• 전자공학회논문지D
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• 제35D권2호
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• pp.1-12
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• 1998

In this paper, an incoherent imaging of a high-contrast cylindrical cavity illuminated by the time-harmonic cylindrical wave is obtained ia the back-projections of he incoherent intensity patterns, which si acquired by averaging out the multi-frequency intensities of the total electric field scattered from this object in the cross-borehole measurement configuration. Multi-freuqncy effect is shown numerically and is intepreted analytically by the mutual coherence function defined in the is frequency domain. This imaging method is validated by imaging high-contrast cylindrical cavidities and the conditions to get better image are investigated.

• 한국인터넷방송통신학회논문지
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• 제11권6호
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• pp.157-162
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• 2011

본 연구에서는 국내 T-DMB 방송 송신기 및 중계기에서 사용하는 공동여파기를 설계하고 제작한다. 설계를 위하여 3차원 field 시뮬레이션 툴인 HFSS를 이용한다. T-DMB 여파기는 Q값이 높아야 하고 대전력인 이유로 공동여파기가 주로 사용되고 있다. 본 연구에서는 공동공진기의 설계를 보다 쉽고 정확한 특성을 얻기 위하여 HFSS를 이용한다. 시뮬레이션된 특성을 바탕으로 여파기를 제작하고 특성을 측정하여 시뮬레이션 결과와 비교한다. 측정한 결과 공진주파수 211.8MHz에서 대역폭 0.1MHz의 특성을 얻음으로써 시뮬레이션 결과와 설계치에 잘 부합되었음을 밝힌다.

• 한국ITS학회 논문지
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• 제10권6호
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• pp.91-97
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• 2011

본 연구에서는 국내 T-DMB 방송 송신기 및 중계기에서 사용하는 공동여파기를 설계하고 제작한다. 설계를 위하여 3차원 field 시뮬레이션 툴인 HFSS를 이용한다. T-DMB 여파기는 Q값이 높아야 하고 대전력인 이유로 공동여파기가 주로 사용되고 있다. 본 연구에서는 공동공진기의 설계를 보다 쉽고 정확한 특성을 얻기 위하여 HFSS를 이용한다. 시뮬레이션된 특성을 바탕으로 여파기를 제작하고 특성을 측정하여 시뮬레이션 결과와 비교한다. 측정한 결과 공진주파수 211.8MHz에서 대역폭 0.1MHz의 특성을 얻음으로써 시뮬레이션 결과와 설계치에 잘 부합되었음을 밝힌다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 추계 학술대회논문집
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• pp.181-184
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• 2006

High-speed flight vehicle have various cavities. The supersonic cavity flow is complicated due to vortices, flow separation and reattachment, shock and expansion waves. The general cavity flow phenomena include the formation and dissipation of vortices, which induce oscillation and noise. The oscillation and noise greatly affect flow control, chemical reaction, and heat transfer processes. The supersonic cavity' flow with high Reynolds number is characterized by the pressure oscillation due to turbulent shear layer, cavity geometry, and resonance phenomenon based on external flow conditions, The resonance phenomena can damage the structures around the cavity and negatively affect aerodynamic performance and stability. In the present study, we performed numerical analysis of cavities by applying the unsteady, compressible three dimensional Reynolds-Averaged Navier-Stokes(RANS) equations with the ${\kappa}-{\omega}$ turbulence model. The cavity model used for numerical calculation had a depth(D) of 15mm cavity aspect ratio(L/D) of 3, width to spanwise ratio(W/D) of 1.0 to 5.0. Based on the PSD(Power Spectral Density) and CSD(Cross Spectral Density) analysis of the pressure variation, the dominant frequency was analyized and compared with the results of Rossiter's Eq.

• 한국전산유체공학회지
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• 제11권4호
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• pp.62-66
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• 2006

High-speed flight vehicle have various cavities. The supersonic cavity flow is complicated due to vortices, flow separation, reattachment, shock waves and expansion waves. The general cavity flow phenomena includes the formation and dissipation of vortices, which induce oscillation and noise. The oscillation and noise greatly affect flow control, chemical reaction, and heat transfer processes. The supersonic cavity flow with high Reynolds number is characterized by the pressure oscillation due to turbulent shear layer, cavity geometry, and resonance phenomenon based on external flow conditions. The resonance phenomena can damage the structures around the cavity and negatively affect aerodynamic performance and stability. In the present study, we performed numerical analysis of cavities by applying the unsteady, compressible three dimensional Reynolds-Averaged Navier-Stokes(RANS) equations with the ${\kappa}-{\omega}$ turbulence model. The cavity model used for numerical calculation had a depth(D) of 15mm cavity aspect ratio (L/D) of 3, width to spanwise ratio(W/D) of 1.0 to 5.0. Based on the PSD(Power Spectral Density) and CSD(Cross Spectral Density) analysis of the pressure variation, the dominant frequency was analyzed and compared with the results of Rossiter's Eq.

