• 제목/요약/키워드: Turbulent Energy

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Measurement of Turbulent Intensity Distributions of a Cylinder Wake

  • Doh, Deog Hee;Cho, Gyeong Rae;Moon, Kyeong Rok;Cho, Yong Beom
    • 한국가시화정보학회지
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    • 제11권1호
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    • pp.41-47
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    • 2013
  • Turbulence properties of a cylinder wake (d=10 mm) have been investigated with a new volume PTV algorithm. The measurement system consists of two-high-cameras(1 $k{\times}1$ k), a Nd-Yag laser and a host computer. A fitness function representing three-dimensional coherency has been adopted to sort out spurious vectors. A hybrid fitness function representing the relations between the fitness and the three-dimensional shortest distances constructed by the two collinears of the two cameras has been also adopted. The constructed algorithm has been employed for the measurements of the cylinder wakes. The Reynolds numbers tested in this paper are 360, 540, 720, 900, 1080 and 1260. More than 10,000 instantaneous 3D vectors have been obtained by the constructed system. The volumetric distributions of the turbulence intensities (for u', v', w') indicate that clearly different patterns for all Reynolds numbers and imply that a regular pattern (like a similarity rule) for the turbulent properties exists.

두 평판 사이의 난류 열대류의 수치해석 (Numerical analysis of turbulent thermal convection between two flat plates)

  • 이장희;윤효철;정명균
    • 대한기계학회논문집
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    • 제12권1호
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    • pp.137-151
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    • 1988
  • 본 논문에서는 아래 평판은 높은 온도 $T_{h}$로 유지되고, 위의 평판은 낮은 온도 $T_{i}$로 유지되어 있을 때 온도차에 의하여 발생하는 난류 열대류 문제를 난류모델 방정식을 사용하여 수치적으로 해석하고자 한다.다.다.

이산 웨이블릿 변환을 이용한 3차원 난류 채널 유동에 관한 연구 (A Study of 3-Dimensional Turbulent Channel Flow Using Discrete Wavelet Transform)

  • 김강식;이상환
    • 대한기계학회논문집B
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    • 제29권3호
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    • pp.314-321
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    • 2005
  • Discrete Wavelet Transform (DWT) has been applied to the Direct Numerical Simulation (DNS) data of turbulent channel flow. DWT splits the turbulent flow into two orthogonal parts, one corresponding to coherent structures and the other to incoherent background flow. The coherent structure is extracted from not vorticity field but velocity's since the channel flow is not isoropic. By comparing DWT's result of channel flow with that of isotropic flow, it is shown that coherent structure maintains the properties of original channel flow. The velocity field of coherent structures can be represented by few wavelet modes and that these modes are sufficient to reproduce the velocity probability density function (PDF) and the energy spectrum over the entire inertial range. The remaining incoherent background flow is homogeneous, has small amplitude, and is uncorrelated. These results are compared with those obtained for the same compression rate using large eddy simulation (LES) filtering. In contrast to the incoherent background flow of DWT, the LES subgrid scales have a much larger amplitude and are correlated, which makes their statistical modeling more difficult.

이산 웨이블릿 변환을 이용한 3차원 난류 채널 유동에 관한 연구 (A Study of 3-Dimensional Turbulent Channel Flow using Discrete Wavelet Transform)

  • 김강식;이상환
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1813-1818
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    • 2004
  • Discrete Wavelet Transform (DWT) has been applied to the Direct Numerical Simulation (DNS) data of turbulent channel flow. DWT splits the turbulent flow into two orthogonal parts, one corresponding to coherent structures and the other to incoherent background flow. The coherent structure is extracted from not vorticity field but velocity's since the channel flow is not isotropic. By comparing DWT's result of channel flow with that of isotropic flow, it is shown that coherent structure maintains the properties of original channel flow. The velocity field of coherent structures can be represented by few wavelet modes and that these modes are sufficient to reproduce the velocity probability distribution function (PDF) and the energy spectrum over the entire inertial range. The remaining incoherent background flow is homogeneous, has small amplitude, and is uncorrelated. These results are compared with those obtained for the same compression rate using large eddy simulation (LES) filtering. In contrast to the incoherent background flow of DWT, the LES subgrid scales have a much larger amplitude and are correlated, which makes their statistical modeling more difficult.

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가스발생기 비-반응 유동의 난류 혼합에 대한 LES 해석 (LES of Turbulent Mixing of Non-Reactive Flow in Gas Generator)

  • 이창진
    • 한국항공우주학회지
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    • 제36권12호
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    • pp.1171-1179
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    • 2008
  • 난류고리와 스플래쉬 판에 의한 난류 혼합과 난류 생성에 관한 연구를 위하여 LES 해석이 가능한 CFD 코드를 개발하였으며 이를 사용하여 LES 해석을 수행하였다. 계산 결과에 의하면 난류고리는 유동장에 매우 강한 난류를 생성하여 후류에서 난류 혼합을 촉진하는 역할을 담당하는 것으로 밝혀졌다. 한편 난류고리 후류 방향으로 스플래쉬 판을 설치하면 난류고리만을 설치한 경우와 매우 다른 형태의 난류 에너지와 엔스트로피 생성을 관찰할 수 있었다. 이 경우의 난류혼합은 판 뒤에 생성되는 매우 강하며 집중적인 난류의 생성에 의하여 이루어지며 압력강하는 초기 압력의 1% 수준으로 매우 낮았다. 또한 계산결과에 의하면 난류고리의 형상이나 돌출 길이 변화는 생성되는 난류의 특성에 매우 커다란 영향을 미치지 못하였다. 난류 혼합을 가장 효과적으로 이룰 수 있는 판의 위치에 관한 연구 는 진행하지 못하였으나 지금까지 계산결과에 의하면 스플래쉬 판이 설치되었을 때 압력 강하도 낮은 수준이며 난류 혼합이 가장 효과적임을 알 수 있었다.

