• 제목/요약/키워드: RNG $k-{\varepsilon}$ model

검색결과 83건 처리시간 0.021초

원형관 및 납작관-평판휜 형상의 밀집형 열교환기에 대한 대류열전달 상관관계식 (Convective Heat Transfer Correlations for the Compact Heat Exchanger with Circular Tubes and Flat Tubes-Plate Fins)

  • 모정하
    • 대한기계학회논문집B
    • /
    • 제34권3호
    • /
    • pp.291-299
    • /
    • 2010
  • 본 연구에서는 열의 수가 세 개인 원형관 및 종횡비가 고려된 납작관-평판휜 형상의 밀집형 열교환기 내 공기의 유동 및 열전달 특성을 RNG $k-{\varepsilon}$ 난류모델을 적용하여 수치적으로 해석하였다. 수치조건의 범위는 원형관인 경우 1,000<$Re_D_h$<10,000이며, 납작관인 경우 1,000<$Re_{D_h}$<10,000 및 3.06$f\;=\;CRe^m_{D_h}$의 형태로, Colburn j 계수는 $j\;=\;CRe^m_{D_h}$ 형태로 상관관계식을 제시하였다. 이러한 상관관계식은 향후 원형관 및 납작관-평판휜 형상의 열교환기 설계시에 기본적인 자료로 충분히 활용될 수 있을 것으로 판단된다.

가스터빈 연소기내의 고온공기 분무연소 해석 (Spray combustion with high temperature air in a Gas Turbine Combustor)

  • 조상필;김호영;박심수
    • 한국연소학회:학술대회논문집
    • /
    • 한국연소학회 2004년도 제28회 KOSCO SYMPOSIUM 논문집
    • /
    • pp.192-198
    • /
    • 2004
  • A numerical study was conducted to determine the effects of high temperature air, including equivalent ratio on flow field, temperature, evaporation, and overall temperature distribution in gas turbine combustor. A sector model of a typical wall jet can combustor, featuring introduction of primary air and dilution air via wall jet, was used in calculations. Flow field and temperature distribution were analyzed. Operating conditions such as inlet temperature and overall equivalent ratio were varied from 373 to 1300 K, and from 0.3 to 0.6, respectively, while any other operating conditions were fixed. The RNG ${\kappa}-{\varepsilon}$ model and eddy breakup model were used for turbulence and combustion model respectively. It was found that the increase with the inlet air temperature, velocity in the combustor is accelerated and evaporation of liquid fuel is not affected in primary zone, high temperature inlet air enhances the evaporation and improves overall temperature distribution factor.

  • PDF

고-기상 독성오염물질 단기 대기확산에 관한 수치해석적 연구 : 화학종, 온도, 상대속도 (A Numerical Study on the Short-term Dispersion of Toxic Gaseous and Solid Pollutant in an Open Atmosphere : Chemical Species, Temperature, Relative Velocity)

  • 나혜령;이은주;장동순;서영태
    • 한국안전학회지
    • /
    • 제10권3호
    • /
    • pp.68-80
    • /
    • 1995
  • A series of parametric calculations have been performed in order to investigate the short-term and short-range plume and puff behavior of toxic gaseous and solid pollutant dispersion in an open atmosphere. The simulation is made by the use of the computer program developed by this laboratory, in which a control-volume based finite-difference method is used together with the SIMPLEC algorithm for the resolution of the pressure-velocity coupling appeared In Wavier-Stokes equation. The Reynolds stresses are solved by the standard two-equation k-$\varepsilon$ model modified for buoyancy together with the RNG(Renormalization Group) k-$\varepsilon$ model. The major parameters considered in this calculation are pollutant gas density and temperature, the relative velocity of pollutants to that of the surrounding atmospheric air, and particulate size and density together with the height released. The flow field is typically characterized by the formation of a strong recirculation region for the case of the low density gases such as $CH_4$ and air due to the strong buoyancy, while the flow is simply declining pattern toward the downstream ground for the case of heavy molecule like the $CH_2C1_2$and $CCl_4$, even for the high temperature, $200^{\circ}C$. The effect of gas temperature and velocity on the flow field together with the particle trajectory are presented and discussed in detail. In general, the results are physically acceptable and consistent.

