• 제목/요약/키워드: K-epsilon turbulent model

검색결과 134건 처리시간 0.022초

난류선회제트 계산에 관한 난류모델 비교 연구 (Comparison of Various Turbulence Models for the Calculation of Turbulent Swirling Jets)

  • 최동규;최도형;김문언
    • 대한기계학회논문집
    • /
    • 제14권2호
    • /
    • pp.440-452
    • /
    • 1990
  • Comprehensive numberical computations have been made for four turbulent swirling jets with and without recirculation to critically evaluate the accuracy and universality of several exising turbulence models as well as of the modified k-.epsilon. model proposed in the present study. A numerical scheme based on the full Navier-Stoke equations ha been developed and used for this purpose. Inlet conditions are given by experiments, whenever possible, to minimize the error due to incorrect initial conditions. The standard k-.epsilon. model performs well for the strongly swirling jets with recirculation while it underpredicts the influence of swirl for weakly swirling jets. Rodi's swirl correction and algebraic stress model do not exhibit universality for the swirling jets. The present modified k-.epsilon. model derived from algebraic stress model accounts for anisotropy and streamline curvature effect on turbulence. This model performs consistently better than others for all cases. It may be because these flows have a strong dependence of stresses on the local strain of the mean flow. The predictions of truculence intensities indicate that this model successfully reflect the curvature effect in swirling jets, i.e. the stabilizing and destabilizing effects of swirl on turbulence transport.

정사각형 관내의 전개 중인 난류 유동 해석 (Calculation of Developing Turbulent Flow in a Square Duct)

  • 신승주;박승오;김의택
    • 대한기계학회논문집
    • /
    • 제13권1호
    • /
    • pp.170-177
    • /
    • 1989
  • 본 연구에서는 부분 포물형 Navier-Stokes 방정식에 Speziale이 제안한 비선형 k-.epsilon. 난류 모형을 적용하여 비직교 조표계에서 전개 중인 유동의 평균 속도와 난류 운동에너지 등을 예측하였다.

고난류강도 자유유동에서 평판 경계층 천이의 예측을 위한 난류 모형 개발 (Development of k-$\epsilon$ model for prediction of transition in flat plate under free stream with high intensity)

  • 백성구;임효재;정명균
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2000년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.337-344
    • /
    • 2000
  • A modified k-$\epsilon$ model is proposed for calculation of transitional boundary layer flows. In order to develop the eddy viscosity model for the problem, the flow is divided into three regions; namely, pre-transition region, transition region and fully turbulent region. The pre-transition eddy-viscosity is formulated by extending the mixing Length concept. In the transition region, the eddy-viscosity model employs two length scales, i.e., pre-transition length scale and turbulent length scale pertaining to the regions upstream and the downstream, respectively, and a university model of stream-wise intermittency variation is used as a function bridging the pre-transition region and the fully turbulent region. The proposed model is applied to calculate three benchmark cases of the transitional boundary layer flows with different free-stream turbulent intensity ( $1\%{\~}6\%$ ) under zero-pressure gradient. It was found that the profiles of mom velocity and turbulent intensity, local maximum of velocity fluctuations, their locations as well as the stream-wise variation of integral properties such as skin friction, shape factor and maximum velocity fluctuations are very satisfactorily Predicted throughout the flow regions.

  • PDF

허브와 중앙스팬 사이의 회전익 후류 3차원 난류유동해석에 관한 연구 (A study on the three dimensional turbulent flow analysis of wake flow behind rotating blade row between hub and midspan)

  • 노수혁;조강래
    • 대한기계학회논문집B
    • /
    • 제21권7호
    • /
    • pp.911-918
    • /
    • 1997
  • The turbulent viscous wake flows behind a single airfoil, two-dimensional stationary blade row and three-dimensional rotating blade row were calculated, and the numerical results were compared with experimental ones. The numerical technique was based on the SIMPLE algorithm using three turbulent closure models, standard k-.epsilon. model(WFM), low Reynolds number k-.epsilon. model(LRN) and Reynolds stress model (RSM). In the case of a single airfoil, WFM, LRN and RSM presented fairly good velocity distributions in the wake compared with experimental data. In the case of the stationary blade row, LRN and RSM presented better results than WFM for wake velocity distribution, and especially LRN showed best results among these three turbulent models. In the case of the rotating blade row, WFM and LRN showed fairly good agreement with experimental data of the three-dimensional velocity component distributions in the range from hub to mid span region. LRN was also superior to WFM in accuracy of prediction for the wake velocity distribution as same with the cases of a airfoil and the stationary blade row.

직사각형 공동 내부 자연연대류 문제에 대한 k-epsilon-vv-f 난류모델의 평가 (Evaluation of the K-Epsilon-VV-F Turbulence Model for Natural Convection in a Rectangular Cavity)

  • 최석기;김성오;김의광;최훈기
    • 한국전산유체공학회지
    • /
    • 제7권4호
    • /
    • pp.8-18
    • /
    • 2002
  • The primary objective of the present study is evaluation of the k-ε-vv-f turbulence model for prediction of natural convection in a rectangular cavity. As a comparative study, the two-layer k-ε model is also considered. Both models, with and without algebraic heat flux model, are applied to the analysis of natural convection in a rectangular cavity. The performances of turbulence models are investigated through comparison with available experimental data. The predicted results of vertical velocity component, turbulent heat fluxes, turbulent shear stress, local Nusselt number and wall shear stress are compared with experimental data. It is shown that, among the turbulence models considered in the present study, the k-ε-vv-f model with an algebraic heat flux model predicts best the vertical mean velocity and velocity fluctuation, and the inclusion of algebraic heat flux model slightly improves the accuracy of results.

