• 한국철도학회:학술대회논문집
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• 한국철도학회 2010년도 춘계학술대회 논문집
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• pp.1464-1469
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• 2010

In this paper, the dynamic stability evaluation of special bridge for high speed railway under ground excitation is performed. The mass, damping, stiffness matrices of bridge are derived from the modal frequencies and mode shape vectors which can be obtained by commercial program. And the high speed train is modeled as multi-single d.o.f models for the sake of vehicle-bridge interaction analysis. In the vehicle-bridge interaction analysis, the vertical directional interaction is only considered. As a numerical example, the 3 span Extradosed bridge which is expected to be installed in Ho-Nam high speed railroad is considered. The analysis results show that the example bridge satisfies the criteria of dynamic stability.

• 한국전자통신학회논문지
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• 제11권3호
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• pp.263-270
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• 2016

본 논문에서는 변형된 항아리형 패치안테나를 사용하여 초 광대역 안테나를 구현하였다. 설계한 패치안테나의 물리적 길이와 홈(노치)를 광대역 특성 조건으로 최적화시켰으며, $10mm{\times}21.8mm$크기로 설계된 변형된 항아리형 패치안테나를 제작하였다. 설계된 최적화 패치안테나의 표면 전류분포를 분석하고 초 광대역 특성 조건을 만족함을 확인하였다. 실험 결과 제작된 초 광대역 패치안테나의 입력반사손실은 -10 dB 이하로 전압정재파비 역시 2 이하의 특성을 나타내었으며, 3.1~10.6 GHz 대역에서 약 1~3 dBi 이득범위를 나타내었다. 이와 같은 실험결과는 초 광대역 통신시스템에 활용이 가능할 것으로 판단된다.

• 대한치과보철학회지
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• 제35권4호
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• pp.719-741
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• 1997

This study was undertaken to compare by Atomic Force Microscope the effects of various finishing and polishing instruments on surface roughness of filling and veneering composite resins. Seven composite resins were studied : Silux Plus (3M Dental Products, U.S.A.), Charisma (Heraeus Kulzer, Germany), Prisma THP (L.D.Caulk, Dentsply, U.S.A.), Photoclearfil (Kuraray, Japan), Cesead (Kuraray, Japan), Thermoresin LC (GC, Japan), Artglass (Heraeus Kulzer, Germany). Samples were placed and polymerized in holes (2mm thick and 8.5mm in diameter) machined in Teflon mold under glass plate, ensuring excess of material and moulded to shape with polyester matrix strip. Except control group (Polyester matrix strip), all experimental groups were finished and polishied under manufacturer's instructions. The finishing and polishing procedure were : carbide bur (E.T carbide set 4159, Komet, Germany), diamond bur (composite resin polishing bur set, GC, Japan), aluminum-oxide disc (Sof-Lex Pop-On, 3M Dental Products, U.S.A.), diamond-particle disc (Dia-Finish, Renfert Germany), white stone bur & rubber point( composite finishing kit, EDENTA, Swiss), respectively. Each specimens were evaluated for the surface roughness with Atomic Force Microscope (AutoProbe CP, Park Scientific Instruments, U.S.A.) under contact mode and constant height mode. The results as follows : 1. Except Thermoresin LC, all experimental composite resin groups showed more rougher than control group after finishing and polishing(p<0.1). 2. A surface as smooth as control group was obtained by $Al_{2}O_{3}$ disc all filling composite resin groups except Charisma and all veneering composite resin groups except Thermoresin LC(p<0.05). 3. In case of Thermoresin LC, there were no statistically significant differences before and after finishing and polishing(p>0.1). 4. Carbide bur, diamond bur showed rough surfaces in all composite resin groups, so these were inappropriate for the final polishing instruments.

• 한국전자파학회논문지
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• 제12권1호
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• pp.18-26
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• 2001

본 논문에서는 압전체를 전기기계 압전파동방정식과 경계조건을 이용하여 고유치 제로 정식화하고, 3차원 유한요소법을 적용하여 초고주파 대역에서 동작하는 압전박막공진기의 공진모드 및 공진특성을 공진기의 입력 임피던스를 통하여 해석하였다. 이를 통하여 1차원 해석에서는 불가능하였던 공진기의 전극형상과 상, 하부 전극의 비대칭 구조에 따른 공진특성과 스퓨리어스특성을 추출하였다. 본 논문에서 제안한 방법으로 계산된 공진주파수를 Mason 등기모델 해석결과 및 실제 제작한 ZnO 압전박막공진기의 공진 특성과 비교한 결과 정확하게 일치함을 확인하였다. 또한 두께진동모드로 동작하기 위한 최적의 길이와 두께의 비가 20 : 1이고 최소한의 길이와 두께의 비가 5:1 이상임을 알 수 있었다.

