• 한국응용곤충학회지
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• 제31권4호
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• pp.509-515
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• 1992

한국산 국화과(초롱꽃목) 잡초를 가해하는 곤충조사 결과, 12속 16종의 잡초에서 5목 17과 43속 45종의 곤충이 채집되었다. 그 중 노린재목과 딱정벌레목의 각각 13종으로 가장 많이 채집되었으며, 중요한 잡초가해 곤충은 진딧물과 잎벌레였다. 식물별로는 참쑥에서 15속 16종의 가장 많은 곤충이 채집되었으며 그외 엉겅퀴와 망초에서도 많은 곤충이 기록되었다. 가해능력이 우수하였던 곤충은 엉겅퀴의 우엉수염진딧물과 엉겅퀴가는잎말이나방이었고 쑥류에서는 쑥민들진딧물외에 쑥잎벌레, 긴발벼룩잎벌레, 금록색잎벌레, Hamushia konishili 잎벌레였다. 기주특이성이 있었던 곤충은 진딧물류와 잎벌레류였으며 쑥류와 망초의 꽃에서 빈번하게 채집되었던 노린재류의 기능은 확인할 수 없었다.

• 한국수소및신에너지학회논문집
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• 제23권3호
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• pp.243-249
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• 2012

A lightweight 200W direct methanol fuel cell (DMFC) stack is designed and fabricated to power a small scale Unmanned Aerial Vehicle (UAV). The DMFC stack consists of 33-cells in which membrane-electrode assemblies (MEAs) having an active area of 88 $cm^2$ are sandwiched with lightweight composite bipolar plates. The total stack weight is around 3.485 kg and stack performance is tested under various methanol feed concentrations. The DMFC stack delivers a maximum power of 248 W at 13.2 V and $71.3^{\circ}C$ under methanol feed concentration of 1.2 M. In addition, the voltage of individual cell in the 33-cell stack is measured at various current levels to ensure the stability of DMFC stack operations. The cell voltage distribution data exhibit the maximum cell voltage deviation of 28 mV at 15 A and hence the uniformity of cell voltages is acceptable. These results clearly demonstrate that DMFC technology becomes a potential candidate for small-scale UAV applications.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2002년도 추계종합학술대회
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• pp.779-783
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• 2002

변성기용 절연 재료로 사용되는 에폭시 수지를 시료로 선정, 5종의 배합비로 제작한 시편에 대해 절연 파괴 실험을 하며, 얻어진 데이터를 와이블 분포식을 이용, 경년 열화(經年劣和) 데이터의 통계 처리 방법을 제안하였다. 경화제 비율이 증가하면 에폭시 경화물의 에스터화로 인해 가교 밀도가 증가함으로써 저온에서의 파괴 강도가 높아졌으며, 유리 전이 온도(Tg) 영역인 11$0^{\circ}C$ 부근에서는 분자 운동이 활발해짐으로써 급격히 파괴 강도가 저하하였다. 또한, 충진제를 첨가한 경우 접합 계면에 전자가 가속되어 전반적인 파괴 강도는 무충진에 비해 낮게 나타났으며, 실란 처리를 한 경우에는 계면 접합 상태가 개선되어 충진제만을 첨가한 시료보다 좋은 절연성을 나타냈다. 와이블 분포의 분석으로부터 기기 절연의 허용 파괴 확률을 0.1% 이하로 낮추기 위해서는 허용인가 전계값이 21.5 MV/cm 이하가 되어야함을 알 수 있었다.

• Steel and Composite Structures
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• 제1권4호
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• pp.427-440
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• 2001

The growing use of unprotected or partially protected steelwork in buildings has caused a lively debate regarding the safety of this form of construction. A good deal of recent research has indicated that steel members have a substantial inherent ability to resist fire so that additional fire protection can be either reduced or eliminated completely. A performance based philosophy also extends the study into the effect of structural continuity and the performance of the whole structural totality. As part of the structural system, thermal expansion during the heating phase or contraction during the cooling phase in most beams is likely to be restrained by adjacent parts of the whole system or sub-frame assembly due to compartmentation. This has not been properly addressed before. This paper describes an experimental programme in which unprotected steel beams were tested under load while it is restrained between two columns and additional horizontal restraints with particular concern on the effect of catenary action in the beams when subjected to large deflection at very high temperature. This paper also presents a three-dimensional mathematical modelling, based on the finite element method, of the series of fire tests on the part-frame. The complete analysis starts with an evaluation of temperature distribution in the structure at various time levels. It is followed by a detail 3-D finite element analysis on its structural response as a result of the changing temperature distribution. The principal part of the analysis makes use of an existing finite element package FEAST. The effect of columns being fire-protected and the beam being axially restrained has been modelled adequately in terms of their thermal and structural responses. The consequence of the beam being restrained is that the axial force in the restrained beam starts as a compression, which increases gradually up to a point when the material has deteriorated to such a level that the beam deflects excessively. The axial compression force drops rapidly and changes into a tension force leading to a catenary action, which slows down the beam deflection from running away. Design engineers will be benefited with the consideration of the catenary action.

