• 국제학술발표논문집
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• The 9th International Conference on Construction Engineering and Project Management
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• pp.436-442
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• 2022

Hurricanes and tornadoes are the most destructive natural disasters in some central and southern states. Thus, storm shelters, which can provide emergency protections for low-rise building residents, are becoming popular nowadays. Both FEMA and ICC have published a series of manuals on storm shelter design. However, the authors found that the materials for related products in the market are heavyweight and hard to deliver and install; renovations are necessary. The authors' previous studies found that lightweight and high-performance composite materials can withstand extreme wind pressure, but some building codes are designated in wind-borne debris areas. In these areas, wind debris can reach greater than 100 mph speed. In addition, the impact damage on the composite materials is an increasing safety issue in many engineering fields; some can cause catastrophic results. Therefore, studying composite structures subjected to wind debris impact is essential. The finite element models are set up using the software Abaqus 2.0 to conduct the simulations to observe the impact resistance behavior of the carbon fiber composite sandwich panels. The selected wood debris models meet the FEMA requirements. The outcome of this study is then employed in future lab tests and compared with other material models.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
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• pp.121-124
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• 2005

This paper was about experimental test properties by mechnical joint of CF1263/Epoxy Al honeycomb panels. In case of mechanical joint using screw, nut shall be secured over than minimize third screw pitch. In case of insert backsheet for increase of joint force, increase weight for assemble by screw pitch. In case of insert backsheet with CF1263/Epoxy, predominant save weight and minimazer of displacement by tensile weight moreover predominant strength. In case of mechanical joint by rivet, rivet of Monobolt has over-hole in hole of CF1263/Epoxy but rivet of PROTRUDING has predominant of mechanical joint.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2002년도 봄 학술발표회 논문집
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• pp.105-110
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• 2002

In this study, a MMA modified polymer mortal sandwich panels was developed : Core was made with the MMA modified polymer mortar whose compressive strength was about 1020 kgf/cm$^2$, and both facings were made with the glass fiber reinforced plastics (GFRP). The results showed that the strain energies increased 20-33 times, respectively, as the thicknesses of facings increased from 1.50 to 2.76 mm with fixing the core thickness to constants (30-50 mm). On the other hand, these values showed a tendency of decrease as the core thickness increased regardless of thickness of facings. A set of basic data for the structural analysis could be provided by investigating the correlations, within the scope of this research, between the resisting moment and the thicknesses of core and facings.

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 1997년도 가을 학술발표회 논문집
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• pp.126-133
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• 1997

For each construction material used, there is certain theoretical limit in sizes. For tall building construction, the reduction in slab weight is the first step to take in order to break such size limits. In this paper, the feasibility of such objective is proven and given by numerical analysis result. For a typical building slab, both concrete and advanced composite sandwich panels are considered. The concrete slab is treated as a special orthotropic plate to obtain more accurate result. For each panel, the deflection under the dead and live loads is compared, since both tensile and compressive strengths of the composites are far more higher than those of concrete. All types of sandwich panels considered, except one case, have weights less than one tenth of that of reinforced concrete slab, with deflections less than that of the concrete slab. The cost analysis result and manufacturing methods will be reported later.

• 한국화재소방학회논문지
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• 제31권3호
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• pp.79-87
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• 2017

샌드위치패널은 양면이 철판이며 단열재로 접착된 특징을 갖는 건축자재로서 시공의 간편성, 자재비용의 경제성 등의 장점으로 공장 및 창고 구조물 등에 사용되고 있다. 그러나 샌드위치패널의 연속적 결합으로 시공되는 패널구조물은 패널과 패널이 연결되는 조인트 부위가 발생하게 된다 조인트부위는 화재시 철판의 용융과 변형으로 화염이 쉽게 유입되며 화재에 취약한 부위이다. 패널 내에 유입된 화염은 급속한 연소로 인해 화재확산을 유발하며 인명 및 재산피해를 발생시킨다. 본 연구에서는 샌드위치패널의 화재확산을 방지하기 위한 화재확산방지플레이트를 개발하였다. 이는 기존 선행연구에서 4면의 패널 접합면을 화재확산방지 재료로 시공하는 방법에서 접합면에 개발 플레이트를 끼우는 방식으로 시공이 용이하게 개선된 것으로서 패널과 패널이 결합되는 연결부에 자립하여 적용 가능하며 화염의 유입 및 화재확산을 방지하도록 고안하였다. 샌드위치패널 시험체에 대해 KS F ISO 13784-1 시험방법의 실물화재시험을 수행하였으며, 패널 연결부에 화재확산방지플레이트의 적용 유무에 따른 연소거동을 파악하고 그 효과를 측정하였다. 시험결과 패널 연결부에 화재확산방지플레이트를 삽입하는 것은 플래시오버의 지연, 시험체의 붕괴방지, 개구부의 온도상승을 지연시키는 것으로 측정되었으며, 효과적으로 패널구조물이 화재안전성을 확보할 수 있는 방안으로 확인되었다. 화재에 취약한 패널 연결부에 시공성과 경제성이 확보된 다양한 방식의 화재확산방지용 시공방법을 적용하는 것은 구조물의 화재안전성을 확보하는데 기여할 것으로 판단된다.

