• 제목/요약/키워드: reacting flow

검색결과 190건 처리시간 0.021초

DES를 이용한 초음속 유동내 수직 연료분사 유동의 비정상 3차원 해석 Part II : 반응 유동장 (Unsteady Three-Dimensional Analysis of Transverse Fuel Injection into a Supersonic Crossflow using Detached Eddy Simulation Part II : Reacting Flowfield)

  • 원수희;정인석;최정열
    • 한국항공우주학회지
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    • 제37권9호
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    • pp.879-888
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    • 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.

배출물 저감을 위한 촉매변환기 내의 3차원 유동해석 (Three-Dimensional Flow Analysis of Catalytic Converter for Reducing Emission)

  • 정수진;김우승
    • 한국자동차공학회논문집
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    • 제6권5호
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    • pp.55-65
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    • 1998
  • A numerical and experimental study of three-dimensional steady incompressible non-reacting flow inside various dual-monolith catalytic converters has been conducted for achievement of performance improvement, reduction of light-off time and longer service life by improving the flow uniformity within the monolith. In this study, the effects of curvature of inlet exhaust pipe and monolith brick length on the flow uniformity and pressure drop within monolith were numerically investigated. The computations are confirmed by measurements of steady flow. The agreement between computations and experiment was relatively good. The result of this study shows that curvature of inlet exhaust pipe and monolith brick length gave a great effect on the flow uniformity and the shorter the brick length, the lower flow uniformity and the less pressure drop.

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Effects of Synthesis Method, Melamine Content and GPC Parameter on the Molecular Weight of Melamine-Urea-Formaldehyde Resins

  • KIM, Minjeong;PARK, Byung-Dae
    • Journal of the Korean Wood Science and Technology
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    • 제49권1호
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    • pp.1-13
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    • 2021
  • This study was conducted to investigate the effects of the synthesis method, melamine content, and GPC parameters (such as flow rate, column-detector temperature, and sample injection temperature) on the molecular weight of melamine-urea-formaldehyde (MUF) resins. Two different synthesis methods were employed. In the first method, MUF-A resins were synthesized by simultaneously reacting urea, formaldehyde, and melamine (5%, 10%, and 20%) using the reaction of alkaline-acid-alkaline steps under controlled temperature and viscosity. In the second method, MUF-B resins were synthesized by first reacting melamine at the same levels with formaldehyde and then by adding urea. The highest weight average molecular weight (Mw) of MUF-A resins was found at 10% melamine content when the flow rate was 0.3 and 0.8 ml/min; Mw decreased slightly at 20% melamine content. The results showed that Mw increased with an increase in the melamine content when the flow rate was 0.5 and 1.0 ml/min. In addition, Mw was the highest when the flow rate, column-detector temperature, and injection temperature were 0.3 ml/min, 50℃, and 25℃, respectively. On the contrary, MUF-B resins had greater Mw and number average molecular weight (Mn) than MUF-A resins. Overall, Mw and Mn increased as the melamine content increased. The optimal GPC parameter for MUF resins was determined as follows: a flow rate of 0.5 ml/min, a column-detector temperature of 50℃, and a sample injection temperature of 50℃.

전기화학반응을 수반한 유로채널 형상에 따른 마찰계수에 대한 연구 (Friction Factor in Micro Channel Flow with Electrochemical Reactions in Fuel Cell)

  • 조선아;이필형;한상석;최성훈;황상순
    • 전기화학회지
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    • 제10권4호
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    • pp.245-251
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    • 2007
  • 주어진 연료전지면적에서 반응면적이 넓을수록 성능이 향상되는 연료전지는 좁은 폭의 채널을 여러 개 존재하게 하는 구조를 선호하지만 채널 폭이 좁아질수록 압력이 커지는 문제가 고려되어져야 한다. 그러나 현재 채널 구조에 따른 압력에 대한 연구는 많이 진행되어져 왔지만 대부분 반응을 고려하지 않았으며, 반응을 고려한 경우에 어떤 경향을 나타내는지 알아보는 것이 연료전지 유로설계에 있어 매우 중요하다. 본 논문에서 화학반응을 고려한 평행류, 90도 밴드형, serpentine 세가지 종류의 유로채널를 가진 연료전지를 수치 해석하여 반응을 고려하지 않은 경우와 마찰계수(fRe), 속도, 압력강하를 비교하여 본 결과 parallel과 bend 형태의 채널은 반응을 고려한 경우 반응에 의한 밀도의 감소에 따라 근소하게 감소한 것을 알 수 있었다. 그러나 serpentine채널은 다공성매체인 확산층을 통해 인접한 채널로 가스가 이동하는 bypass flow 영향에 의하여 상대적으로 낮은 압력강하를 나타내는 것을 알 수 있었다.

