• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.864-870
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• 2001

Flame propagation along vortex tube was experimentally investigated. The vortex tube was generated by the ejection of propane from a nozzle through a single stroke motion of a speaker and the ignition was induced from a single pulse laser. Non-reactive flow fields were visualized using shadow technique. From these images, vortex ring size and translational velocity were measured in order to determine the ignition time and position. Flame structure and flame speed were measured using high speed CCD camera. Flame speed was accelerated during the initial stage of flame kernel growth, and reached near constant value during steady propagation period. Near the completion of propagation, flame speed was decelerated and then extinguished. Flame speed along the non-premixed vortex tube was found to be linearly proportional to circulation, which was similar to that of the flame propagation along premixed vortex ring. Ignition position minimally affects the propagation characteristics. These imply that flame is propagating along the maximum speed locus expected to be along stoichiometric contour and also support the existence of tribrachial flames.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2002년도 제24회 KOSCO SYMPOSIUM 논문집
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• pp.140-146
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• 2002

The tulip-inversion of flames in half-open tubes was investigated experimentally. Experiments was carried out in tubes with various shapes. The image of a flame propagation were pictured by HICCD(High speed intensified CCD) and the dynamic pressure of tubes was measured by a piezo pressure sensor. By analyzing the images of the flame propagation, we found the time and the distance for the occurrence of tulip-inversion. Regardless of the shapes of tubes, time of tulip-inversion are similar and inversely proportional to the burning velocity. But distances have different tendency. In a straight tube, the distance of tulip-inversion increases when the burning velocity increases. But in a converging tube, the distance of tulip-inversion decreases when a burning velocity increases. And the distance of tulip-inversion in a converging tube is much smaller than the distance of tulip-inversion in a straight tube. These results are caused by the deceleration of a flame when the diameter of a hole in open-side of a tube is small. The deceleration causes little effect on the time of tulip-inversion.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.550-555
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• 2003

When a shock wave arrives at an open end of tube, an impulse wave is discharged from the tube exit and complicated flow is formed near tube exit. The flow field is influenced by the cross-sectional geometry of tube exit, such as circular, square, rectangular, trapezoid and etc. In the current study, three-dimensional propagation characteristics of impulse wave discharged from the tube exit with non-circular cross section are numerically investigated using a CFD method. Total variation diminishing (TVD) scheme is used to solve the three-dimensional, unsteady, compressible Euler equations. Computations are performed for the Mach numbers of the incident shock wave $M_{s}$ below 1.5. The results obtained show that the peak pressure of the impulse wave and propagation directivity depends on the cross-sectional geometry of tube exit and the Mach number of incident shock wave.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.350-355
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• 2012

최근 다양한 공학 응용 분야에 Micro Shock Tube의 중요성이 커지고 있다. Pharma Ballistic 기술은 기존의 약물주입방법과 달리 약물입자를 가속하여 피부로 침투시키기 위해 Micro Shock Tube를 적용하는 기술 중 하나이다. 그러나 이러한 장치의 효율적인 설계를 위해서는 Micro Shock Tube 내부유동과 충격특성에 대한 상세한 지식을 필요로 한다. 경계층과 같은 많은 요소들 때문에 Micro Shock Tube 내부의 낮은 Reynolds Number와 높은 Knudsen Number가 형성되며, 이 때의 충격파 전파는 기존의 Macro Shock Tube와 상이하게 나타난다. 본 연구에서는 Micro Shock Tube에서의 충격파 전파와 유동특성을 조사하기 위해 직경 3mm의 Micro Shock Tube를 이용하여 실험을 수행하였으며, 압력은 저압관의 세 지점에서 측정되었다. 충격파 속도와 같은 다른 변수들의 실험값으로부터 충격파 강도를 찾고 충격파 선도를 나타내었다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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• pp.77-78
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• 2015

Laminar burning velocities have been predicted by constant volume combustion chamber, counter flow burner and others. In this study, the measured flame propagation velocities in an assembled annular stepwise diverging tube were plotted with respect to equivalence ratio, length scale, and velocity scale. Three dimensional approach to understand the flame propagation velocity including laminar burning velocity is investigated, and the surface provides the correlation among quenching distance, propagation velocity, and equivalence ratio.