• Steel and Composite Structures
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• 제4권6호
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• pp.471-487
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• 2004

Modular steel scaffolds are commonly used as supporting scaffolds in building construction, and traditionally, the load carrying capacities of these scaffolds are obtained from limited full-scale tests with little rational design. Structural failure of these scaffolds occurs from time to time due to inadequate design, poor installation and over-loads on sites. In general, multi-storey modular steel scaffolds are very slender structures which exhibit significant non-linear behaviour. Hence, secondary moments due to both $P-{\delta}$ and $P-{\Delta}$ effects should be properly accounted for in the non-linear analyses. Moreover, while the structural behaviour of these scaffolds is known to be very sensitive to the types and the magnitudes of restraints provided from attached members and supports, yet it is always difficult to quantify these restraints in either test or practical conditions. The problem is further complicated due to the presence of initial geometrical imperfections in the scaffolds, including both member out-of-straightness and storey out-of-plumbness, and hence, initial geometrical imperfections should be carefully incorporated. This paper presents an extensive numerical study on three different approaches in analyzing and designing multi-storey modular steel scaffolds, namely, a) Eigenmode Imperfection Approach, b) Notional Load Approach, and c) Critical Load Approach. It should be noted that the three approaches adopt different ways to allow for the non-linear behaviour of the scaffolds in the presence of initial geometrical imperfections. Moreover, their suitability and accuracy in predicting the structural behaviour of modular steel scaffolds are discussed and compared thoroughly. The study aims to develop a simplified and yet reliable design approach for safe prediction on the load carrying capacities of multi-storey modular steel scaffolds, so that engineers can ensure safe and effective use of these scaffolds in building construction.

• Steel and Composite Structures
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• 제10권3호
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• pp.207-222
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• 2010

Fire incident in buildings is common, so the fire safety design of the framed structure is imperative, especially for the unprotected or partly protected bare steel frames. However, software for structural fire analysis is not widely available. As a result, the performance-based structural fire design is urged on the basis of using user-friendly and conventional nonlinear computer analysis programs so that engineers do not need to acquire new structural analysis software for structural fire analysis and design. The tool is desired to have the capacity of simulating the different fire scenarios and associated detrimental effects efficiently, which includes second-order P-D and P-d effects and material yielding. Also the nonlinear behaviour of large-scale structure becomes complicated when under fire, and thus its simulation relies on an efficient and effective numerical analysis to cope with intricate nonlinear effects due to fire. To this end, the present fire study utilizes a second-order elastic/plastic analysis software NIDA to predict structural behaviour of bare steel framed structures at elevated temperatures. This fire study considers thermal expansion and material degradation due to heating. Degradation of material strength with increasing temperature is included by a set of temperature-stress-strain curves according to BS5950 Part 8 mainly, which implicitly allows for creep deformation. This finite element stiffness formulation of beam-column elements is derived from the fifth-order PEP element which facilitates the computer modeling by one member per element. The Newton-Raphson method is used in the nonlinear solution procedure in order to trace the nonlinear equilibrium path at specified elevated temperatures. Several numerical and experimental verifications of framed structures are presented and compared against solutions in literature. The proposed method permits engineers to adopt the performance-based structural fire analysis and design using typical second-order nonlinear structural analysis software.

• Steel and Composite Structures
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• 제33권5호
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• pp.717-727
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• 2019

This paper is motivated by the lack of studies in the technical literature concerning to vibration analysis of a single-layered graphene sheet (SLGS) with corner cutout based on the nonlocal elasticity model framework of classical Kirchhoff thin plate. An isogeometric analysis (IGA) based upon non-uniform rational B-spline (NURBS) is employed for approximation of the L-shape SLGS deflection field. Trimming technique is employed to create the cutout in geometry of L-shape plate. The L-shape plate is assumed to be Free (F) in the straight edges of cutout while any arbitrary boundary conditions are applied to the other four straight edges including Simply supported (S), Clamped (C) and Free (F). The Numerical studies are carried out to express the influences of the nonlocal parameter, cutout dimensions, boundary conditions and mode numbers on the variations of the natural frequencies of SLGS. It is precisely shown that these parameters have considerable effects on the free vibration behavior of the system. In addition, numerical results are validated and compared with those achieved using other analysis, where an excellent agreement is found. The effectiveness and the accuracy of the present IGA approach have been demonstrated and it is shown that the IGA is efficient, robust and accurate in terms of nanoplate problems. This study serves as a benchmark for assessing the validity of numerical methods used to analyze the single-layered graphene sheet with corner cutout.

