• Wind and Structures
• /
• 제36권3호
• /
• pp.175-200
• /
• 2023

The large eddy simulation (LES) of the flow around a circular cylinder is not only affected by the sub-grid scale (SGS) model but also by the grid resolution of the computational domain. To study the influence of different grids on the LES results, the LES simulations of the flow around a circular cylinder with different grids at Reynolds number (Re) = 3900 was performed. A circular computational domain with different radial growth rates and circumferential and spanwise grid numbers was adopted for the simulations. Meanwhile, the aerodynamic forces, wind pressure coefficients, mean and instantaneous flow fields, and the effect of grid resolution on them were comprehensively analyzed. The results indicate that the lift coefficient, wind pressure coefficient, and recirculation length are significantly affected by the radial growth rate of the grid and the circumferential grid number. The spanwise grid number has a significant influence on the three-dimensionality of the flow and plays an important role in velocity fluctuations in the wake region. Nevertheless, the aerodynamic coefficients and recirculation length are not sufficiently sensitive to the grid number in the spanwise direction. By comparing the results, it can be concluded that suitable and reliable LES results can be obtained when the radial growth rate is 1.03 or 1.05, the circumferential grid number is 160, 200, or 240, and the spanwise grid number is 64. A radial growth rate 1.05, circumferential grid number 160, and spanwise grid number 64 are recommended to reduce the grid amount and further improve the efficiency.

• International Journal of Aeronautical and Space Sciences
• /
• 제13권3호
• /
• pp.386-397
• /
• 2012

The stability and structure of bluff-body stabilized hydrogen flames were investigated numerically and experimentally. The velocity of coflowing air was varied from subsonic velocity to a supersonic velocity of Mach 1.8. OH PLIF images and Schlieren images were used for analysis. Flame regimes were used to classify the characteristic flame modes according to the variation of the fuel-air velocity ratio, into jet-like flame, central-jet-dominated flame, and recirculation zone flame. Stability curves were drawn to find the blowout regimes and to show the improvement in flame stability with increasing lip thickness of the fuel tube, which acts as a bluff-body. These curves collapse to a single line when the blowout curves are normalized by the size of the bluff-body. The variation of flame length with the increase in air flow rate was also investigated. In the subsonic coflow condition, the flame length decreased significantly, but in the supersonic coflow condition, the flame length increased slowly and finally reached a near-constant value. This phenomenon is attributed to the air-entrainment of subsonic flow and the compressibility effect of supersonic flow. The closed-tip recirculation zone flames in supersonic coflow had a reacting core in the partially premixed zone, where the fuel jet lost its momentum due to the high-pressure zone and followed the recirculation zone; this behavior resulted in the long characteristic time for the fuel-air mixing.

• 대한의용생체공학회:의공학회지
• /
• 제13권4호
• /
• pp.339-352
• /
• 1992

A numerical simulation of the steady and pulsatile flow across the end-to-side anastomosis was performed In order to understand the role of flow dynamics in the preferential bevel opment of distal anastomotic intimal hyperplasla. The finite element technique was employed to solve two-dimensional unsteady pulsatile flow in that region. The results of the steady flow revealed that low shear stresses occur at the proximally occluded host artery and at the recirculation region in the Inner wall just distal to the toe region of the anastomosis. The nor- mal;zed wall shear rate was increased, as was the recirculation zone size in the host artery of the by-pass graft anastomosis, with increased anastomotic junction angle. In order to min imize the size of the low wall shear region which might result in the intimal hyperplasia in the by-pass graft anastomosis, a smaller anastomotic junction angle is recommended. The pulsatile flow simulation revealed flow that regions of low and ascillating mali shear do exist near the anastomosis as In the steady simulation. The shift of stagnation point depends on the pulsation of the flow. As the flow was accelerated at systole, the stagnation point moved downstream, disappered at early diastole and reappeared during late diastole. Low shear stress was also found along both walls of the occluded proximal artery. However, the diastolic flow behavior is quite different from the steady results. The vortex near the occluded artery moved downstream and inwardly during late systole, and disappeared during diastole. Recirculations proximal to the toe and heel regions were significant during diastole. Shear stress oscillation was found along the opposite wall. The results of the present study revealed that tow shear occurs at the proximally occluded host artery aud the recirculation region in the inner wall Just dlstal to the toe region of the anastomosis. The present study suggested that the regions of fluctuated wall shear stress wit flow separation is correlated with the preferential developing regions of anastomosis neointial fibrous hyperplasia.