스크램제트 연소기 내의 난류 연소 유동 해석 (Numerical Analysis of Turbulent Combustion Flow in Scramjet Combustors)

  • 최정열;원수희;정인석
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2005년도 제31회 KOSCO SYMPOSIUM 논문집
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    • pp.261-267
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    • 2005
  • A comprehensive DES quality numerical analysis has been carried out for reacting flows in constant-area and divergent scramjet combustor configuration with and without a cavity. Transverse injection of hydrogen is considered over a broad range of injection pressure. The corresponding equivalence ratio of the overall fuel-air mixture ranges from 0.167 to 0.50. The work features detailed resolution of the flow and flame dynamics in the combustor, which was not typically available in most of the pervious studies. Much of the flow unsteadiness is related not only 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 roles of the cavity, injection pressure, and heat release in determining the flow dynamics are examined systematically.

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LNG 연료를 이용한 가스 터빈 연소기의 연소유동 해석 (Analysis of Combustion Flow of LNG-Fueled Gas Turbine Swirl Burner)

  • 김태호;강기하;최정열;김성철
    • 한국연소학회지
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    • 제13권3호
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    • pp.33-40
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    • 2008
  • Two- and Three- dimensional numerical simulations are carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation using imported and domestic natural gases. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the numerical results with the flow conditions selected from the gas turbine operation data. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well. The flow structures of the recirculation and combustion region was understood from the comparison of the two- and three-dimensional results. The complexity of the three-dimensional swirl flows inside the gas turbine combustor with multiple swirlers was understood those resulting from the interactions of the stage and pilot burners.

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스크램제트 연소기의 비정상 연소현상 (Unsteady Combustion Phenomena in Scramjet Combustor)

  • 최정열
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2005년도 제24회 춘계학술대회논문집
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    • pp.364-367
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    • 2005
  • 공동이 있거나 없는 일정 단면적 및 확장형 스크램제트 연소기 내에 수소 연료가 $0.5\sim1.5\;MPa$ 로 수직 분사되는 것을 고려하여 연소 및 동결 유동에 대한 일련의 수치해석을 수행 하였다. 내재된 물리 과정을 규명하기에 충분한 정확도로 진동하는 유동 및 화염의 동적 특성을 포착하였으며, 이로부터 연소기의 형상과, 공동 및 발열량의 영향을 이해할 수 있었다.

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A COMPUTATIONAL ANALYSIS OF FINITE RATE CHEMICALLY REACTING FLOW BY USING UPWIND N-S METHOD

  • Seo J. I.;Kwon C. O.;Song D. J.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2000년도 춘계 학술대회논문집
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    • pp.166-171
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    • 2000
  • A two-dimensional/axisymmetric CSCM upwind flux difference splitting Wavier-Stokes method has been developed to study the finite rate chemically react-ing invisicd and viscous hypersonic flows over blunt-body. A upwind method was chosen due to its robustness in capturing the strong bow shock waves. For the nonequilibrium chemically reacting air, NS-I species conservation equations were strongly coupled with flowfield equations through convection and species production terms. The nonequilibrium wall pressure and heat transfer rate distributions along the vehicle were compared with those from equilibrium and perfect gas calculations. The nonequilibrium species distribution shows the reduced concentrations of O and N species when compared with equilibrium species distribution. The solutions resolved strong bow shock waves md heat transfer rate very accurately when compared with central difference schemes.

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Numerical Modeling for Combustion and Soot Formation Processes in Turbulent Diffusion Flames

  • Kim, Hoo-Joong;Kim, Yong-Mo
    • Journal of Mechanical Science and Technology
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    • 제16권1호
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    • pp.116-124
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    • 2002
  • In order to investigate the soot formation and oxidation processes, we employed the two variable approach and its source terms representing soot nucleation, coagulation, surface growth and oxidation. For the simulation of the taxi-symmetric turbulent reacting flows, the pressure-velocity coupling is handled by the pressure based finite volume method. We also employed laminar flamelet model to calculate the thermo-chemical properties and the proper soot source terms from the information of detailed chemical kinetic model. The numerical and physical models used in this study successfully predict the essential features of the combustion processes and soot formation characteristics in the reacting flow field.

${\gamma}-Alumina$에 담지된 산화구리에 의한 $SO_x$가스의 제거 특성 (Removal Characterics of $SO_x$ by CuO Impregnated ${\gamma}-Alumina$)

  • 이창선;윤용수
    • 환경위생공학
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    • 제11권3호
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    • pp.29-35
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    • 1996
  • Numerical solutions were obtained to the model equations for various parameters characterizing the pore structure, effective internal diffusion and the chemical reaction constant. The conversion was decreased with the cause of pore closure at the surface of reacting particles, reduction of porosity, surface area of reaction and effective diffusion coefficient in the solid with the progress of reaction. Total conversion was strongly depend on the local conversion at surface. According to the decreasing of impregnated concentration of the copper oxide and the increase of the flue gases concentration, total conversion was increased. And the conversion were affected by gas flow rate and pore size distribution of the reacting solid.

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