• 비파괴검사학회지
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• 제23권1호
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• pp.1-6
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• 2003

배관 내의 스케일은 통수비를 감소시키므로 배관을 적절히 관리하기 위해서는 스케일량에 대한 정량적인 평가가 필수적이다. 상수도 급수관내의 스케일량을 평가하기 위해서 유도초음파를 사용하였다. 가변각 ??지를 사용하여 유도 초음파의 여러 모드를 발생시키고, 노후 배관을 따라서 전파하는 특성을 분석하였다. 실험적으로 관내의 스케일이 증가함에 따라서 $f{\times}d=1.5MHz\;mm$인 경우에 F(M,2) 모드들의 진폭이 크게 감소하는 것을 알 수 있었다. 본 연구의 결과로 상수도 급수관의 스케일량 평가에 적합한 유도 초음파는 F(M,2) 모드들임을 알 수 있었다.

• 비파괴검사학회지
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• 제29권5호
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• pp.458-465
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• 2009

일반적인 산업현장에서 내부결함 평가를 위해 사용되어온 유도초음파기법은 비결함 지역에서는 에너지 감쇠를 고려하지 않고 적용되어 왔다. 결함 지역에서의 신호는 산란과 반사에 의해서 분명한 감쇠가 발생하지만 비결함 지역에서도 작은 감쇠가 발생한다. 또한 분산선도에서 판파(Lamb wave)는 각 두께, 주파수에 의해 분산성이 달라지기에 각 모드에 적합한 감쇠계수를 찾는 것은 중요하다. 이를 위해 접촉식 PZT(piezoelectric)센서를 이용한 pitch-catch 방식으로 거리에 따른 각 모드의 감쇠계수를 구하였다. 본 연구에서는 흔히 쓰이는 알루미늄과 구리판으로, 두께 차이, 모드 차이, 재질 차이에 의한 실험적인 감쇠율을 구하는데 중점을 두었다. 그 결과 각 변수에 따라 감쇠계수는 달라지며, 정량화가 필요하다는 것을 확인하였다.

• 대한토목학회논문집
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• 제29권4B호
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• pp.377-384
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• 2009

다중 계단으로 근사한 사주지형 위를 지나는 선형 파랑전파에 대한 고유함수 전개법에서 크기가 큰 행렬을 풀 때 계산시간을 상당히 단축하기 위하여 분할행렬법을 사용하여 반사율을 계산하였다. 본 모형에 10개의 억류파를 사용하여 현재까지 가장 정밀한 수치해를 구하였고 구한 반사율의 거동은 몇 경우에서 기존 결과와 다름을 보였다. 크기가 큰 행렬을 풀 때 본 분할행렬법의 계산시간과 기억용량은 여전히 커서 효율적인 방법에 대한 개발이 요구된다.

• 한국광학회지
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• 제11권3호
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• pp.198-201
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• 2000

본 논문에서는 Finite-Difference Time-Domain 방법을 이용해서 2차원 광자 밴드캡 구조 중 정삼각형 격자 구조, 정사각형 격자 구조, 그리고 정육각형 격자 구조의 전파의 투과 특성과 디펙트 모드의 특성 변화를 고찰하였다. 디펙트 모드는 디펙트의 위치, 모양 : 유전율 등에 따라 다양하게 변화하는데, 본 논문에서는 특히 유전율 변화를 중심으로 특징을 고찰하였다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2004년도 춘계학술대회논문집
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• pp.843-846
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• 2004

Cavity tone is generated due to the feedback between flow and acoustic wave. It is recognized that the period is determined by the time required for the flow convection in one direction, the time required for the acoustic propagation in the other direction and the time for phase shift depending on the flows and mode. Most of the phenomena have been investigated by experiments and a simple but fundamental theory. But the cause of the phase shift and the correctness of the theory have not been clearly explained so far. In this paper, the phenomena are calculated numerically to obtain detail information of flow and acoustic wave to explain the mechanism including the phase. High order high resolution scheme of optimized high order compact is used to resolve the small acoustic quantities and large flow quantities at the same time. The data are reduced using cross correlation function in space and time and cross spectral density function which has phase information. Abrupt change in pressure near corner in cavity is observed and is relate to phase variation. The time required for the feedback between the flow and acoustic wave is calculated after the numerical simulation f3r various modes. The periods based on the time calculated using the above method and direct observation from the acoustic waves generated and propagated in the numerical simulation are compared. It is found that no phase shift is required if we examine the time required carefully. Rossiter's formula for the cavity tone used for quick estimation needs to be modified far some modes.