• 대한기계학회논문집B
• /
• 제37권2호
• /
• pp.161-170
• /
• 2013

Double cone 버너를 장착한 스월 예혼합 연소기에 대한 유동 및 연소 특성을 분석하여 swirler 모델을 이용한 수치적 모델링 방법을 제시하였다. 버너 출구에서 형성되는 내부 재순환 영역을 근사적으로 구현하도록 swiler의 내 외경을 각각 56 mm, 152 mm로 결정하였으며 이를 토대로 유량, 반경 반향 속도를 결정하였다. 접선 방향 속도의 설정을 위해 swirl 각도와 재순환 각도를 도입하였으며 40 m/s인 경우 유사한 내부 재순환 영역이 형성되었다. 라이너 출구에서 온도와 속도의 오차는 각각 2.8%, 0%로 작았지만, NOx의 경우 67% 가량 감소한 결과를 보였다. Swirler 모델은 EV 버너의 유동 및 연소 특성을 근사적으로 모사하는 모델의 하나로서 정량적 평가 인자에서 오차를 보이지만, 유동 및 화염, NOx 형성 영역의 경향성이 유사하므로 swirler 모델을 채택하여 복잡한 형상의 발전용 가스터빈 연소기의 효율적인 수치해석이 타당할 것으로 판단된다.

• 한국에너지공학회:학술대회논문집
• /
• 한국태양에너지학회, 한국에너지공학회 1993년도 춘계 공동학술발표회 초록집
• /
• pp.33-41
• /
• 1993

본 실험에서는 폐수, 지하수 등에 오염되는 유독성 유기물 처리를 위한 태양반응시스템의 개발을 위하여 실험실 규모의 recirculation형 광분해 반응시스템을 구성하여 유기물 분해를 실시하였다. 0,1 wt % Ti $O_2$ anatase촉매를 채택하고 30 ppm, 50 ppm, 80ppm의 TCE 초기농도에 대하여 동일한 실험조건에서 실험을 수행한 결과로부터 Langmuir - Hinshelwood kinetics equation을 이용하여 reaction constant, $k_{TCE}$와 adsorption constant, $K_{TCE}$를 구하였으며, 이들 갑으로부터 apparent first order reaction constant, k'를 비교하였다. Ti $O_2$ anatase, ZnO 그리고 F $e_2$ $O_3$ 광촉매들의 TCE분해에 미치는 영향을 관찰한 결과 동일 실험조건에서 Ti $O_2$ anatase가 가장 우수한 분해율을 보여주었다. 그리고 이성분 시스템(TCE＋Phenol)의 경우 phenol의 양이 TCE 분해율에 미치는 영향을 관찰하였는데 phenol의 양이 증가할수록 TCE의 분해율이 저하됨을 보여주었다.보여주었다.

• 한국자동차공학회논문집
• /
• 제17권4호
• /
• pp.79-85
• /
• 2009

Low temperature combustion regime for the simultaneous reduction of nitrogen oxides ($NO_x$) and paticulate matter (PM) is demonstrated in single cylinder engine at various operating parameters, such as EGR rate, injection timing, EGR temperature, amount of fuel and swirl rate. Low temperature combustion is accomplished by high exhaust gas recirculation (EGR) rate in this study. Generally, the emission of $NO_x$ almost completely disappears and PM significantly increases in the first decreasing regime of oxygen concentration but after peaking about 10~12% oxygen concentration, PM then decreases regardless of fuel injection quantity. Low temperature combustion regime was extended by low EGR temperature, high injection pressure and low amount of fuel.