  • PDF

Numerical Simulation on the Performance of Axial Vane Type Gas-Liquid Separator with Different Guide Vane Structure

  • Yang, Fan;Liu, Ailan;Guo, Xueyan
    • International Journal of Fluid Machinery and Systems
    • /
    • 제10권1호
    • /
    • pp.86-98
    • /
    • 2017
  • In order to obtain high efficiency and low resistance droplet separation apparatus, axial vane type gas-liquid separators with different guide vanes were designed, and the RNG $k-{\varepsilon}$ model as well as discrete phase model (DPM) were used to investigate the flow pattern inside the separators. It was shown that the tangential velocity distribution under different guide vanes have Rankine vortex characteristics, pressure distribution exhibits a high similarity which value becomes big as the increase of the blade outlet angle and the decrease of the guide vane numbers. The increase of the guide vane numbers and the decrease of the blade outlet angle could make separation improve significantly. The separation efficiency is almost 100% when the droplet diameter is bigger than $40{\mu}m$.

Reliability of numerical computation of pedestrian-level wind environment around a row of tall buildings

  • Lam, K.M.;To, A.P.
    • Wind and Structures
    • /
    • 제9권6호
    • /
    • pp.473-492
    • /
    • 2006
  • This paper presents numerical results of pedestrian-level wind environment around the base of a row of tall buildings by CFD. Four configurations of building arrangement are computed including a single square tall building. Computed results of pedestrian-level wind flow patterns and wind speeds are compared to previous wind tunnel measurement data to enable an assessment of CFD predictions. The CFD model uses the finite-volume method with RNG $k-{\varepsilon}$ model for turbulence closure. It is found that the numerical results can reproduce key features of pedestrian-level wind environment such as corner streams around corners of upwind building, sheltered zones behind buildings and channeled high-speed flow through a building gap. However, there are some differences between CFD results and wind tunnel data in the wind speed distribution and locations of highest wind speeds inside the corner streams. In locations of high ground-level wind speeds, CFD values match wind tunnel data within ${\pm}10%$.

Numerical Study on Flow Characteristics at Blade Passage and Tip Clearance in a Linear Cascade of High Performance Turbine Blade

  • Myong, Hyon-Kook;Yang, Seung-Yong
    • Journal of Mechanical Science and Technology
    • /
    • 제17권4호
    • /
    • pp.606-616
    • /
    • 2003
  • A numerical analysis has been conducted in order to simulate the characteristics of complex flow through linear cascades of high performance turbine blade with/without tip clearance by using a pressure-correction based, generalized 3D incompressible Wavier-Stokes CFD code. The development and generation of horseshoe vortex, passage vortex, leakage vortex, tip vortex within tip clearance, etc. are clearly identified through the present simulation which uses the RNG k-$\varepsilon$ turbulent model with wall function method and a second-order linear upwind scheme for convective terms. The present simulation results are consistent with the generally known tendency that occurs in the blade passage and tip clearance. A 3D model for secondary and leakage flows through turbine cascades with/without tip clearance is also suggested from the present simulation results, including the effects of tip clearance height.

선형터빈 익렬의 익단간극유동에 대한 수치해석적 연구 (Numerical simulation of tip clearance flows through linear turbine cascades)

  • 이훈구;유정열
    • 대한기계학회논문집B
    • /
    • 제21권6호
    • /
    • pp.813-821
    • /
    • 1997
  • Three-dimensional turbulent incompressible flow through the tip clearance of a linear turbine rotor cascade with high turning angle has been analyzed numerically. As a preliminary study to predict the tip clearance loss realistically, a generalized k-.epsilon. model derived by RNG (renormalized group) method is used for the modeling of Reynolds stresses to account for the strain rate of turbulent flow. The effects of the tip clearance flow on the passage vortex, the total pressure loss are considered qualitatively. The existences of vena contract and tip clearance vortex have been confirmed and it has been shown that as the size of the tip clearance increases, the accumulated flow through the tip clearance and the total pressure loss downstream of the cascade increase.

