 소수성 섬유로 분자구조가 치밀하여 분산염료로 염색된다. 그러나 일반적으로 Acetate 섬유의 경우 Acetate용 일반분산염료를 사용하여 저온상압염색을 하는 반면, Tri-Acetate의 경우 고온고압 분산염료를 사용하여 고온고압염색을 한다. PET와 Tri-Acetate 복합소재의 경우, 두 소재의 염색거동이 비슷하여 고온고압 분산염료로 염색이 가능하지만 T/P 복합소재에 상응하는 염색을 위해서는 복합소재를 구성하는 각각의 섬유소재에 적합한 염료의 선정 및 염색법의 개발이 필요하다. 본 연구에서는 Tri-Acetate 및 T/P 복합소재에 대한 염색최적조건을 규명하고자 염색온도별, 2종의 분산염료의 농도별 염색성, 염색시료의 인열강도 및 견뢰도를 측정하여 적정조건을 도출하였다.