• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2005년도 춘계학술대회 논문집
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• pp.168-173
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• 2005

Composite material is combined with two or more chemical ingredient and different components. FRP has been widely used for the structure of aircraft, ships, automobiles, sporting goods and other machines because of their high specific strength, high specific stiffness and excellent fatigue strength. Recently, the development of machine tool and cutting tool greatly relies on high speed process to satisfy high precision, high efficient machining, shortened process time to maximize material removal rate (MRR) through high cutting speed and feed speed. The research molded CFRP, GFRP as stacking sequence methods of two direction (orientation angle $0^{\circ}\;and\;0^{\circ}/9^{\circ}$) hand lay-up, drilled molded plates using cemented carbide drill and examined chip shapes, surface roughness properties.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2002년도 봄 학술발표회 논문집
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• pp.489-496
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• 2002

The lateral buckling of a laminated composite beam is studied. A general analytical model applicable to the lateral buckling of a composite beam subjected to various types of loadings is derived. This model is based on the classical lamination theory, and accounts for the material coupling for arbitrary laminate stacking sequence configuration and various boundary conditions. The effects of the location of applied loading on the buckling capacity are also included in the analysis. A displace-based one-dimensional finite element model is developed to predict critical loads and corresponding buckling modes for a thin-walled composite beam with arbitrary boundary conditions. Numerical results are obtained for thin-walled composites under central point load, uniformly distributed load, and pure bending with angle-ply and laminates. The effects of fiber orientation location of applied load, and types of loads on the critical buckling loads are parametrically studied.

• 한국전산구조공학회논문집
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• 제12권4호
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• pp.599-606
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• 1999

복합 적층 판과 보강 재를 설치한 보강된 복합 적층 패널의 좌굴을 고려한 설계에서, 좌굴이 항상 구조물의 최종 파손을 의미하는 것은 아니므로 이들의 좌굴 및 좌굴 후 거동에 대한 정확한 이해와 연구가 필요하다. 본 연구에서는 유한요소 법을 이용하여 적층 메커니즘과 섬유 배향각, 적층 순서 등이 복합 적층 판과 보강된 복합 적층 패널의 좌굴 및 좌굴 후 거동에 미치는 영향을 체계적으로 해석하였고, 각 변수에 따른 좌굴 및 좌굴 후 거동 특성을 분석하였다.

• 한국생산제조학회지
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• 제20권1호
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• pp.47-52
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• 2011

It is well known that stiffness of composites depends on layup sequence of CFRP(carbon fiber reinforced plastics) laminates because the layup of composite laminates influences their properties. Ultrasonic NDE of composite laminates is often based on the backwall echoes of the sample. A pair of such transducers was mounted in a holder in a nose-to-nose fashion to be used as a scanning probe on composites. Miniature potted angle beam transducers were used (Rayleigh waves in steel) on solid laminates of composites. Experiments were performed to understand the behavior of the transducers and the nature of the waves generated in the composite (mode, wave speed, angle of refraction). C-scan images of flaws and impact damage were then produced by combining the pitch-catch probe with a portable manual scanner known as the Generic Scanner ("GenScan"). The pitch-catch signal was found to be more sensitive than normal incidence backwall echo of longitudinal wave to fiber orientation of the CFRP composites, including low level porosity, ply waviness, and cracks. Therefore, it is found that the experimentally Rayleigh wave variation of pitch-catch ultrasonic signal was consistent with numerical results and one-side ultrasonic measurement might be very useful to detect the defects.

• 대한토목학회논문집
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• 제29권4A호
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• pp.267-279
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• 2009

이 논문에서는 초고강도 강섬유보강 철근콘크리트 구조물의 단조증가 하중에서 비선형 해석모델을 소개하고 있다. 일반콘크리트에 비해 압축강도와 인장강도가 증가한 초고강도 강섬유보강 콘크리트는 그 거동이 일반콘크리트와 다른 특성을 가지고 있다. 초고강도 강섬유보강 철근콘크리트 구조물에 대한 비선형 해석을 하기에 앞서 실험결과를 이용하여 압축영역에서 응력-변형률, 관계를 회귀분석을 통하여 유추하였고, 초고강도 강섬유보강 철근콘크리트 구조물 거동의 정확한 예측을 위하여 등가일축 응력-변형률 관계를 이용하였다. 또한 균열의 진전에 따른 균열각을 모사하기 위해 평면응력 요소를 이용하였고, 분산철근모델을 이용하여 해석에 적용하였다. 한편, 초고강도 강섬유보강 철근콘크리트의 인장영역에서 응력-변형률 관계를 정의하기 위해 철근과 콘크리트의 부착응력-부착슬립 관계와 강섬유의 영향 등을 고려한 새로운 인장강화 모델을 제안하고 있다. 끝으로 제안된 알고리즘과 응력-변형률 관계 및 인장강화 모델을 한국건설기술연구원에서 실험한 초고강도 강섬유보강 철근콘크리트 부재에 대한 수치해석을 수행하여 실험결과와 비교, 평가하였다.