4각 안내덕트 루프형상에 의한 난류특성변화 수치해석 (A Numerical Study of the Turbulent Flow Characteristics in the Inlet Transition Square Duct Based on Roof Configuration)

  • 유근종;최훈기;최기림;신병주
    • 대한기계학회논문집B
    • /
    • 제33권7호
    • /
    • pp.541-551
    • /
    • 2009
  • Configuration of the inlet transition square duct (hereinafter referred to as "transition duct") for heat recovery steam generator (hereinafter referred to as "HRSG") in combined cycle power plant is limited by the construction type of HRSG and plant site condition. The main purpose of the present study is to analyze the effect of a variation in turbulent flow pattern by roof slop angle change of transition duct for horizontal HRSG, which is influencing heat flux in heat transfer structure to the finned tube bank. In this study, a computational fluid dynamics(CFD) is applied to predict turbulent flow pattern and comparisons are made to 1/12th scale cold model test data for verification. Re-normalization group theory (RNG) based k-$\epsilon$ turbulent model, which improves the accuracy for rapidly strained flow and swirling flow in comparison with standard k-$\epsilon$ model, is used for the results cited in this study. To reduce the amount of computer resources required for modeling the finned tube bank, a porous media model is used.

저레이놀즈수 $k-\epsilon$ 난류모델을 사용한 엇갈린 관군 주위에서의 유동 및 열전달에 관한 연구 (A Study on the Fluid Flow and Heat Transfer Around a Staggered Tube Bundles Using a Low-Reynolds $k-\epsilon$ Turbulence Model)

  • 김형수;최영기;유홍선
    • 대한기계학회논문집
    • /
    • 제19권1호
    • /
    • pp.212-218
    • /
    • 1995
  • Turbulent flow and heat transfer characteristics around staggered tube bundles were studied using a non-orthogonal boundary fitted coordinate system and the low Reynolds .kappa. - .epsilon. turbulence model suggested by Lam and Bremhorst. The predicted flow characteristics for two tube pitches and tube arrangement showed good agreement with the experimental data except the strongly curved region. The predicted Nusselt number was compared with measurements obtained in the staggered rough bundles and it revealed the similar trend to measurements, but the location of the maximum and minimum heat transfer differed somewhat from the measurements.

차폐막이 있는 밀폐공간 내에서의 난류 자연대류 - 복사열전달에 관한 연구 (A Study on the Turbulent Natural Convection - Radiative Heat Transfer In a Partitioned Enclosure)

  • 박경우;이주형;박희용
    • 대한기계학회논문집
    • /
    • 제18권10호
    • /
    • pp.2738-2750
    • /
    • 1994
  • The Effects of radiative heat transfer on turbulent flow in a partitioned enclosure is studied numerically. The enclosure is partially divided by a thin, poorly conducting vertical divider projecting from the ceiling of the enclosure. The low Reynolds number $k-{\epsilon}$ model is adopted to calculate the turbulent flow field. The solutions to the radiative transfer equations are obtained by the discrete ordinates method(DOM). This method is based on control volume method and is compatible with the SIMPLER algorithm used to solve the momentum and energy equations. The effects of optical thickness and Planck number on the flow, temperature fields and heat transfer rates are investigated for a moderate Rayleigh number($=10^9$). The changes in buoyant flow fields and temperature distributions due to the variation of baffle length are also analyzed. From the predictions, radiant heat exchange between the baffle and the sidewalls strongly influences the temperature distribution in the baffle and its vicinity and total heat transfer increases as the optical thickness and the baffle length decrease. It is possible to neglect the radiative heat transfer effect when Planck number is over one.

평면 난류 오프셋 제트에 관한 연구 (A Study on the Plane Turbulent Offset Jet)

  • 유정열;강신형;채승기;좌성훈
    • 대한기계학회논문집
    • /
    • 제10권3호
    • /
    • pp.357-366
    • /
    • 1986
  • 본 연구에서는 3공피토우관 및 열선유속계를 사용하여 벽에 평행한 2차원 난류제트의 난류량들을 측정하였고, 스캐니 밸브를 이용하여 벽면아력분포를 측정함 으로써 재순환 영역을 포함한 전체유동장에서의 유동특성을 고찰하였다. 또한 잘 알려진 표준 k-.epsilon. 난류모형 및 유선곡률을 고려한 수정된 k-.epsilon. 난류모형을 이용하여 측정 수치해석을 수행하였다.

경사충돌분류에 관한 연구 (A study on an oblique impinging jet)

  • 조용철;김광용;박상규
    • 대한기계학회논문집
    • /
    • 제14권3호
    • /
    • pp.716-724
    • /
    • 1990
  • 본 연구에서는 2차원 경사충돌분류에 대한 실험을 수행하였고, 이 결과를 수] 치해석에 의한 계산치와 비교하였다. 실험에서는 난류특성을 구명하기 위하여 열선 풍속계를 사용해 충돌각의 변화에 따른 평균속도, 각 난류응력성분, 압력등을 측정하 였다.수치해석을 위한 난류모델로는 표준 K-.epsilon.모델을 사용하였다.