• Title/Summary/Keyword: Turbulent Flows

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정체 유동장에 떠있는 난류 예혼합 화염의 일차 모멘트 닫힘 모사 (First Moment Closure Simulation of Floating Turbulent Premixed Flames in Stagnation Flows)

  • 이은주;허강열
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2000년도 제20회 KOSCO SYMPOSIUM 논문집
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    • pp.122-132
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    • 2000
  • Computational fluid dynamic simulation is performed for the floating turbulent premixed flames stabilized in stagnation flows of Cho et al. [1] and Cheng and Shepherd [2]. They are both in the wrinkled flamelet regime far from the extinction limit with $u'/S^{0}_{L}$ less than unity. The turbulent flux is given in the first moment closure as a sum of the classical gradient flux due to turbulent motions and the countergradient flux due to thermal expansion. The parameter $N_{B}'s$ are greater than unity with the countergradient flux dominant over the gradient flux. The countergradient flux is assumed to be zero in $\bar{c}<0.05$. The flame surface density is modeled as a symmetric parabolic function with respect to $\bar{c}$. The product of the maximum flame surface density and the mean stretch factor is considered as a tuning constant to match the flame location. Good agreement is achieved with the measured $\tilde{w}$ and $\bar{c}$ profiles along the axis in both flames.

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난류에 의해 야기되는 이차유동 예측성능에 대한 비선형 κ-ε 난류모델의 평가 (Evaluation of Nonlinear κ-ε Models on Prediction Performance of Turbulence-Driven Secondary Flows)

  • 명현국
    • 대한기계학회논문집B
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    • 제27권8호
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    • pp.1150-1157
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    • 2003
  • Nonlinear relationship between Reynolds stresses and the rate of strain of nonlinear k-$\varepsilon$models is evaluated theoretically by using the boundary layer assumptions against the turbulence-driven secondary flows in noncircular ducts and then their prediction performance is validated numerically through the application to the fully developed turbulent flow in a square duct. Typical predicted quantities such as mean axial and secondary velocities, turbulent kinetic energy and Reynolds stresses are compared with available experimental data. The nonlinear k-$\varepsilon$ model adopted in a commercial code is found to be unable to predict accurately duct flows with the prediction level of secondary flows one order less than that of the experiment.

난류선회 등온 및 분무연소 유동에 대한 수치해석 (Numerical Study of Turbulent Swirling Isothermal and Spray-Combusting Flows)

  • 김성구;안국영;김용모;이창식
    • 한국자동차공학회논문집
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    • 제4권5호
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    • pp.130-141
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    • 1996
  • Numerical study of a confined, swirling, isothermal and spray-combusting flows has been presented. The pressure-velocity coupling in the Eulerian gas-phase equation is handled by the improved PISO algorithm. The droplet dispersion by turbulence is introduced by a Stochastic Separated Flow(SSF) model. The k-$\varepsilon$ turbulence model and the eddy dissipation model are employed to account for turbulence-combustion interaction. The detailed comparison with experimental data has been made for the isothermal jet swirling flows and the nearly monodisperse spray-combusting flow in the swirl combustor.

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EXPERIMENTAL STUDY OF TURBULENCE MANIPULATION IN STEPPED SPILLWAYS. IMPLICATIONS ON FLOW RESISTANCE IN SKIMMING FLOWS

  • GONZALEZ CARLOS A.;CHANSON HUBERT
    • 한국수자원학회:학술대회논문집
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    • 한국수자원학회 2005년도 학술발표회(1)
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    • pp.588-589
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    • 2005
  • Current expertise in air-water turbulent flows on stepped chutes is limited to laboratory experiments at low to moderate Reynolds numbers on flat horizontal steps. In this study, highly turbulent air-water flows skimming down a large-size stepped chute were systematically investigated with a $22^{\circ}$ slope (Fig. 1). Turbulence manipulation was conducted using vanes or longitudinal ribs to enhance interactions between skimming flows and cavity recirculating regions (Fig. 2). Systematic experiments were performed with seven configurations. The results demonstrated the strong influence of vanes on the air-water flow. An increase in flow resistance was observed consistently with maximum flow resistance achieved with vanes placed in a zigzag pattern.

