• 청정기술
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• 제23권1호
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• pp.42-53
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• 2017

탈질과 탈황을 동시에 수행하는 과산화수소($H_2O_2$) 수용액 세정탑의 반응효율을 증가시키기 위해 예혼합이 이루어지는 혼합 냉각기(mixing quencher) 영역 내부의 유체유동에 대한 수치해석이 수행되었다. 산업공정에서 상용화되고 있는 세정탑 전단부의 혼합냉각기에서 과산화수소 수용액이 주입되는 노즐의 분사방식은 배기가스와 과산화수소 수용액의 혼합에 중요한 역할을 하며, 혼합냉각기에서의 혼합도는 세정탑 의 효율을 결정하는 중요 요소가 된다. 본 연구에서는 혼합냉각기 내부유체의 농도분포 개선을 목적으로 하여 혼합냉각기 내의 노즐 관의 배열을 조절하거나 노즐 팁 각도를 변경하며 유체혼합을 최적화하였다. 전산해석은 이 냉각기영역의 내부유동 및 각 유체 농도에 대한 RMS (root mean square) 값을 계산하여 내부유체의 혼합도의 개선을 확인하였다. 세부적으로는 노즐 관의 위치를 조절할 때 변경되는 냉각기 영역 후단의 농도 RMS 값을 확인하여 난류형성위치에 따른 최적화된 혼합도를 확인하였으며 기본형상 대비 난류형성방향을 조절하는 목적의 노즐 팁 각도를 증감하여 농도분포의 균질화를 비교하였다. 노즐 관의 배열에 따라 난류형성위치와 그에 따른 유체혼합이 해석되었다. 또한 노즐 팁 각도를 조절하는 경우에는 유동방향과의 각도에 따라, 흐름이 병류와 향류에 따라 혼합도의 최적화를 확인할 수 있었다. 노즐 관의 위치는 0.3 m, 노즐 팁은 병류의 $15^{\circ}$일 때 최적의 조건을 가지며 가장 낮은 RMS 값인 12.4%를 가졌다.

• 대한기계학회논문집B
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• 제22권4호
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• pp.417-427
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• 1998

The effect of secondary flow on the heat transfer of a turbulent wake generated by a flat plate was experimentally investigated. The secondary flow was induced in a curved duct in which the flat plate wake generator was installed. All three components of turbulent heat flux were measured in the plane containing the mean radius of curvature of the curved duct. The results showed that mean temperature profiles deviate from the similarity of the straight wake because of the cold fluid transported from the free-stream. The half-width of the mean temperature profile increased rapidly by upwash motion of the secondary flow. The changes to turbulence structure caused by the secondary flow show more pronounced effect on heat transport than on momentum transport. This is because the response to the variation of flow conditions is delayed in temperature field. Negative production of the turbulent heat flux is observed in the inner wake region. From the conditional averaging, it has been found that the negative production of the turbulent heat flux is generated due to a mixing process between the hot and low momentum eddies occupied in the inner wake region and the cold and high momentum eddies in the potential region.

• 대한설비공학회:학술대회논문집
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• 대한설비공학회 2009년도 하계학술발표대회 논문집
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• pp.590-595
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• 2009

PMV and ADPI were numerically investigated in a large space of various ceiling height with air-conditioning systems of two type. The numerical results showed that it is small that the growth of cooling load according to ceiling height rise in a large space without windows. In case of system air-conditioner of duct type embedded in the ceiling, the air mixing effect in indoor is superior to a case installed 4way cassette type in it. For controling thermal comfort at indoor, a system air-conditioner of duct type embedded in the ceiling is little influenced according to ceiling height rise in a large space considered.