• 한국수자원학회논문집
• /
• 제38권2호
• /
• pp.143-153
• /
• 2005

최근 들어 자연형 하천과 하천생태계 복원에 대한 관심이 점증하면서 수리학적 기능 외에, 다양한 생태환경을 제공하고 하안 부근의 경관을 개선하는 기능을 가는 수제에 대한 관심이 커지고 있다. 그러나 현재 국내에는 수제설치에 대한 설계지침이 충분치 않을 뿐 만 아니라 국내 수행된 연구 자료가 매우 부족한 실정이다. 이에 본 연구에서는 수제 설계인자 해석을 위한 수리모형실험을 수행하였다. 실험조건은 수제선단 흐름변화와 수제하류부 재순환영역에 대한 고정상실험으로 수제길이와 투과율을 조절하여 수행하였다. 주요 분석은 수제 선단에서는 중앙부 유속증가와 세굴의 영향인자인 유속과 편향각을 측정하여 수제 선단유속비와 면적비에 대한 실험식을 제안하였다. 또한 수제하류부 재순환 영역에서는 수제 설치의 주요요인인 수제간격의 기초 자료를 해석하기 위해 흐름분리 길이와 입사각의 변화를 분석하였으며 투과율과 수제 설치각에 대한 실험식을 제안하였다.

• 대한환경공학회지
• /
• 제22권11호
• /
• pp.1935-1944
• /
• 2000

본 연구에서는 하부가 활성탄 유동상이고 상부가 플라스틱 충전상인 혐기성 혼성 반응조에서 활성탄충의 유동을 위한 내부순환수의 인출지점이 폐수처리 효율에 미치는 영향을 파악하기 위하여 순환수 인출지점이 유동상 위(R1 반응조) 또는 충전상 위(R2 반응조)에 위치하는 2개의 반응조에 인공폐수를 주입하여 실험을 수행하였다. 연구 결과, $6.2kg\; COD/m^3-day$의 유기물부하(OLR)까지는 R2 반응조의 COD 제거효율이 85.0-95.2%로, R1 반응조보다 좋았으나 그 차이는 크지 않았으며, 그 이상의 OLR에서는 두 반웅조의 COD 제거효율이 크게 악화되었는데 R2 반응조보다 R1 반응조에서 그 경향이 더 심하였다. R2 반응조가 R1 반응조 보다 대략 2배의 넓은 OLR 영역에서 안정적으로 운전되었는데 R2 반응조의 최대 메탄생성량은 $13.3kg\;COD/m^3-day$의 OLR에서$5.5kg\;COD/m^3-day$이었다. 또한 R1 반응조에서는 $6.2kg \;COD/m^3-day$ 이상의 OLR에서, 그리고 R2 반응조에서는 $7.1kg\; COD/m^3-day$ 이상의 OLR에서 처리수의 유기산 농도가 크게 증가하는 경향을 나타내었으며, 그 경향은 R1 반응조에서 더 현저하였다. 결론적으로 활성탄충의 유동을 위한 내부순환수의 인출지점에 따라 반응조가 처리가능한 유기물 부하 범위가 달라졌는데, 유기물 부하가 높을수록 내부순환수의 인출지점을 반응조 부피 전체를 이용할 수 있도록 충전상의 상부에 위치시키는 것이 더 바람직한 것으로 판단되었다.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2012년도 제45회 KOSCO SYMPOSIUM 초록집
• /
• pp.179-182
• /
• 2012

Effect of double post injections on diesel PCCI combustion with focus on HC emission was investigated in a single-cylinder direct-injection diesel engine. The ISFC, HC and CO emissions were reduced by single or double post injections. The application of double post injections could also improve the trade-off relationship between NOx and HC emissions under wide EGR rate range.

• 대한기계학회논문집B
• /
• 제23권8호
• /
• pp.1022-1030
• /
• 1999

A numerical study was carried out to analyze the effect of flow distribution of stirred part and plug flow part on combustion efficiency at the coal gasification process in an entrained bed coal reactor. The model of computation was based on gas phase eulerian balance equations of mass and momentum. The solid phase was described by lagrangian equations of motion. The $k-{\varepsilon}$ model was used to calculate the turbulence flow and eddy dissipation model was used to describe the gas phase reaction rate. The radiation was solved using a Monte-Carlo method. One-step parallel two reaction model was employed for the devolatilization process of a high volatile bituminous Kideco coal. The computations agreed well with the experiments, but the flame front was closer to the burner than the measured one. The flow distribution of a stirred part and a plug flow part in a reactor was a function of the magnitude of recirculation zone resulted from the swirl. The combustion efficiency was enhanced with decreasing stirred part and the maximum value was found around S=1.2, having the minimum stirred part. The combustion efficiency resulted from not only the flow distribution but also the particle residence time through the hot reaction zone of the stirred part, in particular for the weak swirl without IRZ(internal recirculation zone) and the long lifted flame.