• 한국생산제조학회지
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• 제21권3호
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• pp.415-420
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• 2012

Dust collecting performance of axial-vane type cyclone for oil mist was analyzed in this study. For predicting cut diameter size of cyclone, the number and angle of vane (${\beta}_2{^{\prime}}$) was calculated by CFD. As the result, ${\beta}_2{^{\prime}}$ was decreased as the number of vane was increased and the angle of inclination (${\beta}_2{^{\prime}}$) decreased, and it cause strong swirl flow. Therefore, it could be confirmed that as the number of vane was increased and the angle of inclination was decreased, cut diameter size was decreased. Also, by verifying the results of CFD through experiment, the cut diameter size could be 2 ${\mu}m$ at 4 $m^3/min$ of flow rate.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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• pp.457-460
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• 2012

본 연구는 7톤급 연소기용 분사기 검증을 위한 축소형 연소기의 설계 및 제작에 관한 것이다. 7톤급 연소기의 헤드부는 90개의 동축 와류형 분사기로 구성되며, 연소실은 케로신 재생냉각 일체형 연소기이다. 7톤급 연소기에 적용할 분사기로 차압 및 리세스 수를 달리한 분사기를 설계하였다. 설계된 분사기를 실물형 연소기에 적용하기 전 축소형 연소기에 먼저 적용하여 분사기 작동성 및 성능검증을 하고자 한다. 축소형 연소기는 분사기 19개로 구성되며, 연소압력 70 bar, 총 추진제 유량은 4.3 kg/s, 혼합비는 2.45이다.

• 청정기술
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• 제26권3호
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• pp.211-220
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• 2020

본 연구는 80 kW급 단일버너 연소로에서 석탄 연소시 초저 NOx 버너 설계인자를 평가하기 위한 실험적 연구이다. 버너 설계 인자인 선회강도, 총 과잉 공기비, 버너 영역 과잉공기비, 1차/2차 산화제 비율, OFA 비율을 변경하여 총 81개 조건을 대상으로 실험을 수행 하였다. 실험 결과, 선회류가 약하면 연소로 출구에서 CO가 증가하고 연소로 내부 온도가 감소하는 것으로 나타났다. 그러나, 선회류가 강하면 NOx가 증가하기 때문에 적절한 선회류 강도를 결정하는 것은 NOx를 줄이는 데 중요한 요소이다. 1차/2차 산화제의 비율 또한 중요한 요소이며, 생성 된 NOx의 양은 산화제의 비율에 따라 달라진다. 2차 산화제의 비율이 증가하면 연소 초기에 NOx 방출량이 증가하고, 측정 된 배출구 NOx가 증가하게 된다. 그러나, 2차 산화제 비율이 감소하면 화염이 길어지고 CO가 증가한다. 본 연구에 사용 된 연소 시스템은 적절한 조건이 만족 될 때 O₂ 6%를 기준으로 최소 NOx가 82 ppm 생성되는 것으로 확인 되었다. 본 실험에서 대상으로 한 버너는 연소용 공기를 석탄을 이송하는 1차공기 외에 2차공기로 하나의 산화제 유동만 사용하는 방식으로서 추후 3차 및 4차공기로 분할하여 화염형태 및 반응을 세밀하게 제어할 경우 추가적인 NOx 감소가 가능할 것으로 예상된다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.720-726
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• 2001

Two-dimensional, angle-resolved LDV(Laser Doppler Velocimetry) measurements of the turbulent rotating flow field in a confined cylinder have been performed. The configurations of interest are flows between a rotating upper disk with a rod attached by a disk or impeller(${\theta}= 90^{\circ},\;45^{\circ}$) and a stationary lower disk in a confined cylinder. The mean flow velocity as well as the turbulent intensity of the flow field have been measured. The results show that the flow is strongly dependent on the position of the impellers or the disk, negligibly affected by the Reynolds number in turbulent flow. It is observed that the mixing effect of the axial flow impeller(${\theta}= 45^{\circ}$) is better than that of the radial flow impeller(${\theta}= 90^{\circ}$) or a disk.

• 한국자동차공학회논문집
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• 제4권5호
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• pp.197-205
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• 1996

The flow characteristics of five different 4-valve cylinder heads were investigated in a steady flow rig using laser-Doppler velocimetry. The tumble flow of each head with pentroof combustion chamber was quantified by nondimensional tumble number using a tumble adaptor. The formation of tumbling vortex was examined in an optical single-cylinder engine which has windows for in-cylinder LDV measurements. Tumble vortex ratio was estimated from the tumble flow measurement. The four-valve cylinder heads with pent-roof combustion chamber showed the tumble vortex from the intake process, which was investigated in the steady flow test. The tumble adaptor which converts the tumble into swirl flow was found to be feasible in predicting the tumble flow in the real engine. The tumble strength in the steady flow test coincides with that in the real engine experiment within 15%. It was found that the steady flow test on the four-valve cylinder heads provides the tip for a better design of cylinder head.