• 대한기계학회논문집B
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• 제29권5호
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• pp.590-598
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• 2005

The present study has been conducted to investigate the effect of discrete ribs and rotation on heat/mass transfer characteristics in a two-pass square duct with $90^{\circ}-rib$ turbulators. The rib turbulator has a square cross section of 1.5 mm. The rib height-to-hydraulic diameter ratio $({e/D_{h})$ is 0.056, and the rib pitch-to-rib height ratio (p/e) is 10. The gap width is the same as the rib height. The rotation number ranges from 0.0 to 0.2 while Reynolds number is fixed to 10,000. In a stationary duct, the heat/mass transfer on the surfaces with discrete ribs is enhanced because the gap flow promotes local turbulence and flow mixing near the ribbed surface. In a rotating duct, the gap flow affects differently the heat/mass transfer on leading and trailing surfaces with discrete ribs. On the leading surface of the first pass, heat/mass transfer is increased due to the gap flow. On the trailing surface of the first pass, however, heat/mass transfer is decreased because the gap flow disturbs reattachment of main flow. The phenomenon, that is, the difference of heat transfer between the leading and the trailing surfaces is distinctly presented by rotation.

• 동의생리병리학회지
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• 제16권2호
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• pp.373-379
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• 2002

This paper was the design of aerosol generator for inhalation toxicology study of lead and evaluation with real time monitoring, and applied several engineering methodology to classical aerosol generator to cope with it's disadvantages. According to the testing conditions, source temperature 50℃ and inlet-duct band heater temperature 150℃, aerosol generation results for sodium chloride and lead acetate were as followings: CPM(Count Per Minute) for Sodium chloride that used for the testing material in aerosol generation and inhalation system was decreased in the 2nd and the 3rd hour's serial trials, but CVs(coefficient of variation) were maintained within 10%. CPMs for 5 and 2.5 gram of lead acetate that used for aerosol generation and inhalation exposure of lead showed similar results because of the sedimentation of lead acetate on piezoelectric crystal with time. For that reason, heating and mixing of nebulizing solution will be needed to generate lead aerosol with stable profile and maximum generation efficiency. Fluctuations of 10 and 5 gram lead acetate were low but 2.5gram was high. However, CVs for 10, 5, and 2.5gram lead acetate were within 10%. Considering the theoretical efficiencies for sodium chloride and lead acetate, 5gram sodium chloride and 2.5gram lead acetate were appropriate choice. Aerosol generation characteristics for two materials with 1 hour interval were different with respect to the fluctuation of CPM and the decrease to 10gram in it's material. For that reason, sodium chloride can not be used to estimate the aerosol generation and it's related parts for lead acetate. According to the testing conditions, source temperature 20, 50, 70℃, and inlet-duct band heater temperature 20, 50, 100, 150, 200℃, aerosol generation results for sodium chloride and lead acetate were as followings: Excluding inlet-duct band temperature 200℃, maximum CPM for sodium chloride was manifested in source temperature 70℃ with each inlet-duct band temperature conditions. We suggest that this condition was the optimum in the design of aerosol generator, inhalation system, and the testing. Maximum CPMs for 10, 5, and 2.5gram sodium chloride were from source temperature 70℃ and inlet-duct band temperature 20℃. Excluding inlet-duct band temperature 50, 200℃, maximum CPMs for lead acetate were indicated in source temperature 50℃ with each inlet-duct band temperature conditions. We suggest that this condition was the optimum in the design of aerosol generator, inhalation system, and the testing for lead inhalation study. Source and inlet-duct band temperatures for 10, 5, 2.5gram lead acetate were 50 and 100℃, 50 and 100℃, 50 and 150℃, respectively. In conclusion, considering above 2 paragraphs of results for aerosol generation, 5gram efficiencies for sodium chloride, lead acetate were higher than 2.5gram's. If inlet-duct band temperature was same, aerosol generation was increased with increase of source temperature. To get maximum aerosol generation will be the conditions that set the appropriate inlet-duel band temperature for each materials and increase the source temperature.

