• 한국광학회지
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• 제11권6호
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• pp.423-428
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• 2000

방향성 결합 구조의 음향파 도파로를 이용한 편광모드 변환형 파장가변 광 필터를 LiNbO$_3$ 와 Ti 이중 확산 공정기술을 이용하여 제작하였다. 균일 결합구조형 AOTF의 부모드의 크기를 두 음향파 도파로의 방향성 결합형 가중 결합 원리를 이용하여 8 dBwjd도 추가적으로 억제시킬 수 있었다. 1551.6mm 파장의 TE, TM 입사 편광모드와 173.58MHz, 17.78mW RF 구동신호각각에 대해서 -12.68dB 부모드 억압과 90% 변환효율이 측정되었다. 파장변화율과 통과 대역폭은 각각 8.86nm/ MHz, 1.7nm로 측정되었다.

• 한국광학회지
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• 제8권4호
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• pp.315-319
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• 1997

광편향은 광굴절결정내의 두 기록빔 간섭에 의해 유도된 동적 광굴절 부피격자를 이용한다. 본 논문에서는 외부 전기장을 인가할 필요가 없으며, 낮은 광세기에서도 쉽게 광굴절 부피격자가 유도되는 CeO$_{2}$가 0.05Wt.% 도핑된 Sr$_{0.6}$Ba$_{0.4}$Nb$_{2}$O$_{6}$(Ce-SBN:60)결정의 동적 특성을 이용하여 광편향기를 구현하고 해석하였다. 그리고, Ce-SBN:60결정의 광파결합특성을 조사하기 위해 2광파 혼합을 통해 결정의 최대결합계수, 유효전하밀도, 기록빔의 세기비에 따른 회절효율 및 회절효율의 시간응답특성을 측정하고 해석하였다.

• 한국항공우주학회지
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• 제35권6호
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• pp.509-516
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• 2007

본 연구에서는 틸트로터 항공기의 날개-로터 시스템의 수학적 모델링과 자유진동 제어에 대하여 고찰하였다. 날개에 부착된 로터는 수직방향에서 수평방향으로 또는 그 반대로 틸팅각을 변경시킬 수 있다. 로터의 틸팅각, 복합재료 날개의 섬유각, 로터의 회전속도를 변수로 하여 자유진동 특성 및 압전재료를 이용한 자유진동 제어 효과에 대하여 고찰하였다. 복합재료 날개는 상자형 박판 보로 모델링 하였으며, 플랩-래그운동 사이의 연성과 인장-비틀림 운동사이의 연성이 발생하는 CUS 구조로 가정하였다. 수치해석 결과와 그에 따른 결론을 도출하였다.

• 한국전기전자재료학회논문지
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• 제22권4호
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• pp.307-313
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• 2009

Quantitative analysis of optical scattering intensities from a Au nanoparticle with a diameter of 100 nm, which is effected by the localized surface plasmon resonance (LSPR), were numerically carried out by using a dark-field detection scheme on prism basal plane for two different beam incident modes of reflectance (R-mode) and transmittance (T-mode). Two-dimensional finite difference time domain (FDTD) algorithm was adopted, and its applicabilibility was verified by comparing the simulation results with the theoretical ones. Simulation results of the scattered light intensities from a Au nanoparticle revealed that the scattered intensity of the T-mode was much stronger than that of R-mode. Comparison of the calculated results with the theoretical intensity distribution on the prism showed that the scattered intensity is marimized when the evanescent field, which is generated from the interface of prism and air at TIR angle, is coupled with Au nanoparticle.

• 대한토목학회논문집
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• 제10권1호
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• pp.27-36
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• 1990

본(本) 논문(論文)에서는 전단변형(剪斷變形) 효과(效果)가 고려되는 평면(平面)뼈대 구조물(構造物)의 기하적(幾何的)인 비선형(非線形) 해석(解析)을 수행하기 위한 두 가지 방법 즉, 유한분절법(有限分節法)과 유한요소법(有限要素法)을 제시한다. 유한분절법(有限分節法)의 경우에는 평형방정식(平衡方程式)을 직접(直接) 적분(積分)하므로써 엄밀(嚴密)한 접선강도(接線剛度) 매트릭스가 유되되는 반면에 유한요소법(有限要素法)의 경우에는 전단변형(剪斷變形)을 고려하는 Hermitian 다항식(多項式)을 형상함수(形狀函數)로 사용하므로써 탄성(彈性) 및 기하적(幾何的)인 강도(剛度)매트릭스가 산정된다. 선택된 예제(例題)들을 해석(解析)한 결과들과 다른 문헌(文獻)의 결과들을 비교, 검토하므로써 본(本) 논문(論文)에서 제시된 이론(理論)의 정당성(正當性)을 입증(立證)한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2004년도 춘계학술대회논문집
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• pp.575-580
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• 2004