도시하천의 교각 및 횡단 월류형 구조물에 의한 수리영향 분석 (Analysis of Hydraulic effects on Piers and Transverse Overflow Type Structures in Urban Stream)

  • 윤선권;전시영;김종석;문영일
    • 한국수자원학회논문집
    • /
    • 제41권2호
    • /
    • pp.197-212
    • /
    • 2008
  • 최근 하천의 흐름해석 분야에서는 수위 및 하상변동 양상과 오염된 지류유입으로 인한 본류에서의 유속분포 양상 및 혼합과정 등의 실제적인 문제를 해결할 수 있는 1, 2차원적 해석이 이루어지고 있으며, 이는 복잡한 하천을 균일화된 모양과 단순화된 방정식으로 일괄 적용함으로써 많은 한계점을 나타내고 있다. 본 연구에서는 서울시 관내 지방 2급 하천인 우이천 시험유역을 대상으로 하천의 물리적인 특성 변화에 따른 흐름해석을 수행하기 위하여 3차원 RANS (Reynolds Averaged Navier-Stokes Equation)를 지배방정식으로 하는 CFD (Computational Fluid Dynamics)모형인 FLOW-3D를 이용하였고, ${\kappa}-{\varepsilon}$, RNG (Renormalized Group) ${\kappa}-{\varepsilon}$, LES (Large Eddy Simulation) 등의 난류모형을 적용하여 각각의 수치모의 결과를 비교 분석 하였다. 또한, 수치 해석을 통한 교량 설치부와 하류 횡단월류형 구조물에서의 난류영향 및 유속분포, 수위 압력분포, 와류특성 등을 분석하였고, 구조물의 철거에 의한 영향을 비교하여 분석하였다. 이는 향후 도시하천의 기능을 상실한 횡단 구조물 철거에 의한 장기적인 하상변동과 토사의 퇴적, 세굴 및 수질악화 등의 영향을 파악해 볼 수 있는 기초자료로 활용될 수 있으리라 사료된다.

분류층 연소기내의 유동해석 (Flow Analysis in a Entrained Flow Combustor)

  • 양희천;김중현
    • 한국마린엔지니어링학회:학술대회논문집
    • /
    • 한국마린엔지니어링학회 2000년도 추계학술대회 논문집(Proceeding of the KOSME 2000 Autumn Annual Meeting)
    • /
    • pp.30-36
    • /
    • 2000
  • A numerical study was conducted to investigate the effects of flow parameters in a entrained flow combustor on the flow characteristics. The computational model was based on the gas phase Eulerian equations of mass, momentum and energy. The code was formulated with RNG k-$\varepsilon$ model for turbulent flow. The calculation parameters were the magnitude of primary and secondary jet velocity and the height difference between primary and secondary jet. As the secondary jet velocity increased, the upper recirculation zone of the primary jet was strengthened. It was found that as the primary jet velocity increased, there was a critical jet velocity at which the size of upper and lower recirculation zone was changed.

  • PDF

대형버스 바디모델의 후류특성 및 후미 스포일러 효과에 관한 해석적 고찰 (A Numerical Investigation on the Wake Flow Characteristics and Rear-Spoiler Effect of a Large-Sized Bus Body)

  • 김민호;국종영;천인범
    • 한국자동차공학회논문집
    • /
    • 제11권2호
    • /
    • pp.126-133
    • /
    • 2003
  • The aerodynamic characteristics of automobiles have received substantial interest recently. Detailed knowledge of the vehicle aerodynamics is essential to improve fuel efficiency and enhance stability at high-speed cruising. In this study, a numerical simulation has been carried out for three-dimensional turbulent flows around a commercial bus body. Also, the effect of rear-spoiler attached at rear end of bus body was investigated. The Wavier-Stokes equation is solved with SIMPLE method in general curvilinear coordinates system. RNG $k-\varepsilon$ turbulence model with the MARS scheme was used for the evaluating aerodynamic forces, velocity and pressure distribution. The results showed details of the three-dimensional wake flow in the immediate rear of bus body and the effect of rear-spoiler on the wake structure. A maximum of 14% reduction in drag coefficient was achieved for a model with a rear-spoiler.