• 한국추진공학회지
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• 제16권5호
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• pp.74-80
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• 2012

최근 Micro Combution, Micro Propulsion, Particle Delivery Systems 등 다양한 공학 응용 분야에서 Micro Shock Tube의 중요성이 커지고 있다. 그러나 여러 분야에 Micro Shock Tube를 효율적으로 적용하기 위해서는 관내유동과 충격특성에 대한 상세한 지식을 필요로 한다. 경계층과 같은 많은 요소들 때문에 Micro Shock Tube 내부의 낮은 Reynolds Number와 높은 Knudsen Number가 형성되며, 이때의 충격파 전파는 기존의 Macro Shock Tube와 상이하게 나타난다. 본 연구에서는 Micro Shock Tube에서의 충격파 전파와 유동특성을 조사하기 위해 직경 3 mm와 6 mm의 두 가지 Micro Shock Tube를 이용하여 실험을 수행하였으며, 압력은 고압관의 파막압력과 저압관의 세 지점에서 측정되었다. 충격파 속도와 같은 다른 변수들의 실험값으로부터 충격파 강도를 찾고 충격파 선도를 나타내었다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.364-370
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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. 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 and unstable pitch modes for the lower and higher activation energies, respectively. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of two modes. The maximum pressure history in the stable pitch remained nearly constant, and the single Mach leg existing on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the unstable pitch due to the generation and decay of complex Mach interaction on the shock front shape. The high frequency oscillation was self-induced because the intensity of the transverse wave was changed during propagation in one cycle. The high frequency behavior was not always the same for each cycle, and therefore the low frequency oscillation was also induced in the pressure history.

• 한국가시화정보학회지
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• 제10권1호
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• pp.40-46
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• 2012

Recently micro shock tube is extensively being used in many diverse fields of engineering applications but the detailed flow physics involved in it is hardly known due to high Knudsen number and strong compressibility effects. Unlike the macro shock tube, the surface area to volume ratio for a micro shock tube is very large. This unique effect brings many complexities into the flow physics that makes the micro shock tube different compared with the macro shock tube. In micro shock tube, the inter- molecular forces of working gas can play an important role in specifying the flow characteristics of the unsteady shock wave flow which is essentially generated in all kinds of shock tubes. In the present study, a CFD method was used to predict and visualize the unsteady shock wave flows using the unsteady compressible Navier-Stokes equations, furnished with the no-slip and slip wall boundary conditions. Maxwell's slip equations were used to mathematically model the shock movement at high Knudsen number. The present CFD results show that the propagation speed of the shock wave is directly proportional to the initial pressure and diameter of micro shock tube.

• 한국음향학회지
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• 제23권5호
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• pp.353-361
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• 2004

증기발생기 세관에서의 유도초음파 전파 특성에 관한 연구를 수행하였다. 증기 발생기 세관의 분산선도 및 특정 모드에 대응하는 초음파 입사각을 계산하였다. 수신된 유도초음파에 대하여 short time Fourier transform을 이용한 시간-주파수 분석을 통하여 유도초음파 모드를 확인하였다. 실험적으로 유도 초음파가 증기발생기 세관의 곡관 부분을 통과할 때 뚜렷한 모드 변환을 관측할 수 없었다. 유도 초음파를 이용한 증기발생기 세관의 최적 검사 모드를 제안하고 실험에 의하여 이를 확인하였다.

• 한국추진공학회지
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• 제17권5호
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• pp.54-59
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• 2013

현재 Micro Shock Tube는 다양한 공학응용분야에 적용되고 있으며, 특히 우주항공 및 연소기술 그리고 약물전달 등의 분야에서 광범위한 잠재력을 가진 장치 중 하나이다. 그러나 Micro Shock Tube에서의 유동 특성은 작은 직경으로 인해 형성되는 매우 낮은 Reynolds Number와 높은 Knudsen Number의 영향으로 일반적으로 잘 알려진 Macro Shock Tube의 유동 특성과 상이하게 나타난다. 본 연구에서는 이러한 Micro Shock Tube의 유동 특성을 상세히 연구하기 위해 직경이 다른 두 가지 Micro Shock Tube의 실험을 수행하였다. 충격파 전파를 측정하기 위해 고압관의 파막압력 그리고 저압관의 세 지점에 센서를 설치하여 압력을 측정하고 분석하였다. 본 연구로부터, 동일한 파막압력에서 Micro Shock Tube 직경의 증가에 따라 충격파 전파속도가 증가하였고, 반사파의 영향도 더 크게 받았다.