• Journal of the Korea Institute of Information and Communication Engineering
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• v.12 no.7
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• pp.1165-1172
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• 2008

In this paper, the scattering parameters of the metamaterial slab are obtained using the 2D FDTD(Finite-Difference Time-Domain) method. FDTD method is one of strongest electromagnetic numerical method which is widely used to analyze the metamaterial structure because of its simplicity. But it is very difficult to obtain frequency response of metamaterial itself because frequency dispersive model such as Lorentz, Drude model are used in FDTD. We used the well-known m-n-m cycle sine pulse to obtain the frequency response of the metamaterials. Comparisons between the wideband Gaussian input pulse and band-limited m-n-m cycle sine pulse are performed in this paper also. From the results, we concluded that the scattering parameters in frequency domain can be obtained using specific input pulse in FDTD even if the response has valid only for limited bandwidth.

• Computational Structural Engineering
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• v.8 no.3
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• pp.11-21
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• 1995

3차원 대규모 지하구조물의 동적응답을 결정하기 위한 일반적인 수치해석이 제안되었다. 지반과 구조물을 해석하기 위하여 Laplace 변환을 적용한 경계요소법을 설명하였고, 지반-구조물계에 작용하는 외부 동적하중과 지진파를 고려할 수 있도록 공식화하였다. 동적교란이 전파되는 경우에 시간영역의 응답을 얻기 위하여는 구해진 변화된 해를 수치적인 Laplce 역변환을 수행하여야 하지만 동적교란이 조화적인 경우에는 응답이 주파수 영역으로부터 직접 얻어지며, 역변환이 필요하지 않다. 이 방법의 특징은 높은 정확도와 효율성이며, 지반-구조물계에 대하여 초기조건 및 점탄성 재료의 거동을 쉽게 고려할 수 있다는 것이다. 그러므로 이 방법은 다양한 지하구조물의 동적거동과 지진에 대한 취약함을 연구하기 위한 적절한 도구로 사용되어 질 수 있다.

• Proceedings of the KIEE Conference
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• 2015.07a
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• pp.125-126
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• 2015

통신 시스템에서의 더 늘어난 대역폭(Band Width)의 수요로 인해 집적회로(Integrated Circuit)에서 더 높은 동작 주파수(Operating Frequency)를 필요로 하게 되었다. 고주파 영역에서는 SRF(Self Resonance Frequency) 문제와 소자 값의 정확성(Accuracy)에 대한 문제 때문에 정수소자(Lumped Element)를 이용하여 해석을 할 수 없으며 이로 인하여 어떠한 회로의 전기적 특성을 평가함에 있어서 전송선로(Transmission Line)를 이용하여 해석을 하는 것은 중요한 역할을 하게 되었다. 이러한 해석을 위해 순수한 내부 특성을 얻기 위하여 디 임베딩(De-Embedding)이라는 기법이 사용되고 있으나, 알려진 몇 가지의 방법들은 인터커넥터 부분을 완벽히 나타내지 못한다. 따라서 본 논문에서는 1-Port 측정을 기반으로 한 8-Term Error을 이용한 디 임베딩(De-Embedding) 방법을 이용하여 넓은 주파수 영역에서의 교정 값을 얻는 방법에 대하여 소개하고자 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.3
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• pp.209-214
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• 2012

Recently, there were significantly increased cracks failure for external fuel tank horizontal fin of F-5 aircraft. In this paper, the dynamic behavior of horizontal fin was to quantitate by using Finite Element Method. To achieve this goal, the fatigue analysis for time and frequeucy domain has been performed by using the dynamic load spectrum of speed brake. In conclusion, it was proved that fatigue life of the horizontal fin was reduced by the influence of dynamic behavior.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2011.04a
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• pp.485-488
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• 2011

본 연구에서는 경부고속철도의 콘크리트궤도에서 열차주행안전측면에서 관리해야할 레일패드강성의 상한값을 차량 및 궤도의 동특성과 운영환경을 고려하여 결정하는 방법을 제시하였다. 차량과궤도의 상호작용의 해석의 중요 입력파라메타인 궤도틀림과 관련하여 프랑스 및 독일에서 제시한 궤도틀림 PSD(Power Spectral Density)와 경부 1단계구간 콘크리트궤도에서 계측한 궤도틀림 자료를 통하여 얻은 PSD를 기초로 하여 넓은 범위의 주파수영역에서 적용할 수 있는 콘크리트궤도의 궤도틀림 PSD를 제시하였다. 제시된 PSD 기준모델을 사용하여 시간영역에서의 궤도틀림 입력을 Random Generation을 통하여 구한 후 개발된 차량-궤도 상호작용해석 기법을 사용하여 레일패드에 따른 윤중감소율을 산정하였다. 산정된 윤중감소율에 대하여 국내 철도차량 안전기준에 관한 규칙의 탈선계수 규정을 적용하여 주행안전측면에서 허용할 수 있는 레일패드강성의 상한값을 제시하였다.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.22 no.9
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• pp.1968-1974
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• 1997

In this paper, the spectral domain approach is employed to investigate the characteristics of symmetrical and asymmetrical broadside-coupleed coplanar waveguides(BSC-CPW). These structures have large even(c)-odd(.pi.) mode-velocity ratio, suitable for wide-band and tight-coupling microwave circuit design. Efficient design parameters can be obtained from the effective dielectric constants and characteristic impedances calculated by varying the strip widths and slot widths in the BSC-CPW structure.

• Journal of the Korean Society for Precision Engineering
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• v.14 no.10
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• pp.164-169
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• 1997

The aim of this paper is to present some results of sensitivity analysis in frequency domain. The sensitivity fonctions in frequency domain is not depend on the external excitation but depend on the frequency of the system's resonance. The sensitivity functions are determined as function of partial derivatives of system transfer functions taken with respect to system design parameters. The logarithmic sensitivity function is the dimensionless sensitivity funciton available, making it useful to compare the influence of various parameters on system variables. Two degree of fredom system is used to illustrate the procedure for sensitivity analysis proposed in this paper.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.11 no.2
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• pp.186-196
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• 2000

In this paper, modified square loop frequency selective surface for dualband communication antenna systems is proposed, and the scattering characteristics is discussed. The analysis for the problem of scattering by periodic structures with a dielectric slab is formulated using the spectral-domain immittance approach and Floquet's theorem. The method of moments which uses rooftop subdomain basis function is employed to solve the equations. Numerical results include the comparison between the transmission characteristic of general square loop and that of modified square loop. Also, the transmission characteristics of modified square loop for arbitrary incident angle and polarization is presented. To verify analysis results, modified square loop frequency selective surface was fabricated and the calculated results were compared with the measured results. The measured results showed good agreement with the calculated results.

• Transactions of the Korean Society of Mechanical Engineers
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• v.18 no.7
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• pp.1808-1817
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• 1994

Unsteady aerodynamic analysis of an aircraft is done using a frequency domian 3-D panel method. The method is based on an unsteady linear compressible lifting surface theory. The lifting surface is placed in a flight patch, and angle of attack and camber effects are implemented in upwash. Fuselage effects are not considered. The unsteady solutions of the code are validated by comparing with the solutions of a hybrid doublet lattice-doublet point method and a doublet point method for various wing configurations at subsonic and supersonic flow conditions. The calculated results of dynamic stability derivatives for aircraft are shown without comparision due to lack of available measured data or calculated results.

• Proceedings of the Korean Institute of Communication Sciences Conference
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• 1996.10a
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• pp.1185-1188
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• 1996