• 한국전자파학회논문지
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• 제20권10호
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• pp.1031-1041
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• 2009

본 논문에서는 다중 대역에서 매크로-마이크로 주파수 튜닝이 가능한 소형의 패치 모노폴 안테나를 소개하였다. 제안된 재구성 안테나는 PCB 기판(FR-4: $\varepsilon_r=4.4$ and tan $\delta=0.02$) 위에 미앤더(meander) 형태의 안테나로 설계하였고, Wibro(2.3~2.4 GHz)와 WLAN a/b(2.4~2.5 GHz/5.15~5.35 GHz)대역에서 일정한 이득을 유지하면서 각각의 서비스 대역에서 동작한다. 두 개의 다이오드, 핀 다이오드와 버렉터 다이오드가 주파수 튜닝을 위해 안테나 상에 내장되었으며, 핀 다이오드는 2 GHz와 5 GHz의 대역을 스위칭(매크로 튜닝)하기 위해 사용되었으며, 버렉터 다이오드는 2.3~2.5 GHz와 5.15~5.35 GHz의 서비스 대역 내 미세 주파수 튜닝(마이크로 튜닝)을 위하여 사용되었다. 또한, 두 주파수 대역(2 GHz와 5 GHz) 사이에서의 불요 공진(spurious resonance)은 미앤더(meander) 사이의 갭을 조정하여 제거되었다. 안테나는 각각의 서비스 대역에서 2 dBi 이상의 일정한 이득을 보인다. 제안된 안테나의 측정 결과는 매크로-마이크로 주파수 튜닝 기술이 재구성 가능한 다중 대역 다중 모드(Multi-Mode Multi-Band: MMMB) 무선 통신 시스템에서 유용하게 사용될 수 있음을 보여준다.

• 한국결정성장학회지
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• 제18권1호
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• pp.10-14
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• 2008

GaN nanowires는 수평 VPE법으로 합성 되었다. 본 실험에서는 source와 기판과의 거리가 합성된 GaN nanowires의 형상에 미치는 영향에 대하여 실험하였다. GaN nanowires는 $950^{\circ}C$ 온도에서 Ar 과 $NH_3$ 가스가 각각 1000, 50 sccm 의 유량에서 합성되었다. 합성된 GaN nanowires의 단면형태는 삼각형의 모양을 가졌으며, GaN nanowires의 길이는 200에서 500 nm 정도 였다. 합성된 GaN nanowires의 모양은 FESEM 으로 확인하였고, XRD 분석을 통하여 그 구조가 wurzite 구조인 것을 확인하였다. 또한, HRTEM 사진과 SAED 패턴을 통하여 합성된 GaN nanowires의 표면과 구조를 분석하였다. 성장된 GaN nanowires의 광학적 특성은 PL분석을 통하여 이루어졌다.

• Macromolecular Research
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• 제8권1호
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• pp.12-18
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• 2000

Six aromatic polyesters with ether-linkages were prepared from 4,4'-oxybis(benzoic acid) and naphthalenediol (ND) isomers which were 1,4-, 1,5-, 1,6-, 2,3-, 2,6- and 2,7-derivatives. The solution viscosity numbers ranged from 0.23 to 0.65 dL/g. The glass transition temperatures ranged from 142 to 179$\^{C}$. The initial decomposition temperatures were all above 400$\^{C}$, and the residue weights at 600$\^{C}$ were in the range of 50-64%. Only the polyesters derived from 1,5- and 2,6-NDs, which have a linear linking mode, were found to be semicrystalline and could form thermotropically nematic phase. Multiple melting phenomena and annealing of the polyester derived from 1,5-ND and related polymers are described. The experimental results show that the polyester derived from 1,4-ND of linear shape was amorphous and non-liquid crystalline. Particularly, the polyester derived from 2,3-ND could form a smectic mesophase as banana-shaped molecules, and this is ascribed to the C/sub_2v/ symmetry where highly kinked molecules are packed in the same direction.