• 한국가시화정보학회:학술대회논문집
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• 한국가시화정보학회 2004년도 추계학술대회 논문집
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• pp.102-103
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• 2004

Simultaneous CH and OH planar laser induced fluorescence(PLIF) and stereoscopic particle image velocimetry(PIV) measurements have been developed to investigate the local flame structure of turbulent premixed flames. The developed simultaneous two radical concentrations and three component velocity measurements on a two-dimensional plane was applied for relatively high Renolds number turbulent premixed flames in a swirl stabilized combustor. All measurements were conducted for methane-air premixed flames in the corrugated flamelets regime. Strong three-dimensional fluctuation implies that misunderstanding of the flame/turbulent interactions would be caused by the analysis of two-component velocity distribution in a cross section. Furthermore, comparisons of CH-OH PLIF and three-component velocity field show that the burned gases not always have high-speed velocity in relatively high Renolds number turbulent premixed flame.

• 한국분무공학회지
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• 제1권3호
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• pp.51-59
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• 1996

An experiment was carried out on the structure of twin spray from pressurize-swirl nozzles, in order to investigate the effect of different size of spray nozzles on the characteristics of the overlap of two single sprays, for example, mean diameter, number density, and spatial distribution of flow rate. Using image processing method, the distributions of size and velocity of droplets of a single spray and twin spray were measured and compared to investigate the overlapping effect of two identical sprays. Comparing experimental results from a twin-spray with those from two-single sprays shows that the flow rate distribution of the twin-spray was concentrated around the midst of the overlapping region of two sprays. In this region, Sauter mean diameter (SMD) did not change much in the twin spray from 6032 nozzles, but it was smaller by 10 micrometers in the twin-spray than two-single sprays from 60063 nozzles. In spite of large difference in Weber numbers of the colliding sprays between the 60063 and 6032 nozzles, the phenomena did not have a big change in the overlapping region of twin spray. This shows that in the collision between droplets from two single spray in the overlapping region to cause the disruption of droplets, the size distribution of spray droplets was also important as well as Weber number.

• 한국가시화정보학회지
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• 제8권3호
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• pp.1-5
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• 2010

The 14th International Symposium on Flow Visualization (ISFV14) was held at Daegu (Korea), June 21-24, 2010. The number of participants was 304 from 17 countries. The number of papers presentated was 243 from 19 countries. Two special lectures and four invited lectures, 48 paper sessions, and one poster session were opened in five and in a lobby for four days. Special events such as awarding "the Asanuma Award" and "the Leonardo Da Vinci Award" to the prominent contributors were also held. Photo and Movie Awards were given to three scientists for the excellences in their photos and movies. Among 48 sessions 5 sessions were on Biological Flows and on Micro/Nano Fluidics, which were the largest session number. 4 sessions were held on Compressible and Sonic Flows, and on PIV/PTV. 3 sessions were held on Swirl Flows, Image Processing, and on Industrial Applications. Other sessions on LIF, Wake and Vortex Flows, Physiological Flows, Environment Flows, Measurements Techniques, and on Reacting Flows.

• 대한기계학회논문집B
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• 제40권11호
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• pp.727-736
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• 2016

본 연구에서는 복합화력 화력 발전소용 고압 다단펌프의 레이디얼 디퓨저 형상에 따른 펌프의 성능(양정, 효율)변화를 수치 해석적으로 분석하였다. 레이디얼 디퓨저 설계 변수는 크게 디퓨저 베인수, 디퓨저 외경비($D_4/D_3$), 리턴채널 출구각도(${\alpha}_6$), 압력회복계수($C_p$) 등으로 선정하였다. 수치해석 결과 디퓨저 외경비가 큰 경우 양정 및 효율이 가장 크게 예측되었으며, 리턴채널의 출구각도(${\alpha}_6$)가 60도인 경우 디퓨저 출구에서의 Pre-Swirl로 인해 출구각도가 90도인 것에 비해 양정이 저하되는 것을 알 수 있다.

• 한국항공우주학회지
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• 제34권7호
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• pp.97-104
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• 2006

분사조건과 주위기체 압력에 따라 스월 인젝터의 분무각과 분열길이를 측정함으로써, 스월 인젝터의 분무 및 분열특성에 대한 연구를 수행하였다. 분사조건으로 축방향 We 수(Wel)를 1554까지 주위기체 압력을 4.0MPa까지 증가시켰다. Wel과 주위기체 밀도(ρ)가 증가함에 따라 공기역학적 힘이 증가하여 원추형 액막 표면의 교란이 증가하게 되고, 따라서 분열이 빨리 일어난다. 결과에 따르면 주위기체 밀도에 따른 분무각의 변화가 분열이 일어나기 전과 후가 다르게 나타났다. 분열이전에는 분무각이 주위기체 밀도 변화에 관계없이 거의 일정하였으나, 분열이 일어나게 되면 분무각이 감소하게 된다. 또한 측정된 분열길이를 선형불안정이론과 비교해 보았는데, 액막두께의 감쇠를 고려한 수정된 이론이 측정결과와 상당히 유사한 결과를 얻을 수 있었다.