• Current Optics and Photonics
• /
• 제2권6호
• /
• pp.519-524
• /
• 2018

We propose a transverse load sensor with reconfigurable measurement accuracy based on a microwave photonic filter in the $K_u$ band, incorporating a polarization-maintaining fiber Bragg grating. A prototype sensor with a reconfigurable measurement accuracy tuning range from 6.09 to 9.56 GHz/(N/mm), and corresponding minimal detectable load range from 0.0167 to 0.0263 N/mm, is experimentally demonstrated. The results illustrate that up to 40% manufacturing error in the grating length can be dynamically calibrated to the same corresponding measurement accuracy for the proposed transverse load sensor, by controlling the semiconductor optical amplifier's injection current in the range of 154 to 419 mA.

• 한국분무공학회지
• /
• 제12권2호
• /
• pp.115-122
• /
• 2007

The spray characteristics and drop size measurements have been experimentally studied in liquid jets injected into subsonic crossflow. With water as fuel injection velocity, injection angle and atomize. internal flows were varied to provide of jet operation conditions. The injector internal flow was classified as three modes such as a non-cavitation flow, cavitation, and hydraulic flip flows. Pulsed Shadowgraph Photography measurement was used to determine the spatial distribution of the spray droplet diameter in a subsonic crossflow of air. And this study also obtains the SMD (Sauter Mean Diameters) distribution by using Planar Liquid Laser Induced Fluorescence technique. The objectives of this research are get a droplet distributions and drop size measurements of each condition and compare with the other flow effects. As the result, This research has been showned that droplet size were spatially dependent on air-stream velocity, fuel injection velocity, injection angle effects, and normalized distance from the injector exit length(x/d, y/d). There are also different droplet size characteristics between cavitation, hydraulic flip and the non-cavitation flows.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2008년 영문 학술대회
• /
• pp.486-491
• /
• 2008

The spray characteristics and drop size measurements have been experimentally studied in liquid jets injected into subsonic crossflow. With water as fuel injection velocity, injection angle and atomizer internal flows were varied to provide of jet operation conditions. The injector internal flow was classified as three modes such as a non-cavitation flow, cavitation, and hydraulic flip flows. Pulsed Shadowgraph Photography measurement was used to determine the spatial distribution of the spray droplet diameter in a subsonic crossflow of air. And this study also obtains the SMD(Sauter Mean Diameters) distribution by using PLLIF(Planar Liquid Laser Induced Fluorescence) technique. The objectives of this research are getting a droplet distribution and drop size measurement of each condition and compare with the other flows effect. As the result, This research have been showed the droplet size were spatially dependent on air-stream velocity, fuel injection velocity, injection angle effects and normalized distance from the injector exit length.(x/d, y/d)There are also different droplet size characteristics between cavitation, hydraulic flip and the non-cavitation flows.

• 한국항공우주학회지
• /
• 제37권9호
• /
• pp.879-888
• /
• 2009

초음속 주 유동내 수소의 수직분사에 의한 비정상 반응 유동장에 대한 3차원 수치해석이 DES 난류 모델과 상세 화학반응 모델을 이용하여 수행되었다. 난류 반응 유동의 물리적 현상을 이해하기 위하여 해석 및 실험 결과를 비교하였다. 계산에 의해 구해진 OH 분포는 실험의 OH-PLIF 결과를 잘 모사하고 있다. 반면, 점화 지연 시간은 계산과 실험 사이에 차이를 보이고 있으며, 이는 실험적 계측의 한계에 기인하는 것으로 생각된다. RANS 및 DES 계산 결과의 비교로부터 간헐 현상을 확인하였으며, 유선을 따른 온도 분포 및 중첩된 OH 질량 분율을 통해 시 공간적 간헐 현상을 정량적으로 측정하였다.

• 한국항공우주학회지
• /
• 제37권9호
• /
• pp.863-878
• /
• 2009

초음속 주 유동내 연료의 수직분사에 따른 비정상 3차원 유동장을 DES 난류 모델을 이용해 모사하였다. 해석 결과는 시간에 따른 에디 거동 및 생성 빈도에 대해 실험과 비교되었으며, 에디 생성 메커니즘을 이해하기 위해 분사기 주변 와도에 대한 분석을 수행하였다. DES 난류 모델은 에디의 대류 특성을 비교적 정확하게 모사하고 있으나, 에디 생성빈도는 다소 과대 예측하고 있다. 분사기 상류 재순환 영역에서 엇회전하는 와류가 번갈아 떨어져 나가면서 에디 구조가 생성된다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2008년도 제31회 추계학술대회논문집
• /
• pp.447-448
• /
• 2008

The goal of this study is to find flame dynamic behavior using a transverse fuel injection in a model combustor, and is to investigate main causes of unstable combustion in a liquid-fueled combustor. For transverse fuel injection into air cross flow, spray result shows similar tendency with Wu et al.[1998] until spray arrives at flame-holder. However, passing through flame-holder, fuel inflow into recirculation region of flameholder is not sufficient so it makes large difference between shear flame and recirculation flame behind flameholder. In combustion tests, the stable flame shows a kind of shear flames and low peaks of dynamic pressure frequencies. On the other hand, unstable flame shows periodic detached flame in recirculation zone and a strong peak of dynamic pressure frequency. The instability frequency is highly affected by influx air velocity, air temperature, equivalence ratio and wake or vortex shedding frequency behind the flameholder.

