• 대한기계학회논문집A
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• 제35권8호
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• pp.957-964
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• 2011

본 연구에서는 압전 밴드 갭 구조물(포논 결정) 에 대한 체적 탄성파의 전파 특성을 주파수 및 모드 별로 파악하기 위한 유한 요소법의 적용 방안을 제안하였다. 이를 위해 체적 탄성 진행파의 면내 모드 뿐만 아니라 면외 모드를 포함하도록 3 차원 주기 경계 조건을 고려하였다. 특히, 체적 탄성파 모드 간의 비연성 특성을 전기 분극 방향에 따라 유도한 다음, 그 결과를 유한 요소 모델링에 반영하였다. 제안된 방법은 실제 시뮬레이션을 통해 다양한 형태의 압전 밴드 갭 구조물의 파동 특성 분석에 적용될 수 있는 일반적이고 효율적인 방법임을 확인하였다.

• 한국소음진동공학회논문집
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• 제11권6호
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• pp.181-192
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• 2001

The power flow analysis (PFA) has been performed to analyze the vibration of coupled plates excited by a point force in an arbitrary direction. The point force generates the out-of-plane vibration associated wish flexural waves and the in-plane vibration associated with longitudinal and shear waves. The energy governing equation for each type of waves was introduced and solved to Predict the vibrational energy density and intensity generated by the out-of-plane and in-plane components of the point force in an arbitrary direction. The wave transmission approach was used to consider the mode conversion at the joint of the coupled plates. Numerical results for vibrational energy density and intensity on the coupled plates were presented. Comparison of the results by PFA with exact results showed that PFA can be an effective tool to predict the spatial variation of the vibrational energy and intensity on the coupled plates at high frequencies.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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• pp.423-426
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• 2006

An analysis is made of flow and rocket motion during a supersonic separation stage of air-launching rocket(ALR) from the mother plane. Three-dimensional compressible Navier-Stokes equations is numerically solved to analyze the steady/unsteady flow field around the rocket which is being separated from the mother plane configuration(F-4E Phantom). The simulation results clearly demonstrate the effect of shock-expansion wave interaction between the rocket and the mother plane. To predict the behavior of the ALR according to the change of the C.G., three cases of numerical analysis are performed. As a result, a design-guideline of supersonic air-launching rocket for the safe separation is proposed.

• 한국전자파학회논문지
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• 제19권4호
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• pp.418-426
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• 2008

본 논문은 스펙트럴 영역에서 마이크로스트립 선로의 접지면에 있는 DGS 슬롯의 임피던스 특성을 구하고, 이를 스텝 임피던스 마이크로스트립 저역 통과 필터 특성 개선에 응용하였다. 슬롯 해석에 사용한 방법은 슬롯에 의한 불연속으로 인한 전압과 스펙트럴 영역에서 self-reaction을 이용한 방법이다. 이 방법을 이용한 수치 해석 결과는 full-wave 방법의 결과와 비교해도 정확하다는 것을 보였다. 그리고 기존 스텝 임피던스 마이크로스트립 저역 통과 필터의 주파수 특성을 개선하기 위해서, 균일한 또는 비균일한 DGS 슬롯을 갖는 필터를 설계 제작하였다. 실험 결과를 통해, 제안된 스텝 임피던스 저역 통과 필터는 기존 필터보다 차단 대역이 넓어지고 차단주파수 이후 급격한 차단 특성과 같은 개선된 필터 특성을 확인할 수 있었다.

• Earthquakes and Structures
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• 제9권1호
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• pp.173-194
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• 2015

Site response analysis is an important topic in earthquake engineering. A time-domain numerical method called as one-dimensional (1D) finite element artificial boundary method is proposed to simulate the homogeneous plane elastic wave propagation in a layered half space subjected to the obliquely incident plane body wave. In this method, an exact artificial boundary condition combining the absorbing boundary condition with the inputting boundary condition is developed to model the wave absorption and input effects of the truncated half space under layer system. The spatially two-dimensional (2D) problem consisting of the layer system with the artificial boundary condition is transformed equivalently into a 1D one along the vertical direction according to Snell's law. The resulting 1D problem is solved by the finite element method with a new explicit time integration algorithm. The 1D finite element artificial boundary method is verified by analyzing two engineering sites in time domain and by comparing with the frequency-domain transfer matrix method with fast Fourier transform.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 1999년도 추계학술발표대회 논문집
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• pp.258-263
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• 1999

