• Title/Summary/Keyword: Turbulent Scale

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The Study on Changes of Mixing Layer Caused by Acoustic Excitation (음향 여기에 의한 혼합층 유동구조의 변화에 대한 연구)

  • 정양범
    • Journal of Advanced Marine Engineering and Technology
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    • v.24 no.6
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    • pp.120-127
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    • 2000
  • This study is concerned with evaluating the effects of acoustic excitation on the development of two stream mixing layer generated by split plate. The ratios of two velocities U1 and U2 either side of the splitter plate were such that $U_1/U_2$=1.0 (uniform flow) or $U_1/U_2$<1.0(shear flow). The mixing layers were disturbed acoustically through the edge of split plate. Quantitative data were obtained with hot-wire anemometry. Flow visualization with smoke-wire was also employed for qualitative study. the results show that the large scale structures of mixing layers are strongly affected by excitation frequency and amplitude in both uniform and shear flows. The maximum streamwise and vertical turbulent intensities of the excited flow fields are apt to be decreased as compared with those of without excitation. The flow characteristics of uniform flow are more influenced by acoustic excitation than those of shear flow.

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Large-eddy simulation of a turbulent buoyant jet (난류 부력젵의 큰 와 모의)

  • Paik, Joong-Cheol
    • Proceedings of the Korea Water Resources Association Conference
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    • 2011.05a
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    • pp.134-134
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    • 2011
  • 3차원 난류 부력젵의 혼합을 큰 와 모의(large-eddy simulation) 기법을 이용하여 수치모의 한다. 개발된 수치모형은 3차원 열동수역학 모형을 이용하여 부력젵의 퍼짐, 자기 보존 그리고 주변류의 연행 등을 포함하는 난류젵의 동적 특성을 분석할 수 있다. 수치해석에서 하부격자규모 (subgrid scale, SGS) 난류 응력은 부력항을 수정한 Smagorinsky 모형을 이용한다. 여과된 엔탈피 수송방정식에서 하부격자규모의 스칼라 플럭스는 상수의 SGS Prandtl 수를 가지는 단순 경사수송 가설에 근거하여 모의한다. 계산된 결과를 실험결과와 비교하며, 결과는 양호하게 일치함을 보여준다. 계산결과에 따르면 부력항의 수정이나 SGS 난류 Prandtl 수는 결과에 큰 영향을 미치지 않지만 SGS 모형 상수인 Cs 값은 부력젵 확산 예측에 중요한 영향을 미치는 것으로 나타났다.

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Experimental and Numerical Investigation for NOx Reduction with Fuel Lean Reburning System (NOx저감을 위한 연료희박 재연소 기법의 실험 및 수치적 연구)

  • Kim, Hak-Young;Baek, Seung-Wook;Son, Hee;Kim, Se-Won
    • Journal of the Korean Society of Combustion
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    • v.14 no.2
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    • pp.18-25
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    • 2009
  • Fuel lean reburning method is very attractive way in comparison with conventional reburning method for reducing NOX. Meanwhile, the knowledge of the how flue gas re-circulated, temperature distribution and species concentration is crucial for the design and operation of an effective fuel lean reburning system. For this reason, numerical analysis of fuel lean reburning system is a very important and challenge task. In this work, the effect of fuel lean reburn system on NOX reduction has been experimentally and numerically conducted. Experimental study has been conducted with a 15kW lab scale furnace. Liquefied Petroleum Gas is used as main fuel and reburn fuel. To carry out numerical study, the finite-volume based commercial computational fluid dynamics (CFD) code FLUENT6.3 was used to simulate the reacting flow in a given laboratory furnace. Steady state, three dimensional analysis performed for turbulent reactive flow and radiative heat transfer in the furnace.

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PDF properties of ISM turbulence

  • Jo, Hyeon-Jin;Gang, Hye-Seong;Ryu, Dong-Su;Kim, Jong-Su;Jo, Jeong-Yeon
    • The Bulletin of The Korean Astronomical Society
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    • v.36 no.2
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    • pp.107.1-107.1
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    • 2011
  • Density Probability Distribution Functions (PDFs) are a classic statistical way to study properties of Interstellar Medium (ISM) turbulence. In our three-dimensional MHD simulations, density PDFs of the position-position velocity (PPV) spaces are close to a log-normal distribution. the PDF widths depend on the plasma parameters such as magnetic strength and sonic Mach number. Futhermore, we compare these simulations results to Galactic molecular clouds observed by Jackson et. al (2006). By fitting of the velocity dispersion in the spectral line observation, volume density PDFs of the defined molecular clouds indicate that the sound speeds of the turbulences seem to have a few times larger than the simulation results. In order to understand the inconsistency with general characteristics of turbulence, we consider other simulations inducing the turbulent flow randomly at small driving scales. We find that the density PDF width decreases at more smaller driving scale. Finally, the simulations suggest that sources of ISM turbulence in Galactic molecular clouds can be important on small scales.