A CLOSED-FORM SOLUTION FOR TURBULENT WAVE BOUNDARY LAYERS

  • Larson, Magnus
    • 한국해안해양공학회:학술대회논문집
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    • 한국해안해양공학회 1995년도 정기학술강연회 발표논문 초록집
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    • pp.66-70
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    • 1995
  • The oscillatory boundary layer that develops when surface waves propagate over the sea bottom affects many flow-pendent phenomena in the coastal zone. Examples of such phenomena are wave energy dissipation due to bottom friction and the initiation and transport of sediment (Grant and Madsen 1986). In nature the boundary layer under waves will almost always be turbulent (Nielsen 1992). (omitted)

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Structural Characteristics of Turbulent Diffusion Flame Combusted with Simulated Coal Syngas

  • Park, Byung-Chul;Kim, Hyung-Taek;Chun, Won-Gee
    • 에너지공학
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    • 제11권4호
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    • pp.350-358
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    • 2002
  • The present work determined the flame structure characteristics of coal syngas combusted inside swirl burners with various nozzle types. Fuel nozzle types are largely classified into two groups of axial and tangential. Experiments were carried out for investigating the effects of fuel nozzle geometry, fuel composition ratio, heating rate, excess air, and degree of swirl on the turbulent diffusion flame structure. To determine the characteristics of the flame structure, axial type fuel nozzle diameter of laboratory-scale combustor is varied to 1.23, 1.96, and 2.95 ㎜ and the direction of tangential type nozzles are varied to radial, clockwise, and counter-clockwise. The comparison of the experimental results was performed to understand functional parameters relating the flame structure. Data analysis showed that the vertical straight flame height generally decreased with increasing swirl number and decreasing axial type nozzle diameter. Flame height established with tangential type nozzle is 3 times shorter than that with vertical type. The flame structures among the 3 different tangential fuel nozzles relatively showed no particular difference. By increasing the heating rate, the width of flame increased generally in both vertical and tangential flame. Within the present experimental parameters of the investigation, flame structure is mainly depends on the nozzle type of the combustor. The visually investigated flame lengths are confirmed through the analysis of temperature profile of each flame.

엇갈린 다이아몬드형 핀휜의 형상에 따른 난류열전달 성능해석 (ANALYSIS OF TURBULENT HEAT TRANSFER FROM STAGGERED PIN-FIN ARRAYS WITH DIAMOND SHAPED ELEMENTS AT VARIOUS GEOMETRICAL CONFIGURATIONS)

  • 조안태;김광용
    • 한국전산유체공학회지
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    • 제13권2호
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    • pp.20-26
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    • 2008
  • A numerical study is carried out to analyze the steady three-dimensional turbulent flow and convective heat transfer in a staggered pin-fin array with diamond shaped elements at various geometrical configurations. Steady Reynolds-averaged Navier-Stokes equations and energy equation are solved using a finite volume based solver. Shear stress transport (SST) model is used as turbulence closure. The computational domain is composed of one pitch of pin-fin displacement with periodic boundary conditions on the surfaces normal to the streamwise direction and the cross-streamwise direction. The numerical results for Nusselt number and friction factor are validated with experimental results. The effects of pin angle, pin height and pitch on Nusselt number, friction factor and efficiency index are investigated.

Effect of Dynamic SGS Model in a Kerosene-LOx Swirl Injector under Supercritical Condition

  • Heo, Jun-Young;Hong, Ji-Seok;Sung, Hong-Gye
    • International Journal of Aeronautical and Space Sciences
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    • 제16권2호
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    • pp.254-263
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    • 2015
  • In this study, numerical simulations are carried out to investigate the dynamic SGS model effects in a Kerosene-LOx coaxial swirl injector under high pressure conditions. The turbulent model is based on large-eddy simulation (LES) with real-fluid transport and thermodynamics. To assess the effect of the dynamic subgrid-scale (SGS) model, the dynamic SGS model is compared with that of the algebraic SGS model. In a swirl injector under supercritical pressure, the characteristics of temporal pressure fluctuation and power spectral density (PSD) present comparable discrepancies dependant on the SGS models, which affect the mixing characteristics. Mixing efficiency and the probability density (PDF) function are conducted for a statistical description of the turbulent flow fields according to the SGS models. The back-scattering of turbulent kinetic energy is estimated in terms of the film thickness of the swirl injector.

표면에 부착된 장애물 주위의 난류전단유동에 관한 수치해석 (Numerical Simulation on Turbulent Shear Flows over Surface-Mounted Obstacles)

  • 명현국
    • 대한기계학회논문집B
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    • 제20권8호
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    • pp.2593-2600
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    • 1996
  • A modified k-$\varepsilon$ turbulence model having a generality is proposed in the present study, in which the constant $C_{\varepsilon2}$in the $\varepsilon$-equation is simply changed as a functional form of a new parameter both satisfying the tensor invariant condition and representing the extra straining effect on complex shear flows. With this model turbulent shear flows over two-dimensional obstacles placed in a channel are numerically studied for different blockage ratios and aspect ratios. Comparing with the available experimental data, the predicted results with the present model provide definite improvements over the standard model's results and work fairly well with the experimental data on the size of the recirculation zone, as well as mean velocity, wall static pressure, turbulent kinetic energy and Reynolds stresses.