• 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.

• 한국음향학회지
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• 제9권4호
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• pp.18-32
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• 1990

최근 신호 처리 기기와 센서로서 각광을 받고 있는 SAW Device 는 때론 목적에 따라 수중에서 사용해야 할 때가 있다. 그러나 유체내의 고체 표면을 전파하는 표면파의 경우, 유체내로의 에너지 손실로 인해 설계상에 많은 어려움을 주고 있다. 따라서 본 연구에서는 이러한 어려움을 극복할 수 있는 최적 설계법으로서, 컴퓨터 모형해석을 통해 수중에서 압전물질에 의한 표면파의 최대 발진 효율, 최소 전파 감쇄율, 그리고 pure mode 전파를 이룰 수 있는 SAW Device 의 최적 geometry, 즉 초적 압전 결정 평면, 표면과 전파 방향, 그리고 무차원 전파 계수 들을 구하였다. 본 논문에서는 표면파가 전파하는 고체 재료로서 PZT와 PVDF 적층, 그리고 쇠 하부층을 사용하였으나, 이 설계법은 임의의 유체층과 고체층의 조합에도 적용할 수 있다. 동일한 기술은 수중음향 계측기, antifouling, 그리고 산업 및 의료 분야 등에 쓰이는 센서와 발진기의 설계에도 바로 응용할 수 있다.

• Structural Engineering and Mechanics
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• 제75권4호
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• pp.435-444
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• 2020

Ultrasonic guided wave testing is a very promising non-destructive testing method for rails, which is of great significance for ensuring the safe operation of railways. On the basis of the semi-analytical finite element (SAFE) method, a analytical model of 59R2 grooved rail was proposed, which is commonly used in the ballastless track of modern tram. The dispersion curves of ultrasonic guided waves in free rail and supported rail were obtained. Sensitivity analysis was then undertaken to evaluate the effect of rail elastic modulus on the phase velocity and group velocity dispersion curves of ultrasonic guided waves. The optimal guided wave mode, optimal excitation point and excitation direction suitable for detecting rail integrity were identified by analyzing the frequency, number of modes, and mode shapes. A sinusoidal signal modulated by a Hanning window with a center frequency of 25 kHz was used as the excitation source, and the propagation characteristics of high-frequency ultrasonic guided waves in the rail were obtained. The results show that the rail pad has a relatively little influence on the dispersion curves of ultrasonic guided waves in the high frequency band, and has a relatively large influence on the dispersion curves of ultrasonic guided waves in the low frequency band below 4 kHz. The rail elastic modulus has significant influence on the phase velocity in the high frequency band, while the group velocity is greatly affected by the rail elastic modulus in the low frequency band.

• 전기의세계
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• 제20권5호
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• pp.15-18
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• 1971

Up to now, there have been numerous investigations about the effect of diffusion on the wave propagation in gaseous plasmas, but not so much in semiconductor magnetoplasmas. However, currently, it becomes the centor of interest to work with the latter problem, and this paper deals with the dispersion equation including diffusion effect in the latter case to see how diffusion affects the equation in which diffusion term is neglected in the first place, and the analysis is based on the assumption that the plasma can be treated as a hydrodynamical fluid, since, from a macroscopic view point, the plasma interacting with a magnetic field can be considered as a magneto-hydrodynamical fluid, an electrically conducting fluid subjected to electromagnetic force, and the system is linear. The results of the relation and computation show that in the non-streaming case the diffusion terms appear in the equation as perturbation terms and the amplitude of the wave vector changes parabolically with the variation of the angular frequency and the longitudinal modes are observed.