• The Korean Journal of Pain
• /
• 제24권3호
• /
• pp.141-145
• /
• 2011

Background: Stellate ganglion block is usually performed at the transverse process of C6, because the vertebral artery is located anterior to the transverse process of C7. The purpose of this study is to estimate the location of the transverse process of C6 using the cricoid cartilage in the performance of stellate ganglion block. Methods: We reviewed cervical lateral neutral-flexion-extension views of 48 patients who visited our pain clinic between January and June of 2010. We drew a horizontal line at the surface of the cricoid cartilage in the neutral and extension views of cervical lateral x-rays. We then measured the change in the shortest distance from this horizontal line to the lowest point of the transverse process of C6 between the neutral and extension views. Results: There was a statistically significant difference in the shortest distance from the horizontal line at the surface of the cricoid cartilage to the lowest point of transverse process of C6 between neutral position and neck extension position in both males and females, and between males and females in both neutral position and neck extension position. The cricoid cartilage level was 4.8 mm lower in males and 14.4 mm higher in females than the lowest point of transverse process of C6 in neck extension position. Conclusions: Practitioners should recognize that the cricoid cartilage has cephalad movement in neck extension. In this way, the cricoid cartilage can be still useful as a landmark for stellate ganglion block.

• 터널과지하공간
• /
• 제23권6호
• /
• pp.470-479
• /
• 2013

수압파쇄는 암반에서 유체의 흐름을 촉진시키기 위한 방법으로 사용되며 지열개발, 세일가스의 개발 등 최근 에너지 분야에서 그 어느 때 보다 활발한 연구가 이루어지고 있다. 수압파쇄의 대상이 되는 암반은 등방성을 갖지 않는 경우가 대부분이며 일부 퇴적암층에서는 횡등방성 암반에서 수압파쇄가 이루어진다. 횡등방성 암반에서는 수압파쇄에서 발생하는 균열의 성장 방향이 반드시 최대주응력 방향과 일치하지 않으며 이방성 구조에 따라 변화하게 된다. 그러므로 이 연구에서는 입자결합모델을 이용하여 횡등방성 암석에서의 수압파쇄 특성을 고찰하고 분석하고자 하였다. 또한 실험실 규모의 수압파쇄 실험을 실시하여 수치해석 결과의 타당성을 분석하고자 하였다. 본 연구에서는 가압되는 유체의 점도 및 층리면의 각도 그리고 이방성에 의한 영향으로 균열의 성장 및 균열 패턴에 큰 차이를 보였으며, 횡등방성 모델의 경우 전단균열에 의한 수압파쇄 균열의 성장이 우세한 것으로 나타났다.

• 한국추진공학회지
• /
• 제22권3호
• /
• pp.53-64
• /
• 2018

본 논문에서는 초음속 유동장 내 연료 수직 분사 조건에서 분사구의 형상에 따른 연료/공기 혼합 특성을 분석하고자 하였다. 이를 위해 동일한 분사구 출구 면적과 유량 조건에 대해 수소와 공기에 대한 비반응 유동장 전산 해석을 수행하였다. 해석 결과의 검증을 위하여 자유류 마하수 3.38, 제트-자유류 운동량 플럭스비 1.4 인 평판 분사 시험을 모의하였다. 5개의 서로 다른 형상을 갖는 분사구를 이용하여 형태에 따른 박리 구간, 분사 제트의 구조의 차이를 살펴보고 분사구 후류에서 수소의 침투 높이와 수소-공기의 혼합에 따른 가연 면적에 변화를 확인함으로써 분사구 형상에 따른 연료/공기 혼합 특성을 정량적으로 비교하였다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2003년도 제21회 추계학술대회 논문집
• /
• pp.191-194
• /
• 2003

A series of computational simulations have been carried out for non-reacting and reacting flows in a supersonic combustor configuration with and without a cavity. Transverse injection of hydrogen, a simplest form of fuel supply, is considered in the present study with the injection pressure of 0.5 and 1.0 ㎫. The corresponding equivalence ratios are 0.17 and 0.33. The work features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the previous studies. In particular, oscillatory flow characteristics are captured at a scale sufficient to identify the underlying physical mechanisms. Much of the flow unsteadiness is related not only to the cavity, but also to the intrinsic unsteadiness in the flowfield. The interactions between the unsteady flow and flame evolution may cause a large excursion of flow oscillation. The role of the cavity, injection pressure, and amount of heat addition are examined systematically.