• 한국자동차공학회논문집
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• 제6권6호
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• pp.132-141
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• 1998

Particle image velocimetry(PIV), a planar measuring technique, is an efficient tool for studying the complicated flow field such as in-cylinder flow, and intake port flow. PIV can be also used for analyzing the integral length scale of turbulence, which is a measure of the size of the large eddies that contain most of the turbulence kinetic energy. In this study, dual color scanning PIV was designed and demonstrated by using a rotating mirror and a beam splitter. This PIV system allowed enlargement of flexibility in the intensity of vectors to be calculated by spatial filtering technique, even in combustion chamber with high velocity gradient and high vorticity$({\sim}1000s^{-1})$. A new color image processing algorithm was developed, which was used to find the direction of particle movement directly from the digital image. These measuring techniques were successfully applied to obtaining the turbulence intensity (~0.1m/s) and the turbulent integral length scale of vorticity(~1mm).

• 한국분무공학회지
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• 제24권3호
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• pp.137-144
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• 2019

The Y-jet nozzle has benefits such as simple design and wide operating conditions. Because of these benefits, it is used in various combustion devices including industrial boilers. The most important variables in the design of the Y-jet nozzle are the mixing chamber length, the supply diameter of the liquid fuel and gas, and the exit orifice diameter. In addition, because of the use of a twin-fluid, optimized data is required depending on the spray condition. In this study, spray experiment was carried out under the pressure condition of 7 bar or more, which is the spraying condition used in industry. There was no change in flow rate with the length of the Y-jet nozzle mixing chamber, but the difference in SMD was confirmed. Adjusting the exit orifice diameter is most important to achieve the desired flow rate. Changes in the liquid and gas inlet port diameters ratio were found to be help improve the operating range and significant difference in SMD was observed.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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• pp.288-293
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• 2006

본 논문은 축소형 액체로켓엔진 연소기의 성능 및 연소특성에 관한 것이다. 축소형 연소기는 분사기 헤드부, 내열재 실린더부, 그리고 강제 물냉각 노즐부로 구성되어 있다. 분사기 헤드부는 18개의 주분사기와 한 개의 점화기용 분사기로 구성되어 있다. 분사기의 형태는 동축 와류형 분사기이며, 리세스 길이에 따른 4종류의 분사기를 적용한 각각의 축소형 연소기의 연소시험 결과, 성능 비교 및 정압, 동압 특성에 대해 기술하였다. 또한 설계점 및 탈설계점에서의 연소특성에 대해서도 기술하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.407-410
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• 2005

고성능 액체 로켓엔진에서 일반적으로 사용되는 기체-액체형 분사기가 장착된 연소실의 음향장을 수치적으로 해석하였다. 해당 분사기는 반파장 공명기의 역할을 할 수 있다. 다수의 공명기가 장착된 경우 연소실과 분사기간의 음향학적인 연계성으로 특이한 음향학적 특성이 관측되었다. 분사기 길이가 반파장 공명기 길이에 도달함에 따라 분사기와 연계된 새로운 음향 모드가 나타났으며, 그 음향 모드의 감쇠인자는 상당히 작았다. 따라서, 분사기의 음향감쇠 효과를 최적화 하려면 본래의 반파장 길이보다 약간 작은 길이를 갖도록 해야함을 알았다.

• 한국안전학회지
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• 제27권6호
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• pp.70-77
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• 2012

Experimental investigations were performed to examine the characteristics of propagating flame fronts around multiple bars within a rectangular chamber. The explosion chamber is 400 mm in height, $700{\times}700mm^2$ in cross-section and has a large top-venting area, $A_v$, of $700{\times}210mm^2$. This results in a value of 0.44 for $A_v/V^{2/3}$ and a L/D value of 0.57. The multiple obstacles of length 700 mm with a blockage ratio of 30 % were placed within the chamber. Temporally resolved flame front images were recorded by a high speed video camera to investigate the interaction between the propagating flame and the obstacles. Results showed that the flame propagation speeds before the flame impinges onto the obstacle almost equal to the laminar burning velocity. As the propagating flame impinged on the obstacle, the central region of flame began to become concave, this resulted in the flame deceleration in the region. As the flame interacted with the modified flow filed generated behind the central obstacle, the probability density functions(PDFs) of the local flame displacement speed were extensively distributed toward higher speeds.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.251-255
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• 2005

본 연구에서는 스월 인젝터의 기하학적 형상에 따른 분무특성 파악을 위해 액막두께 측정방법을 사용하였다. 액막두께 측정을 위해 특별히 제작된 인젝터를 사용하였으며, 백홀과 스월챔버 그리고 오리피스의 길이에 따른 분무특성을 확인하였다. 분무특성 파악을 위해 분사압에 따른 유량변화, 오리피스 하단의 액막두께와 분무각을 측정하였다.