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Depth-Integrated Models for Turbulent Flow and Transport by Long Wave and Current (흐름과 장파에 의해 발생하는 난류 및 수송모의를 위한 수심적분형 모형)

  • Kim, Dae-Hong;Lynett, Patrick
    • Proceedings of the Korea Water Resources Association Conference
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    • 2010.05a
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    • pp.546-550
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    • 2010
  • 흐름과 장파에 의하여 발생되는 난류의 subgrid scale mixing effects를 고려할 수 있는 수심적분형 모형(depth-integrated model)을 제시하였다. 완전비선형의 수심적분형 모형은 약분산(weakly dispersive) 환경에서 흐름의 회전성(rotational)을 고려하도록 perturbation approach를 이용하여 유도되었다. 동일한 방법을 이용하여 수심적분형 이송확산방정식(depth-integrated scalar transport equation)을 유도하였다. 방정식은 4차정확도의 유한체적기법을 이용하여 해석하였으며, 다양한 혼합양상을 보이는 흐름에 대한 수치모의를 수행하였다.

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Interaction of turbulences with non-breaking divergent waves in an open channel

  • Hwang, Ayoung;Seok, Woochan;Lee, Sang Bong
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.13 no.1
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    • pp.35-49
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    • 2021
  • This paper presents a direct numerical simulation of turbulent flows over a bump in an open channel to examine the turbulence characteristics near divergent waves emanating from the bump and to investigate the interaction of the turbulences with the divergent waves. To verify the reliability of the simulations, the mean velocity profile and root-mean-square of velocity fluctuations are compared with previous data. The anisotropic invariant maps show that the ratio of the streamwise to spanwise velocity fluctuations plays an important role in characterizing the anisotropic nature of the separated shear layer behind the bump in the vicinity of the free surface. The vortex identification discloses a large-scale streamwise vortical structure from the mean velocity field and a cluster of small coherent structures from the instantaneous velocity field, which are responsible for the anisotropic characteristics of the turbulence beneath the free surface.

Relationship Between Local Wall Thinning and Velocity Components of Deflected Turbulent Flow Inside the Tee Sections of Carbon Steel Piping (탄소강 배관 티에서 편향 난류유동에 따른 속도성분과 국부감육의 상관관계)

  • Kim, Kyung-Hoon;Hwang, Kyeong-Mo;Kang, Deok-Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.35 no.7
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    • pp.717-722
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    • 2011
  • The aim of this study is to identify the locations at which local wall thinning occurs and to determine the turbulence coefficients related to local wall thinning. Experiments and numerical analyses of the tee sections of different down-scaled piping components were performed and the results were compared. Numerical analyses of full-scale models of actual plants were performed in order to simulate the flow behaviors inside the piping components. In order to determine the relationship between the turbulence coefficients and the rate of local wall thinning, numerical analyses of the tee components in the main feedwater systems were performed. The turbulence coefficients obtained from the numerical analyses were compared with the local wear rate obtained from the measurement data. From the comparison of the results, the vertical flow velocity component (Vr) flowing to the wall after separating in the wall due to the geometrical configuration and colliding with the wall directly at an angle of some degree was analogous to the configuration of local wall thinning.

Vortex induced vibration and flutter instability of two parallel cable-stayed bridges