In this study, the numerical and experimental investigations were conducted to understand ultrasonic wave propagation and to evaluate the degree of fiber waviness in thick composites nondestructively. The path, energy and traveling time of insonified wave were predicted by adopting the ray and plane wave theories. In the analysis, the composites were assumed to have continuous fiber with sinusoidal waviness in a matrix and were modeled as stacks of infinitesimally short length off-axis elements with varying fiber orientation along the length direction. From the experiments on the specially fabricated thick composite specimens with various degrees of uniform fiber waviness, the energy distributions of received wave were obtain for the various positions of transmitter. It was observed that the energy of wave was converged to the adjacent peaks of fiber waviness. The location where maximum energy of wave was detected from the experiments showed good agreement with the location obtained from theoretical predictions. Finally, the test procedure was Proposed to evaluate fiber waviness in thick composites by considering the energy of wave and relative distance between transmitter and receiver.

• International Journal of Naval Architecture and Ocean Engineering
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• 제4권2호
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• pp.96-111
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• 2012

Hull Mounted Sonar (HMS) is a long range submerged vehicle's hull-mounted passive sonar system which detects low-frequency noise caused by machineries of enemy ships or submerged vehicles. The HMS needs a sound absorption /insulation multi-layer structure to shut out the self-noise from own machineries and to amplify signals from outside. Therefore, acoustic analysis of the multi-layer system should be performed when the HMS is designed. This paper simplified the HMS multi-layer system to be an infinite planar multi-layer model. Also, main excitations that influence the HMS were classified into mechanical, plane wave and turbulent flow excitation, and the investigations for each excitation were performed for various models. Stiffened multi-layer analysis for mechanical excitation and general multi-layer analysis for turbulent flow excitation were developed. The infinite planar multi-layer analysis was expected to be more useful for preliminary design stage of HMS system than the infinite cylindrical model because of short analysis time and easiness of parameter study.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 1998년도 추계종합학술대회 논문집
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• pp.335-338
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• 1998

This paper presents calculated results for the infinite phased arrays of the probe-fed rectagualr microstrip patches. A numerical model that is based on a rigorous Green's function and galerkin solutionsis is described. In an arbitrary scan plane, the input impedance and the input reflection coefficient versus the scand angle are calculated. The effects of substrate parameters on the phased arry antenna are considered. The scan blindness phenomenon due to the surface wave is observed and the input impedance bandwidth in the arbitrary scan plane is calculated.

• 한국음향학회지
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• 제33권3호
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• pp.200-209
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• 2014

본 논문에서는 평면파 합성 송신집속 방법의 모델을 제시하고 수학적 해석을 통해 그 특성을 분석하였으며 일반적인 구형파 기반의 집속 방법과 비교하였다. 이를 통하여 평면파를 이용한 합성 송신집속 방법은 거리에 따라 주엽의 폭이 변하지 않는 비회절 빔을 발생함을 확인하였다. 또한 그레이팅 로브의 발생을 억제하며 원하는 주엽 폭을 얻기 위한 평면파 합성 방법, 그리고 비회절 특성이 유지되는 영역을 효과적으로 확장시킬 수 있는 방법을 제시하였다. 제안된 방법과 해석결과들을 컴퓨터 모의실험을 통해 검증하였다.

• 전자공학회논문지A
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• 제29A권11호
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• pp.19-24
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• 1992

In this paper, a high frequency method is developed which combines the uniform Geometrical Theory of Diffraction(GTD) and the Aperture Integration(AI) to analyze electromagnetic plane wave scattering by a perfectly-conducting, open-ended, semi-infinite parallel plate waveguide with a uniform layer of absorbing material on its inner wall, and with a slanted planar termination inside. In this method, first, the field of an arbitary point inside the paraller plate waveguide is computed by the GTD. Second, the field scattered into exterior region by the waveguide is found using the equivalent current, which can be obtaind from the aperture field of the waveguide and using the AI. Numerical results based on this GTD method are presented and compared with those based on the mode matching method.