• 대한기계학회논문집B
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• 제29권11호
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• pp.1248-1256
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• 2005

This study was undertaken to investigate the flow characteristics of emulsified fuel with the ultrasonic energy-adding system by using the chaotic method. Efffcts of water contents within emulsified fuel, flow rate and tube length with 5m in diameter from an emulsified chamber has been discussed on the strange attractor and power spectral density function. Five probe sensors were set up from 0.5 to 2.5m by length in 0.5m increments in the tube. In particular, the chaotic features of this system have been practically characterized in terms of chaotic statistics such as the power spectral density function and phase space portraits by resorting to the somewhat noble deterministic chaos theory. In the tube, the dominant frequency increased with increasing water contents and flow rate, but decreased a little with an increase in the length from the emulsified chamber.

• 한국안광학회지
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• 제16권3호
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• pp.293-297
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• 2011

목적: 본 연구는 고령의 성인을 대상으로 굴절이상과 안광학 성분들 사이의 연관성을 알아보고자 하였다. 방법: 안과적 수술을 받지 않은 고령의 95명을 대상으로 굴절이상과 각막곡률반경, 각막굴절력, 안축장, 전방깊이, 수정체 두께를 측정하고 분석하였다. 결과: 안축장(AL)/각막곡률반경(CR) 비와 각막굴절력, 안축장, 전방깊이는 양의 상관관계를 보였고(r=0.510, r=0.439 r=0.411), AL/CR 비와 각막곡률반경과는 음의 상관관계를 나타냈다(r = -0.516). 각 막굴절력과 안축장 사이에서 가장 높은 연관성(r = -0.545, p=0.000)을 보였으며 굴절이상과 AL/CR 비는 음의 상관관계로 분석되었다(r = -0.359). 결론: 눈의 굴절이상을 진단하는데 AL/CR 비가 고령의 성인에서 중요한 지표자료임을 알 수 있었다.

• 한국의학물리학회지:의학물리
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• 제33권1호
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• pp.1-9
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• 2022

Purpose: To evaluate the effective volume of the Korea Research Institute of Standards and Science free air chamber (KRISS FAC) L1 used for the primary standard device of the low-energy X-ray air kerma. Methods: The mechanical dimensions were measured using a 3-dimensional coordinate measuring machine (3-d CMM, Model UMM 500, Carl Zeiss). The diameter of the diaphragm was measured by a ring gauge calibrator (Model KRISS-DM1, KRISS). The elongation of the collector length due to electric field distortion was determined from the capacitance measurement of the KRISS FAC considering the result of the finite element method (FEM) analysis using the code QuickField v6.4. Results: The measured length of the collector was 15.8003±0.0014 mm with a 68% confidence level (k=1). The aperture diameter of the diaphragm was 10.0021±0.0002 mm (k=1). The mechanical measurement volume of the KRISS FAC L1 was 1.2415±0.0006 cm³ (k=1). The elongated length of the collector due to the electric field distortion was 0.170±0.021 mm. Considering the elongated length, the effective measurement volume of the KRISS FAC L1 was 1.2548±0.0019 cm³(k=1). Conclusions: The effective volume of the KRISS FAC L1 was determined from the mechanically measured value by adding the elongated volume due to the electric field distortion in the FAC. The effective volume will replace the existing mechanically determined volume in establishing and maintaining the primary standard of the low-energy X-ray.

• 한국추진공학회지
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• 제18권1호
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• pp.50-57
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• 2014

70 N급 액체로켓엔진 개발모델의 추력실 최적설계형상 도출을 위한 지상연소시험을 수행하였다. 단일추진제급(순도: ${\geq}98.5%$) 하이드라진이 연소시험용 추진제로 선정되었고, 특성길이($L^*$) 2.79, 2.95, 그리고 3.13 m를 갖는 추력실에 대한 성능평가가 수행되었다. 시험조건 내에서의 촉매대 $L^*$ 증가는 추력기의 성능저하를 야기하는 것이 관찰되었으며, 개발모델의 펄스응답 성능이 현재 상용화되어 있는 하이드라진 추력기와 비교하여 우수한 것이 확인되었다.