• 한국진공학회지
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• 제17권5호
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• pp.408-418
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• 2008

본 논문에서는 집속이온빔의 플라즈마원을 위한 간단한 직육면체형태의 공진 공동을 설계하고 특성연구를 수행하였다. 공진에 최적인 공동 구조는 HFSS(High Frequency Structure Simulator)를 이용한 전기장 분포를 통해 구체적으로 계산하였다. 공진 공동은 내부 석영관 및 플라즈마 등의 유전체의 영향을 받기 때문에 공동의 한축 길이를 변화시킬 수 있는 구조로 설계되었다. 실험적으로 관찰되는 마이크로웨이브 방전시작전압을 통해 방전에 최적인 공동 길이를 측정하여 HFSS 계산된 값과 비교하였다. 공동은 석영관으로 인한 내부 유효유전율의 변화에 의해 석영관을 고려하지 않았던 길이에 비해 10cm가 감소된 길이에서 최적화됨을 공통적으로 확인할 수 있었다. 또한 압력변화에 따른 방전시작전압은 Paschen Curve와 유사한 결과를 나타내었다. 방전이 발생한 후에는 입력전력에 따라 플라즈마 밀도가 증가하였고 플라즈마의 영향으로 감소한 유효유전율에 의해 10cm가 증가한 길이에서 최적화가 되었다. 하지만 300W이상의 높은 입력 전력에서는 마이크로웨이브가 투과할 수 없는 고밀도 플라즈마 경계층(cut off layer)이 확장하여 더 이상 공동길이 조절을 통한 공동 최적화가 불가능함을 확인하였다. 따라서 고밀도 플라즈마를 만들기 위한 마이크로웨이브 공동의 정확한 설계를 위해 마이크로웨이브가 통과할 수 없는 고밀도 플라즈마 영역을 도체로 가정하고 그 외의 저밀도 플라즈마 영역을 밀도에 고유한 특정 유전율을 가지는 유전체로 설정하여 공동 내부의 전기장 분포를 해석하는 과정이 꼭 필요하다.

• 마이크로전자및패키징학회지
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• 제16권4호
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• pp.5-8
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• 2009

In this paper, a high-quality low-temperature co-fired ceramic (LTCC) solenoid inductor using a solder ball and an air cavity on a silicon wafer for three-dimensional (3-D) system-in-package (SiP) is proposed. The LTCC multi-layer solenoid inductor is attached using Ag paste and solder ball on a silicon wafer with the air cavity structure. The air cavity is formed on a silicon wafer through an anisotropic wet-etching technology and is able to isolate the LTCC dielectric loss which is equivalent to a low k material effect. The electrical coupling between the metal layer and the LTCC dielectric layer is decreased by adopting the air cavity. The LTCC solenoid inductor using the solder ball and the air cavity on silicon wafer has an improved Q factor and self-resonant frequency (SRF) by reducing the LTCC dielectric resistance and parasitic capacitance. Also, 3-D device stacking technologies provide an effective path to the miniaturization of electronic systems.

• 제어로봇시스템학회논문지
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• 제20권2호
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• pp.107-111
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• 2014

An SIW cavity is a useful tool to design an FSS which shows a rapid roll-off rate and insensitivity to polarizations and incident angles of electromagnetic waves. However, due to its high Q-factor, the FSS also shows narrow bandwidth which is undesirable for high-capacity communication. To address this drawback, we propose a novel technique to enhance the bandwidth while maintaining similar frequency response characteristics and minimizing the increase of the overall thickness of the SIW cavity FSS. In order to verify the performance of the technique, simulated frequency responses will be provided. Also, a parameter which affects the bandwidth will be studied. Finally the stability to polarizations and incident angles will be observed through the simulated results.

• Wind and Structures
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• 제38권3호
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• pp.193-202
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• 2024

Modern high-rise tower designs incorporating recessed balcony cavity spaces can be prone to high-frequency and narrow-band Rossiter aerodynamic excitations under glancing incident winds that can harmonize and compete with recessed balcony volume acoustic Helmholtz modes and facade elastic responses. Resulting resonant inertial wind loading to balcony facades responding to these excitations is additive to the peak design wind pressures currently allowed for in wind codes and can present as excessive facade vibrations and sub-audible throbbing in the serviceability range of wind speeds. This paper presents a methodology to determine Cavity Amplification Factors to account for façade resonant inertial wind loads resulting from balcony cavity aero-acoustic-elastic resonances by drawing upon field observations and the results of full-scale monitoring and model-scale wind tunnel tests. Recessed balcony cavities with single orifice type openings and located within curved façade tower geometries appear particularly prone. A Cavity Amplification Factor of 1.8 is calculated in one example representing almost a doubling of local façade design wind pressures. Balcony façade and tower design recommendations to mitigate wind induced aero-acoustic-elastic resonances are provided.

• 한국초전도학회:학술대회논문집
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• 한국초전도학회 2000년도 High Temperature Superconductivity Vol.X
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• pp.173-178
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• 2000

A prototype for a highly sensitive, automated measurement system for the microwave surface resistance of high-T$_c$ superconductor films was set up, and tested by measuring the microwave surface resistances of high-T$_c$ YBa$_2$Cu$_3$O$_{7-{\delta}}$(YBCO) films at the frequency of about 19.6 GHz and the temperature of 30 K ${\sim}$ 90 K. An open-ended TE$_{011}$ mode sapphire-loaded cylindrical cavity resonator was used as the measurement probe, where YBCO films were used as the endplates of the cylindrical cavity. The characteristics of the measurement system include functions to display the unloaded ${\varrho}$ and the resonant frequency of the TE$_{011}$ mode resonator as well as the microwave surface resistance of the YBCO films, all simultaneously as a function of temperature. Applicability of the measurement system for investigating the homogeneity in the microwave properties of large high-T$_c$ superconductor films is discussed.