• 한국전자파학회:학술대회논문집
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• 한국전자파학회 2001년도 종합학술발표회 논문집 Vol.11 No.1
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• pp.16-19
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• 2001

접지된 유전체위에 스트립 격자에 대해 파가 비스비스듬하게 도파할 경우에 비교적 평탄한 Helix 구조로 볼수 있으며 이때 누설파 안테나 관점에서 복소전파상수와 복사패턴을 구하는 방법을 제시하였다. 그리고 유전체 두께가 매우 얇은 경우와 비교적 두꺼운 경우에 대하여 유전체 내부에서 파가 스트립 격자를 가로 질러 도파하거나 비스듬하게 도파하는 경우에 복소전 파상수와 복사패턴을 수치 계산하여 비교 고찰하였다.

• 전자공학회논문지A
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• 제32A권7호
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• pp.30-35
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• 1995

Periodically slotted dielectrically filled paralled-plate waveguide as a leaky wave antenna is analysed for E-polarization case. The homogeneous linear equation whose unknown is the surface current density over the conducting strip is formulated, from which the complex propagation constant is calculated and compared with the previous results. Good correspondence between them is observed. And a method for the radiation pattern is also considered.

• 전자공학회논문지A
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• 제33A권12호
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• pp.33-38
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• 1996

In this paper, we modeled the complex dielectric constant and analyzed the projpagation characteristics of a FR-4 composite substrate with different compositions. From the wideband dielectric modeling and the propagation loss analysis of FR-4 composites that consists of FR-4 resin and E-glass reinforcement,we have found that the propagation loss and velocity increase with the volume fraction of FR-4 resin above 1 GHz. These results are helpful in determining to deisgn optimum substrate composition ratio and cross-sectional geometry of high-speed and high-density transmission line.

• Journal of Mechanical Science and Technology
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• 제20권8호
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• pp.1240-1247
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• 2006

Large eddy simulation of turbulent premixed flame in turbulent channel flow is studied by using G-equation. A flamelet model for the premixed flame is combined with a dynamic subgrid combustion model for the filtered propagation flame speed. The objective of this work is to investigate the validity of the dynamic subgrid G-equation model to a complex turbulent premixed flame. The effect of model parameters of the dynamic sub grid G-equation on the turbulent flame speed is investigated. In order to consider quenching of laminar flames on the wall, wall-quenching damping function is employed in this calculation. In the present study, a constant density turbulent channel flow is used. The calculation results are evaluated by comparing with the DNS results of Bruneaux et al.

• Structural Engineering and Mechanics
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• 제62권3호
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• pp.325-344
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• 2017

The present paper investigates the propagation of Love-type wave in a composite structure comprised of imperfectly bonded piezoelectric layer with lower fiber-reinforced half-space with rectangular shaped irregularity at the common interface. Closed-form expression of phase velocity of Love-type wave propagating in the composite structure has been deduced analytically for electrically open and short conditions. Some special cases of the problem have also been studied. It has been found that the obtained results are in well-agreement to the Classical Love wave equation. Significant effects of various parameters viz. irregularity parameter, flexibility imperfectness parameter and viscoelastic imperfectness parameter associated with complex common interface, dielectric constant and piezoelectric coefficient on phase velocity of Love-type wave has been reported. Numerical computations and graphical illustrations have been carried out to demonstrate the deduced results for various cases. Moreover, comparative study has been performed to unravel the effects of the presence of reinforcement and piezoelectricity in the composite structure and also to analyze the existence of irregularity and imperfectness at the common interface of composite structure in context of the present problem which serves as a salient feature of the present study.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 학술대회
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• 한국전자파학회논문지
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• 제12권5호
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• pp.772-772
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• 2001

본 논문에서는 영상법 기반의 3차원 광선추적법에 패치산란모델을 이용하여 실내 구조물을 고려할 수 있는 실내 전파모델링 방법을 제시하였다. 실내 구조물을 모델링하기 위한 패치산란모델은 패치형태의 직사각형 평면에 대한 RCS를 이용하여 입사에 대한 산란현상을 정의한 것으로써, 책상이나 테이블 같은 평면적인 실내구조물에 대한 산란현상을 각각의 구조물에 대한 영상 안테나를 발생시키는 복잡한 과정 없이 간단하게 해석하기 위한 것이다. RCS는 간단히 입사 전력에 대한 산란 전력의 비로 정의되며 본 논문에서는 다양한 수신 각도에서 바라보는 bistatic RCS를 물리광학(Physical Optics)을 이용하여 수식적으로 유도하여 패치산란모델에 이용하였다. 또한 실내의 다중경로 성분에 대해 계산하지 않는 패치산란모델을 실내에 적용하기 위하여 복잡한 수식보다는 단순한 보정값인 실내보정값을 정의하였는데, 본 논문에서는 이 값을 다양한 패치 환경의 측정에 의한 경험적 상수로 처리함으로써 RCS의 고려만으로는 실내에 적용할 수 없는 점을 극복하였다.

• 한국전자파학회논문지
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• 제12권5호
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• pp.722-733
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• 2001

본 논문에서는 영상법 기반의 3차원 광선추적법에 패치산란모델을 이용하여 실내 구조물을 고려할 수 있는 실내 전파모델링 방법을 제시하였다. 실내 구조물을 모델링하기 위한 패치산란모델은 패치형태의 직사각형 평면에 대한 RCS를 이용하여 입사에 대한 산란현상을 정의한 것으로써, 책상이나 테이블 같은 평면적인 실내구조물에 대한 산란현상을 각각의 구조물에 대한 영상 안테나를 발생시키는 복잡한 과정 없이 간단하게 해석하기 위한 것이다. RCS는 간단히 입사 전력에 대한 산란 전력의 비로 정의되며 본 논문에서는 다양한 수신 각도에서 바라보는 bistatic RCS를 물리광학(Physical Optics)을 이용하여 수식적으로 유도하여 패치산란모델에 이용하였다. 또한 실내의 다중경로 성분에 대해 계산하지 않는 패치산란모델을 실내에 적용하기 위하여 복잡한 수식보다는 단순한 보정값인 실내보정값을 정의하였는데, 본 논문에서는 이 값을 다양한 패치 환경의 측정에 의한 경험적 상수로 처리함으로써 RCS의 고려만으로는 실내에 적용할 수 없는 점을 극복하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제37회 추계학술대회논문집
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• pp.263-267
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• 2011

본 연구는 에틸렌-공기 혼합물로 채워져 있는 굽은 관에서의 충격파와 화염의 상호 작용, 화염 가속, 연소폭발천이 현상을 수치적으로 살펴보았다. 여기서 사용되는 모델은 지배방정식으로 Navier-Stokes 방정식과 경계조건 처리 방법으로 ghost fluid 기법을 사용하였다. 굽은 관에서 여러 충격파 강도를 이용한 모델링을 통하여 화염과 강한 충격파의 충돌에 의한 열점 생성과 화염 전파의 가속 현상을 확인하였으며 추가적으로 평균 화학적 열 발생률이 대략 20 MJ/($g{\cdot}s$)이 되는 지점에서 최초 폭굉이 발생한다는 것을 확인하였다. 즉, 우리는 복잡한 형상에 의한 효과를 포함하는 수치적 계산 결과를 기반으로 관에서의 강한 충격파, 충격파와 화염의 상호 작용, 열점, 연소폭발천이 현상 등의 발생을 확인하였다.