  • Junruang, Jirawat;Boonyapinyo, Virote
    • Wind and Structures
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    • v.30 no.6
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    • pp.633-648
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    • 2020
  • The objective of this work was to investigate the interference effects of two-parallel bridge decks on aerodynamic coefficients, vortex-induced vibration, flutter instability and flutter derivatives. The two bridges have significant difference in cross-sections, dynamic properties, and flutter speeds of each isolate bridge. The aerodynamic static tests and aeroelastic tests were performed in TU-AIT boundary layer wind tunnel in Thammasat University (Thailand) with sectional models in a 1:90 scale. Three configuration cases, including the new bridge stand-alone (case 1), the upstream new bridge and downstream existing bridge (case 2), and the downstream new bridge and the upstream existing bridge (case 3), were selected in this study. The covariance-driven stochastic subspace identification technique (SSI-COV) was applied to identify aerodynamic parameters (i.e., natural frequency, structural damping and state space matrix) of the decks. The results showed that, interference effects of two bridges decks on aerodynamic coefficients result in the slightly reduction of the drag coefficient of case 2 and 3 when compared with case 1. The two parallel configurations of the bridge result in vortex-induced vibrations (VIV) and significantly lower the flutter speed compared with the new bridge alone. The huge torsional motion from upstream new bridge (case 2) generated turbulent wakes flow and resulted in vertical aerodynamic damping H1* of existing bridge becomes zero at wind speed of 72.01 m/s. In this case, the downstream existing bridge was subjected to galloping oscillation induced by the turbulent wake of upstream new bridge. The new bridge also results in significant reduction of the flutter speed of existing bridge from the 128.29 m/s flutter speed of the isolated existing bridge to the 75.35 m/s flutter speed of downstream existing bridge.

A Study on the Particle Behavior in Turbulent Pulverized Coal Flame (난류 미분탄화염 내 입자거동에 관한 연구)

  • Hwang, Seung-Min
    • Journal of Korean Society of Environmental Engineers
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    • v.32 no.12
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    • pp.1111-1118
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    • 2010
  • Combustion measurements based on optical techniques have recently become of major interest as tools not only for clarifying the combustion mechanism but also for validating the computational results for the combustion fields. In this study, the particle behavior in turbulent pulverized coal flame are investigated using advanced optical diagnostics. A laboratory-scale pulverized coal combustion burner is specially fabricated as open type in order to apply various optical measurement techniques. The detailed particle behavior is performed by LDV (laser Doppler velocimetry) and SDPA (shadow Doppler particle analyzer). It is observed that the particle mean diameter increase as the distance from burner increases, and this is found to be caused by the decrease of small particles' diameter and increase of large particles' diameter. This is because of result in the char reaction and the particle swelling due to devolatilization, respectively. The size-classified streamwise velocities of pulverized coal particles in the central region of the jet show the same magnitude, whereas those in the outer region are different depending on the particle size. The results show that the velocity and size-classified diameter of the pulverized coal particles in the flame can be measured well by SDPA.

An Analytical Investigation on the Build-up of the Temperature Field due to a Point Heat Source in Shallow Coastal Water with Oscillatory Alongshore-flow

  • Jung, Kyung-Tae;Kim, Chong-Hak;Jang, Chan-Joo;Lee, Ho-Jin;Kang, Sok-Kuh;Yjm, Ki-Dai
    • Ocean and Polar Research
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    • v.25 no.1
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    • pp.63-74
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    • 2003
  • The build-up of the heat field in shallow coastal water due to a point source has been investigated using an analytical solution of a time-integral form derived by extending the solutions by Holley(1969) and also presented in Harleman (1971). The uniform water depth is assumed with non-isotropic turbulent dispersion. The alongshore-flow is assumed to be uni-directional, spatially uniform and oscillatory. Due to the presence of the oscillatory alongshore-flow, the heat build-up occurs in an oscillatory manner, and the excess temperature thereby fluctuates in that course and even in the quasi-steady state. A series of calculations reveal that proper choices of the decay coefficient as well as dispersion coefficients are critical to the reliable prediction of the excess temperature field. The dispersion coefficients determine the absolute values of the excess temperature and characterize the shoreline profile, particularly within the tidal excursion distance, while the decay coefficient determines the absolute value of the excess temperature and the convergence rate to that of the quasi-steady state. Within the e-folding time scale $1/k_d$ (where $k_d$ is the heat decay coefficient), heat build-up occurs more than 90% of the quasi-steady state values in a region within a tidal excursion distance (L), while occurs increasingly less the farther we go to the downstream direction (about 80% at 1.25L, and 70% at 1.5L). Calculations with onshore and offshore discharges indicate that thermal spreading in the direction of the shoreline is reduced as the shoreline constraint which controls the lateral mixing is reduced. The importance of collecting long-term records of in situ meteorological conditions and clarifying the definition of the heat loss coefficient is addressed. Interactive use of analytical and numerical modeling is recommended as a desirable way to obtain a reliable estimate of the far-field excess temperature along with extensive field measurements.