• 한국재료학회지
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• 제4권2호
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• pp.194-205
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• 1994

본 연구에서는 원료 석탄 핏치와 흑연화성이 우수한 THF 가용성분만을 추출한 핏치 결합재에 8H/Satin woven fabric 프리프레그 및 고탄성 및 고강도계 연속 탄소섬유 등을 보강하여 가압열성형법으로 green body 를 제조한 다음 탄화, 함침, 재탄화 및 흑연화 공정을 거쳐 열적 미 기계적물성이 우수한 CFRC를 제조하였으며, 주사전자현미경, 편광현미경, X선회절분석,열중량분석, 굴곡강도, 굴곡탄성률, 충간전단강도 등을 시험하였다. THFSP결합재를 $2300^{\circ}C$까지 열처리 한 다음 X선회절분석을 한 결과, 결정성이 가장 우수하여 (002) 면에서 $C_0$/2인 값이 3.380$\AA$였으며, 2$\theta$값도 $26.276^{\circ}$로 천연흑연의 Bragg angle에 거의 접근하였으며 공기산화 반응특성을 시험하기 위하여 등온 열중량분석을 한 결과 $2300^{\circ}C$까지 흑연화 한 THFSP결합재가 산화에 대하여 가장 우수한 저항성을 나타내었다. 섬유용적률이 증가됨에 따라 65~70%까지는 기계적 물성이 중가하는 경향을 보였지만 그이상 섬유가 보강된 CFRC는 결합재의 부족으로 인하여 오히려 기계적 물성이 감소하였다. 또한 굴곡강도 시험후 주사전자현미경으로 파괴 단면을 관찰한 결과 THFSP결합재가 흑연화성이 우수하여 파괴시 결합재가 외력에 대한 흡수가 양호하여 보강재의 파괴를 억제했기 때문에 기계적 물성도 우수하게 나타났다.

• Advances in aircraft and spacecraft science
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• 제3권4호
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• pp.427-445
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• 2016

Star sensors are the attitude estimation sensors of the satellite orbiting in its path. It gives information to the control station on the earth about where the satellite is heading towards. It captures the images of a predetermined reference star. By comparing this image with that of the one captured from the earth, exact position of the satellite is determined. In the process of imaging, stray lights are eliminated from reaching the optic lens by the mechanical enclosures of the star sensors called Baffles. Research in space domain in the last few years is mainly focused on increased payload capacity and reduction in launch cost. In this paper, a star sensor baffle made of Aluminium is considered for the study. In order to minimize the component weight, material wastage and to improve the structural performance, an alternate material to Aluminium is investigated. Carbon Fiber Reinforced Polymer is found to be a better substitute in this regard. Design optimisation studies are carried out by adopting suitable design modifications like implementing an additional L-shaped flange, Upward flange projections, downward flange projections etc. A better configuration of the baffle, satisfying the design requirements and achieving manufacturing feasibility is attained. Geometrical modeling of the baffle is done by using UNIGRAPHICS-Nx7.5(R). Structural behavior of the baffle is analysed by FE analysis such as normal mode analysis, linear static analysis, and linear buckling analysis using MSC/PATRAN(R), MSC-NASTRAN(R) as the solver to validate the stiffness, strength and stability requirements respectively. Effect of the layup sequence and the fiber orientation angle of the composite layup on the stiffness are also studied.

• Fibers and Polymers
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• 제5권2호
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• pp.122-127
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• 2004

In this study, we evaluated the effect of the molecular weight of the polymer on electrospun poly(ethylene terephthalate) (PET) nonwovens, and their mechanical properties as a function of the linear velocity of drum surface. Polymer solutions and electrospun PET nonwovens were characterized by means of viscometer, tensiometer, scanning electron microscope(SEM), wide angle X-ray diffraction measurement (WAXD) and universal testing machine (UTM). By keeping the uniform solution viscosity, regardless of molecular weight differences, electrospun PET nonwovens with similar average diameter could be obtained. In addition, the mechanical properties of the electrospun PET nonwovens were strongly dependent on the linear velocity of drum surface. From the results of the WAXD scan, it was found that the polymer took on a particular molecular orientation when the linear velocity of drum surface was increased. The peaks became more definite and apparent, evolving from an amorphous pattern at 0 m/min to peaks and signifying the presence of crystallinity at 45 m/min.

• Structural Engineering and Mechanics
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• 제75권2호
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• pp.247-269
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• 2020

A finite strip formulation was developed for buckling and free vibration analysis of laminated composite plates based on different shear deformation plate theories. The different shear deformation theories such as Zigzag higher order, Refined Plate Theory (RPT) and other higher order plate theories by variation of transverse shear strains through plate thickness in the parabolic form, sine and exponential were adopted here. The two loaded opposite edges of the plate were assumed to be simply supported and remaining edges were assumed to have arbitrary boundary conditions. The polynomial shape functions are applied to assess the in-plane and out-of-plane deflection and rotation of the normal cross-section of plates in the transverse direction. The finite strip procedure based on the virtual work principle was applied to derive the stiffness, geometric and mass matrices. Numerical results were obtained based on various shear deformation plate theories to verify the proposed formulation. The effects of length to thickness ratios, modulus ratios, boundary conditions, the number of layers and fiber orientation of cross-ply and angle-ply laminates were determined. The additional results on the same effects in the interaction of biaxial in-plane loadings on the critical buckling load were determined as well.

• 한국생산제조학회지
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• 제21권6호
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• pp.865-870
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• 2012

CFRP of the advanced composite materials as structure materials for vehicles has a widely application in lightweight structural materials of air planes, ships and automobiles because of high strength and stiffness compared with conventional materials. This study is to investigate the energy absorption characteristics and collapse mode of CFRP single and double hat shaped structural member under the axial static collapse test. The CFRP single and double hat shaped structural members stacked at different angles (${\pm}15^{\circ}$, ${\pm}45^{\circ}$, ${\pm}90^{\circ}$, $90^{\circ}/0^{\circ}$ and $0^{\circ}/90^{\circ}$ where the direction on $0^{\circ}$ coincides with the axis of the member). The axial static collapse tests were carried out for each member. Collapse mode and energy absorption characteristics of the each member were analyzed.