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정상상태의 이차원 슬롯 충돌제트에 관한 수치 해석 (Numerical Simulation of Two-Dimensional Impinging Slot Jet)

  • 박태현;최형권;유정열
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 추계학술대회논문집B
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    • pp.603-608
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    • 2000
  • The characteristics of laminar and turbulent slot impinging jet flows are examined using segregated FEM with SUPG. Turbulent flows are modeled using $Wilcox^{(1)}$ $k-\;{\omega}$ turbulence model. The results are validated by comparing with velocity field of the existing experimental data. The distance of the target plate from the nozzle varies between 2, 4 and 5 times the slot jet width. Present study shows that the $k-\;{\omega}$ model gives results which agree well with the existing experimental data. In turbulence flows, the velocity profile of present calculation is more accurate than the existing numerical calculations. In laminar flows, We found tertiary vortex which was not found in the previous numerical study by M. $chen^{(6)}$ et al due to the numerical difference.

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Effect of taper on fundamental aeroelastic behaviors of super-tall buildings

  • Kim, Yong Chul;Tamura, Yukio;Yoon, Sung-Won
    • Wind and Structures
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    • 제20권4호
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    • pp.527-548
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    • 2015
  • Aeroelastic wind tunnel experiments were conducted for conventional and tapered super-tall building models to investigate the effect of taper on fundamental aeroelastic behaviors in various incident flows. Three incident flows were simulated: a turbulent boundary-layer flow representing urban area; a low-turbulent flow; and a grid-generated flow. Results were summarized focusing on the effect of taper and the effect of incident flows. The suppression of responses by introducing taper was profound in the low-turbulence flow and boundary-layer flow, but in the grid-generated flow, the response becomes larger than that of the square model when the wind is applied normal to the surface. The effects of taper and incident flows were clearly shown on the normalized responses, power spectra, stability diagrams and probability functions.

Visualization of Unsteady Fluid Flows by Using Large Eddy Simulation

  • Kobayashi, Toshio;Taniguchi, Nobuyuki
    • Journal of Mechanical Science and Technology
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    • 제15권12호
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    • pp.1750-1756
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    • 2001
  • Three-dimensional and unsteady flow analysis is a practical target of high performance computation. As recently advances of computers, a numerical prediction by the large eddy simulation (LES) are introduced and evaluated for various engineering problems. Its advanced methods for the complex turbulent flows are discussed by several examples applied for aerodynamic designs, analysis of fluid flow mechanisms and their interaction to complex phenomena. These results of time-dependent and three-dimensional phenomena are visualized by interactive graphics and animations.

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난류 모형에 따른 수직 평판 위 파동 액막류의 수치해석 연구 (Numerical Study of Wavy Film Flow on Vertical Plate Using Different Turbulent Models)

  • 민준기;박일석
    • 대한기계학회논문집B
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    • 제38권5호
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    • pp.373-380
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    • 2014
  • 액막류는 다양한 산업분야에 적용되는 쉘-튜브 열교환기의 주요 열교환기구로 오랫동안 연구되어왔다. 액막류의 한쪽 경계는 고정벽에 접하고 있지만 반대편에서는 기체 영역과 경계를 형성하므로 액막 레이놀즈 수가 증가함에 따라 쉽게 불안정해지는 특징을 가지고 있다. 따라서 레이놀즈 수가 증가함에 따라 자유표면 파동 현상이 나타나는데, 층류 영역에서는 큰 진폭의 고립파가, 난류 천이 이후에는 낮은 진폭의 물결파가 나타난다. 액막류의 열전달 성능은 액막의 두께에 의해 크게 지배받는데 액막류에 동반된 파동은 액막 두께의 시공간적 변화를 의미하는 것이므로 이에 대한 정보를 해석적으로 수집하는 것은 액막류 열전달 성능을 예측하는데 필수적이다. 본 연구에서는 낮은 진폭의 물결파를 동반한 난류 액막류에 대하여 여러 가지 난류 모형을 적용한 해석결과들을 실험결과와 비교함으로써 난류 모형들에 대한 평가를 실시하였다.

Large Eddy Simulation of Turbulent Combustion Flow Based on 2-scaler flamelet approach

  • Oshima, Nobuyuki;Tominaga, Takuji
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2006년도 추계 학술대회논문집
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    • pp.18-21
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    • 2006
  • This paper investigates LES of turbulent combustion flow based on 2-scalar flamelet approach, where a G-equation and a conserved scalar equation simulate a propagation of premixed flame and a diffusion combustion process, respectively. The turbulent SGS modeling on these flamelet combustion approach is also researched. These LES models are applied to an industrial flows in a full scale gasturbine combustor with premixed and non-premixed flames. The numerical results predict the characteristics of experiment temperature profiles. Unsteady features of complex flames in combustor are also visualized.

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