• Composites Research
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• 제19권1호
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• pp.9-14
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• 2006

본 연구는 KS F 2278 2003 (창호의 단열성 시험 방법)에 의하여 철도차량 및 버스의 내/외장재로 적용 가능한 카본/에폭시 스킨-알루미늄 하니콤 & 발사코어 샌드위치 판넬(두께 : 37mm), 카본/에폭시 스킨-알루미늄 하니콤 코어 샌드위치 판넬(두께 : 57mm, 단열재 포함) 및 카본/에폭시 스킨-알루미늄 하니콤 코어 샌드위치 판넬(두께 : 37mm)에 대한 열관류율 시험을 하였다. 또한 KS F2277 . 2002 (건축용 구성재의 단열성 측정방법-교정열상자법 및 보호열상자법)에 의하여 추가로 알루미늄 스킨-알류미늄 하니콤 샌드위치 판넬들 (두께 : 27mm, 35n1m)과 알루미늄 스킨-포밍 알루미늄 샌드위치 판넬 (두께27mm)에 대한 열관류율 시험을 수행하였다. 본 연구를 통해 면제와 심재사이에 열전달은 실제 단면적이 넓을수록 열관류율이 높았으며, 하이브리드형 복합재 일수록 단열성능이 우수함을 확인하였다.

• Structural Engineering and Mechanics
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• 제47권5호
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• pp.623-641
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• 2013

The fiber-reinforced polymer (FRP) composite panel, with the benefits of light weight, high strength, good corrosion resistance, and long-term durability, has been considered as one of the prosperous alternatives for structural retrofits and replacements. Although with these advantages, a further application of FRPs in bridge engineering may be restricted, and that is partly due to some unsatisfied thermal performance observed in recent studies. In this regard, Kansas Department of Transportation (DOT) conducted a field monitoring program on a bridge with glass FRP (GFRP) honeycomb hollow section sandwich panels. The temperatures of the panel surfaces and ambient air were measured from December 2002 to July 2004. In this paper, the temperature distributing behaviors of the panels are firstly demonstrated and discussed based on the field measurements. Then, a numerical modeling procedure of temperature fields is developed and verified. This model is capable of predicting the temperature distributions with the local environmental conditions and material's thermal properties. Finally, a parametric study is employed to examine the sensitivities of several temperature influencing factors, including the hollow section configurations, environmental conditions, and material properties.

• 한국항공우주학회지
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• 제38권8호
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• pp.798-805
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• 2010

전구조 소형 복합재 위성인 과학기술위성 3호가 국내 최초로 개발되었다. 과학기술위성 3호는 기존의 위성과 달리 알루미늄 프레임이 없는 구조로 되어있으며 알루미늄 코어에 적층복합재 스킨을 가진 샌드위치 패널의 조합으로 구성되었다. 이 복합재 패널의 결합으로 구성된 격자형태의 공간에 다수의 전장박스와 탑재체 및 장치들이 장착된다. 본 연구는 과학기술위성 3호의 랜덤진동 응답에 관한 연구이며 이를 위하여 FEA 해석과 시험이 수행 되었다. 진동시험 결과와 전산해석결과를 서로 상호 비교 검토함으로써 위성의 진동 특성을 규명하고 결과의 신뢰성을 검증하였다.

• Structural Engineering and Mechanics
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• 제68권6호
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• pp.721-733
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• 2018

The modal frequency responses of functionally graded (FG) sandwich doubly curved shell panels are investigated using a higher-order finite element formulation. The system of equations of the panel structure derived using Hamilton's principle for the evaluation of natural frequencies. The present shell panel model is discretised using the isoparametric Lagrangian element (nine nodes and nine degrees of freedom per node). An in-house MATLAB code is prepared using higher-order kinematics in association with the finite element scheme for the calculation of modal values. The stability of the opted numerical vibration frequency solutions for the various shell geometries i.e., single and doubly curved FG sandwich structure are proven via the convergence test. Further, close conformance of the finite element frequency solutions for the FG sandwich structures is found when compared with the published theoretical predictions (numerical, analytical and 3D elasticity solutions). Subsequently, appropriate numerical examples are solved pertaining to various design factors (curvature ratio, core-face thickness ratio, aspect ratio, support conditions, power-law index and sandwich symmetry type) those have the significant influence on the free vibration modal data of the FG sandwich curved structure.

• 한국소음진동공학회논문집
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• 제15권12호
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• pp.1361-1369
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• 2005

Based on a full layerwise displacement shell theory, the nitration and damping characteristics of cylindrical sandwiched panels with viscoelastic layers are investigated. The transverse shear deformation and the normal strain of the cylindrical hybrid panels are fully taken into account for the structural damping modelling. The present finite element model Is formulated by using Hamilton's virtual work principle and the cylindrical curvature of hybrid panels is exactly modeled. Modal loss factors and frequency response functions are analyzed for various structural parameters of cylindrical sandwich panels. Present results show that the full layerwise finite element method can accurately predict the vibration and damping characteristics of the cylindrical hybrid panels with surface damping treatments and constrained layer damping.