• 한국산학기술학회논문지
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• 제21권10호
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• pp.317-324
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• 2020

천연가스를 연료로 사용하는 복합화력발전소는 석탄화력 대비 기동 및 정지가 용이하고 오염물질의 배출에 대한 부하가 적어 국내 발전설비 중 차지하는 비중이 꾸준히 상승하고 있다. 그러나 복합화력발전소는 가스터빈의 기동초기 및 저부하 운전 영역에서 황연현상을 일으키는 이산화질소(NO2)의 농도가 높은 특성을 가지고 있어 민원의 원인이 되며, 이의 제어 기술로서 황연제거설비가 2000년대 중반에 개발되어 운영되어 지고 있었다. 하지만 이 기술은 가스터빈 냉간기동 조건에서 기동초기 약 10~20분 동안은 기화시스템의 예열이 충분하게 이루어 지지 않아 황연현상을 제어할 수가 없는 실정이었다. 이에 본 연구에서는 환원제를 기화기를 사용하지 않고 액상의 상태로 가스터빈 Exhaust Duct에 직접 분사하여 황연현상을 제어하는 기술의 도출을 위해 CFD 해석 및 실증시험을 수행하였다. 가스터빈 Exhaust Duct에 위치에 있는 Diffuser에 의해 Duct의 외곽으로 형성된 배기가스에 액상의 환원제를 직분사하는 방안으로 배기가스 조건에 따라 5가지 Case로 분류하여 CFD를 수행하였으며, 그 결과 5가지 Case 모두에서 RMS가 15%이하로 양호한 혼합도를 보였다. 이를 바탕으로 실증설비를 설치 및 시험을 실시한 결과, 기존 기상주입방식에서 제어할 수 없었던 기동 초기 약 10~20분 구간의 황연현상도 완벽하게 제어할 수 있었다.

• 한국표면공학회지
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• 제46권3호
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• pp.133-138
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• 2013

We have developed a 2D axi-symmetric numerical model for an inductively coupled plasma system in order to analyze gas mixing effect through a narrow gap shower head. For frictional flow, holes of 0.5 mm diameter and 2 mm length are approximately modeled in 2D. Gas velocity distribution 10 mm below the shower head showed 2 times difference between the center and the edge at 10 mTorr. At 10 mm above the wafer, it was increased to 6 times difference due to the pumping duct effect. The model with a 5 mm height buffer region of a shower head showed reasonable behavior of Ar discharge. The density of Ar metastable showed additional peak inside the buffer region around the edge holes.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1670-1675
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• 2004

A thermal vapor compressor in which the subsonic/supersonic flow appears simultaneously, has been accurately designed through the CFD analysis for the various shape parameters such as the primary nozzle shape, converging duct shape. mixing tube diameter, and so on. The performance of the developed thermal vapor compressor has been experimentally verified to be installed in a Multi Effect Desalination(MED) plant as an important element, In this paper, the experimental results for Various boundary conditions(motive pressure, suction pressure, and discharge pressure) are presented in comparing with CFD results. The two results show a good agreement with each other within 3.5 % accuracy with regard to the entrainment ratio.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2002년도 제18회 학술발표대회 논문초록집
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• pp.50-54
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• 2002

With a view to estimating the effect of flows on evolving sprays and combustion in ramjet combustor and corresponding extent of combustion, ram air flows in combustion chamber is numerically experimented. Preconditioned three dimensional Navier-Stokes system of equations per transient, compressible, turbulent flows in IRR(Integral Rocket Ramjet) combustor is numerically integrated. Flow properties in the side-dump ramjet combustor, rectangular duct with two 60-deg curved inlets located radially at an angle of 180-deg, are addressed in terms of mixing quality and extent of combustion efficiency.

• 대한기계학회논문집
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• 제19권5호
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• pp.1291-1299
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• 1995

In confined coaxial jets, the flow-mixing characteristics depend on the initial conditions at the nozzle outlet such as velocity ratio and nozzle radius ratio. In this study, nozzle ratio(inner/outer) was 0.3. Longitudinal axial velocity, turbulent intensity and Reynolds shear stress were measured by CTA. Measurements were made from the duct inlet to the region where similarity solution could exist. This study investigated flow charicteristics according to the variation of similitude parameter which was derived from the theory of Craya-Cutet. The range of similarity region depends on the variation of the similitude patameter. The form factor obtained from the axial velocity profile in the similarity region was constant. The higher the similitude parameter, the wider the spread rate of the jets. Due to this fact, the similarity conditions developed more quickly and the region where the similarity holds became narrow. Present experimental data confirmed the validity of Craya-Curtet theory.