• 제목/요약/키워드: Lattice Boltzmann

검색결과 173건 처리시간 0.027초

마이크로 채널 내의 이상유동에 대한 실험 및 수치해석적 연구 (Experimental and Numerical Study on the Binary Fluid Flows in a Micro Channel)

  • 박재현;허형석;서용권
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2006년도 추계학술대회 논문집
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    • pp.86-91
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    • 2006
  • In this parer, we present the bubble forming and motion in the micro channel by using the two-dimensional numerical computation and experiment. In the numerical computation, The Lattice Boltzmann method(LBM) and free-energy model is used to treat the interfacial force and deformation of binary fluid system, drawn in to a micro channel and a numerical simulation is carried out by using the parallel computation method. The urn in this investigation is to examine the applicability of LBM to numerical analysis and experimental method of binary fluid separation and motion in the micro channel.

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Numerical Prediction of Acoustic Sounds Occurring by the Flow Around a Circular Cylinder

  • Kang, Ho-Keun;Ro, Ki-Deok;Michihisa Tsutahara;Lee, Young-Ho
    • Journal of Mechanical Science and Technology
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    • 제17권8호
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    • pp.1219-1225
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    • 2003
  • Acoustic sounds generated by uniform flow around a two-dimensional circular cylinder at Re=150 are simulated by applying the finite difference lattice Boltzmann method. A third-order-accurate up-wind scheme is used for the spatial derivatives. A second-order-accurate Runge-Kutta scheme is also used for time marching. Very small acoustic pressure fluctuation, with same frequency as that of Karman vortex street, is compared with pressure fluctuation around a circular cylinder. The propagation velocity of acoustic sound shows that acoustic approaching the upstream, due to the Doppler effect in uniform flow, slowly propagates. For the downstream, on the other hand, it quickly propagates. It is also apparent that the size of sound pressure is proportional to the central distance ${\gamma}$$\^$-1/2/ of the circular cylinder.

미소 채널의 형상변화에 의한 혼합효율에 관한 수치 해석적 연구 (Numerical Analysis on Mixing Efficiency in a Micro-channel with Varied Geometry)

  • 윤준용;한규석;변성준
    • 공업화학
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    • 제16권2호
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    • pp.275-281
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    • 2005
  • 본 연구에서는 격자 볼츠만 방법 중 Scalar Passive 코드를 사용하여 미소채널 내에서의 수동형 믹서의 혼합에 대하여 계산을 수행하였다. 미소채널 내에서의 수동형 믹서의 혼합에 대하여 유선과 압력분포를 통해 혼합과 압력 강하를 물리적으로 규명하였으며, 혼합에 영향을 주는 인자에 대해서 알아보았다. 수동형 믹서의 경우 고정물의 간격보다는 고정물의 개수와 고정물의 크기가 혼합효율과 압력강하에 큰 영향을 주었다.

내부자유도를 갖는 차분래티스볼츠만 모델에 의한 에지톤의 수치계산 (Numerical Simulation of Edge Tone by Finite Difference Lattice Boltzmann Model with Internal Degree of Freedom)

  • 강호근;김은라;오세경
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권8호
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    • pp.929-937
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    • 2005
  • A lattice BGK model based on a finite difference scheme with an internal degree of freedom is employed and it is shown that a diatomic 9as such as air is successfully simulated In a weak compressive wane problem and Coutte flow, the validity and characteristics of the applied model are examined. With the model. furthermore. we present a 2-dimensional edge tones to predict the frequency characteristics of discrete oscillations of a jet-edge feedback cycle by the FDLB model (I.D.F FDLBM) in which any specific heat ratio $\gamma$ can be chosen freely. The jet is chosen long enough in order to guaranteed the Parabolic velocity profile of a jet at the outlet. and the edges have of an angle of $\alpha$=$23^{0}$ and $20^{0}$. A sinuous instability wane with real frequency resulting from Periodic oscillation of the jet around the edge is propagated on the upper and lower of wedge.