• Elastomers and Composites
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• 제44권1호
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• pp.47-54
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• 2009

본 연구에서는 다양한 종류의 보강제를 혼합한 EPDM 컴파운드의 원적외선에 의한 가교 반응을 조사하였다. 보강제가 원적외선에 의한 가교 반응에 미치는 영향을 평가하기 위하여 컴파운드의 발열 온도 및 DSC 분석에 의한 가교도를 측정하였으며, 특히 원적외선에 의한 가교 특성을 비교하기 위하여 동일 조건에서 열풍에 의한 가교 반응을 조사하였다. 원적외선 가교 조건에서 카본블랙을 혼합한 EPDM 컴파운드는 입자크기가 증가함에 따라 열전도도가 증가하며 이에 따라 원적외선에 의한 가교도 역시 증가하였으나, 열풍에 의한 가교도의 변화에는 거의 영향을 주지 못하였다. 보강제 종류에 따른 원적외선 가교 특성 평가 결과, 열전도도가 높은 아세틸렌 블랙을 함유한 컴파운드의 가교도가 가장 높게 나타났으며, 열전도도가 유사한 카본블랙 및 침강실리카의 경우 상대적으로 원적외선 흡수 특성이 우수한 침강실리카 배합 컴파운드의 경우 원적외선에 의한 가교도가 높게 나타났다.

• The Journal of Advanced Prosthodontics
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• 제5권2호
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• pp.98-103
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• 2013

PURPOSE. To evaluate the effects of hydrofluoric acid etching and Er,Cr:YSGG laser irradiation on the shear bond strength of resin cement to lithium disilicate ceramic. MATERIALS AND METHODS. Fifty-five ceramic blocks ($5mm{\times}5mm{\times}2mm$) were fabricated and embedded in acrylic resin. Their surfaces were finished with 1000-grit silicon carbide paper. The blocks were assigned to five groups: 1) 9.5% hydrofluoric-acid etching for 60 s; 2-4), 1.5-, 2.5-, and 6-W Er,Cr:YSGG laser applications for 60 seconds, respectively; and 5) no treatment (control). One specimen from each group was examined using scanning electron microscopy. Ceramic primer (Rely X ceramic primer) and adhesive (Adper Single Bond) were applied to the ceramic surfaces, followed by resin cement to bond the composite cylinders, and light curing. Bonded specimens were stored in distilled water at $37^{\circ}C$ for 24 hours. Shear bond strengths were determined by a universal testing machine at 1 mm/min crosshead speed. Data were analyzed using Kruskal-Wallis and Mann-Whitney U-tests (${\alpha}$=0.05). RESULTS. Adhesion was significantly stronger in Group 2 ($3.88{\pm}1.94$ MPa) and Group 3 ($3.65{\pm}1.87$ MPa) than in Control group ($1.95{\pm}1.06$ MPa), in which bonding values were lowest (P<.01). No significant difference was observed between Group 4 ($3.59{\pm}1.19$ MPa) and Control group. Shear bond strength was highest in Group 1 ($8.42{\pm}1.86$ MPa; P<.01). CONCLUSION. Er,Cr:YSGG laser irradiation at 1.5 and 2.5 W increased shear bond strengths between ceramic and resin cement compared with untreated ceramic surfaces. Irradiation at 6 W may not be an efficient ceramic surface treatment technique.

• 항공우주기술
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• 제1권1호
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• pp.8-27
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• 2002

본 연구에서는 현재 개발중에 있는 복합재료 선미익 항공기의 날개에 작용하는 하중해석을 수행하였다. 중량, 공력계수, 구조설계속도, 하중 등을 계산하기 위해 사용된 Tool은 Excel에서 운용되는 Visual Basic 프로그램으로 계산에 많은 도움을 주었다. 하중해석에 기본적으로 요구되는 항공기의 형상치수, 부품의 종류 및 중량 그리고 좌표계 등은 Catia 모델링, 실제측정 또는 재료밀도 값 등을 이용해 구하였으며, 이들 자료를 통하여 항공기의 중량, 무게중심, 관성모멘트, 구조설계속도, 날개의 하중분포, 힘과 모멘트 등을 계산하였다. 또한 항공기의 날개 및 동체의 임계하중 조건을 선정하는데 필수적인 항공기의 V-n 선도를 도시하였으며, 이 V-n 선도는 항공기의 최대중량 2,573 파운드 및 해면고도조건에서 설계속도 $V_A$, $V_C$, $V_D$ 및 하중계수 +3.8G, -1.52G에 대한 비행범위를 제시하고 있다. 앞으로는 V-n 선도로부터 선정된 임계하중을 이용하여 해석된 동체 및 날개에 대한 하중을 제시하고자 한다.