In this work, the effect of composite couplings and mass distributions on hub loads of a hingeless rotor in forward flight is investigated. 1'he hingeless composite rotor is idealized as a laminated thin-walled box-beam. The nonclassical effects such as transverse shear and torsion warping are considered in the structural formulation. The nonlinear differential equations of motion are obtained by applying Hamilton's principle. The blade responses and hub loads are calculated using a finite element formulation both in space and time. The aerodynamic forces acting on the blade are calculated using the quasi-steady strip theory. The theory includes the effects of reversed flow and compressibility The magnitude of elastic couplings obtained by MSC/NASTRAN is compared with the classical pitch-flap($\delta$$_{3}$) coupling. It is observed that the elastic couplings and mass distributions of the blade have a substantial effect on the behavior of $N_{b/}$rev hub loads. About 40% hub loads is reduced by tailoring or redistributing the structural properties of the blade.f the blade.

• 대한전자공학회논문지
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• 제24권4호
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• pp.696-700
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• 1987

Guide modes in a graded index multinmode optical fiber are turned into clad modes when the optical fiber was bended into a perpendicular direction to its optical axes by microbending forces, which causes the loss of the guiding optical power. The theories reported on this microbending power loss can be applied to calculation of the transmission power loss only when the beding period equals to the mode coupling length. In this paper, we obtained the general expression of the optical power transmission loss in a graded index multimode fiber bended periodically. This can be applied to the calculation of the power loss of the periodically microbended fiber with an arbitrary bending shape and period. Also, by using the beam theory in mechanics, we could derive the expression of the displacement of the optical fiber caused by the external force which bends the fiber into a periodic trapezoidal shape. Experiments were carried out to determine the dependence of the power loss on the period of the microbending forces. Experimnetal results were in good agreement (in the same order of the magnitude) with theoritical values derived in our work within the bending period region of 2mm-10mm.

• The Journal of the Acoustical Society of Korea
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• 제13권1E호
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• pp.45-54
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• 1994

탄성표면파 소자용 압전재료의 특성을 평가하여 최적 절단명과 전파방형을 결정하였다. 압전단결정 $LiTaO_4$에 대하여 Rayleigh파의 속도, 결합계수, 표면유전상수, 주파수-온도계수, 감쇠계수, 퓨어모드 전하, 빔 산란, 그리고 정열오차 감도 등의 항목들을 평가하였다. 이론적 계산 결과 Y절단면상의 X축 방향이 최적치로 나타났고, 이결과는 시럼에 의해 확인되었다. 본 논문의 평가방법은 여타 다른 압전재료들에도 동일하게 적용이 가능하다.

• 한국레이저가공학회지
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• 제8권1호
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• pp.9-18
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• 2005

The laser direct writing method using a UV Argon-ion laser is studied for fabrication of waveguide. The laser direct writing system is constructed with a vision camera, a xy-stage, a motion controller and the delivery components of a laser beam. The UV Argon-ion laser has wavelength range of $333.6\~363.8$ nm. A photo-active UV curable polymer for a planar light-wave circuit(PLC) of single mode is used. This polymer is irradiated by Argon-ion laser and developed by a solvent after a post-baking. The optimum laser direct writing condition is obtained experimentally by changing various process parameters such as laser power, writing speed and focal length. The propagation and coupling loss of a optical waveguide was measured as 1dB/cm and 0.6dB/cm, respectively. Also, the minimum width of waveguide of $100{\mu}m$(ZPLW-207) is obtained. Finally, the waveguides of line, bend and branch type are successfully fabricated.

• 한국소음진동공학회논문집
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• 제14권8호
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• pp.734-740
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• 2004

In this work, the effect of composite couplings and mass distributions on hub loads of a hingeless rotor in forward flight is investigated. The hingeless composite rotor is idealized as a laminated thin-walled box-beam. The nonclassical effects such as transverse shear and torsion warping are considered In the structural formulation. The nonlinear differential equations of motion are obtained by applying Hamilton’s principle. The blade responses and hub loads are calculated using a finite element formulation both in space and time. The aerodynamic forces acting on the blade are calculated using the quasi-steady strip theory. The theory includes the effects of reversed flow and compressibility. The magnitude of elastic couplings obtained by MSC/NASTRAN is compared with the classical pitch-flap($\delta$$_3$) coupling. It Is observed that the elastic couplings and mass distributions of the blade have a substantial effect on the behavior of $N_{b}$ /rev hub loads. About 40％ hub loads is reduced by tailoring or redistributing the structural properties of the blade.e.