• 수산해양기술연구
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• 제48권4호
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• pp.487-494
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• 2012

Acoustical backscattering characteristics of Japanese anchovy can be estimated by Kirchhoffray mode model (KRM model) due to estimate exact body and swim-bladder shape of the fish, the samples were rapidly frozen by dry-ice and alcohol. X-ray photos for ventral and lateral direction for 6 samples were taken and the 3D coordinates of the body swim-bladder were estimated by digitizing from the photos. The angles between the axis of body and swim-bladder were about $9^{\circ}$ at 38kHz and $7^{\circ}$ at 120kHz, 200kHz. General formula of TS and BL estimated were < $TS_{38kHz}$ >=20logBL-67.3, < $TS_{120kHz}$ >=20logBL-66.6, < $TS_{200kHz}$ >=20logBL-67.0. As a result, we confirmed KRM model is very useful to estimate TS (Target Strength) for design of experiment and it also can be applied to estimate the abundance of Japanese anchovy distributed by 2 frequency difference method in the survey area.

• 한국진공학회:학술대회논문집
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• 한국진공학회 2015년도 제49회 하계 정기학술대회 초록집
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• pp.60-60
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• 2015

Nanosheets of graphene and related 2D materials have attracted much attention due to excellent physical, chemical and mechanical properties. Single-layer graphene (SLG) was first synthesized by Blakely et al in 1974 [1]. Following his achievements, we initiated the growth and characterization of graphene and h-BN on metal substrates using surface segregation and precipitation in 1980s [2,3]. There are three important steps for nanosheet growth; surface segregation of dopants, surface reaction for monolayer phase, and subsequent 3-D growth (surface precipitation). Surface phase transition was clearly demonstrated on C-doped Ni(111) by in situ XPS at elevated temperatures [4]. The growth mode was clarified by inelastic background analysis [5]. The surface segregation approach has been applied to C-doped Pt(111) and Pd(111), and controllable growth of SLG has been demonstrated successfully [6]. Recently we proposed a promising method for producing SLG fully covering an entire substrate using Ni films deposited on graphite substrates [7]. A universal method for layer counting has been proposed [8]. In this paper, we will focus on the effect of competitive surface-site occupation between carbon and other surface-active impurities on the graphene growth. It is known that S is a typical impurity of metals and the most surface-active element. The surface sites shall be occupied by S through surface segregation. In the case of Ni(110), it is confirmed by AES and STM that the available surface sites is nearly occupied by S with a centered $2{\times}2$ arrangement. When Ni(110) is doped with C, surface segregation of C may be interfered by surface active elements like S. In this case, nanoscopic characterization has discovered a preferred directional growth of SLG, exhibiting a square-like shape (Fig. 1). Also the detailed characterization methodologies for graphene and h-BN nanosheets, including AFM, STM, KPFM, AES, HIM and XPS shall be discussed.

• International Journal of Aeronautical and Space Sciences
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• 제13권4호
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• pp.446-457
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• 2012

Aeroelastic analysis of an aircraft with a high aspect ratio wing for medium altitude and long endurance capability was attempted in this paper. In order to achieve such an objective, various structural models were adopted. The traditional approach has been based on a one-dimensional Euler-Bernoulli beam model. The structural analysis results of the present beam model were compared with those by the three-dimensional NASTRAN finite element model. In it, a taper ratio of 0.5 was applied; it was comprised of 21 ribs and 3 spars, and included two control surfaces. The relevant unsteady aerodynamic forces were obtained by using ZAERO, which is based on the doublet lattice method that considers flow compressibility. To obtain the unsteady aerodynamic force, the structural mode shapes and natural frequencies were transferred to ZAERO. Two types of unsteady aerodynamic forces were considered. The first was the unsteady aerodynamic forces which were based on the one-dimensional beam shape; the other was based on the three-dimensional FEM model shape. These two types of aerodynamic forces were compared, and applied to the foregoing flutter analysis. The ultimate goal of the present research is to analyze the possible interaction between the rigid-body degrees of freedom and the aeroelastic modes. This will be achieved after the development of a reliable nonlinear beam formulation that would validate the current results as well as enable a thorough investigation of the nonlinearity. Moreover, such analysis will allow for an examination of the above-mentioned interaction between the flight dynamics and aeroelastic modes with the inclusion of the rigid body degrees of freedom.