Vortex-Edge의 상호작용에 기인한 유동소음의 전산해석 (Numerical Analysis of Flow-Induced Noise by Vortex-Edge Interaction)

  • 강호근;김은라
    • 한국해양공학회지
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    • 제18권5호
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    • pp.15-21
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    • 2004
  • An edge tone is the discrete tone or narrow-band sound produced by an oscillating free shear layer, impinging on a rigid surface. In this paper, we present a 2-D edge tone to predict the frequency characteristics of the discrete oscillations of a jet-edge feedback cycle, using the finite difference lattice Boltzmann method (FDLBM). We use a modified version of the lattice BGK compressible fluid model, adding an additional term and allowing for longer time increments, compared to a conventional FDLBM, and also use a boundary fitted coordinates system. The jet is chosen long enough in order to guarantee the parabolic velocity profile of the jet at the outlet, and the edge consists of a wedge with an angle of ${\alpha}$ = 23. At a stand-off distance, the edge is inserted along the centerline of the jet, and a sinuous instability wave, with real frequency, is assumed to be created in the vicinity of the nozzle and propagates towards the downstream. We have succeeded in capturing very small pressure fluctuations, resulting from periodical oscillations of a jet around the edge. The pressure fluctuations propagate with the speed of sound. Its interaction with the wedge produces an non-rotational feedback field, which, near the nozzle exit, is a periodic transverse flow, producing the singularities at the nozzle lips.

Vortex-Edge 의 상호작용에 의한 유동소음의 수치계산 (Numerical Investigation of Aerodynamic Sounds by Vortex-Edge Interaction)

  • 강호근;김정환;김유택;이영호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1915-1920
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    • 2004
  • An edge tone is the discrete tone or narrow-band sound produced by an oscillating free shear layer impinging on a rigid surface. In this paper we present a two-dimensional edge tone to predict the frequency characteristics of the discrete oscillations of a jet-edge feedback cycle by the finite difference lattice Boltzmann method. We use a new lattice BGK compressible fluid model that has an additional term and allow larger time increment comparing a conventional FDLB model, and also use a boundary fitted coordinates. The jet is chosen long enough in order to guarantee the parabolic velocity profile of the jet at the outlet, and the edge consists of a wedge with an angle of ${\alpha}=23^{\circ}$ . At a stand-off distance ${\omega}$ , the edge is inserted along the centreline of the jet, and a sinuous instability wave with real frequency f is assumed to be created in the vicinity of the nozzle and to propagate towards the downstream. We have succeeded in capturing very small pressure fluctuations result from periodically oscillation of jet around the edge. That pressure fluctuations propagate with the sound speed. Its interaction with the wedge produces an irrotational feedback field which, near the nozzle exit, is a periodic transverse flow producing the singularities at the nozzle lips.

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격자 볼츠만 방법에 의한 지반 내 오염물질의 거동 분석 (Analysis of Contaminant Transport in the Ground using the Lattice-Boltzmann Method)

  • 강동훈;윤태섭
    • 대한토목학회논문집
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    • 제32권6C호
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    • pp.267-274
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    • 2012
  • 오염물질의 거동은 간극 배열과 연결망에 의해 결정되지만 흙에서 오염물질의 이동을 계산하는 전통적인 접근은 거시 스케일에서 적용된다. 나비에-스토크스 방정식을 풀기 위해 소요되는 컴퓨팅 비용 때문에 간극 스케일에서 이동과 결과를 관찰하기 쉽지 않다. 본 논문에서는 단일상 다성분 유체유동에서 국부적인 유속과 밀도를 효과적으로 평가할 수 있는 격자 볼츠만 방법에 대해 설명한다. 오염물질의 시공간적 거동은 유체 유동의 이송에 의해 명시적으로 결정된다. 두 가지 형태의 이상화된 간극은 유체의 경로를 제공한다. 또한 오염물질 이동, 유속장, 오염물질의 평균 농도는 정상상태의 유동에서 계산된다. 굴곡비와 같은 간극 형상은 오염물질 거동의 영향을 준다. 이는 흙이나 암반의 불연속면에서 동일한 간극률를 가져도 간극의 배열과 형상의 중요함을 강조한다.