• 제목/요약/키워드: Navier stokes

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Mixer-Ejector 노즐 유동장에 관한 수치해석 (Computational Analysis of the Flowfield of a Mixer-Ejector Nozzle)

  • Park, Yun-Ho
    • 한국추진공학회지
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    • 제6권1호
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    • pp.71-82
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    • 2002
  • 본 연구에서는 2차원의 압축성 Navier-Stokes 코드를 개발하여 mixer-ejector 노즐의 유동장 해석을 다양한 덕트와 노즐 면적비 및 노즐 압력비에 대하여 계산을 수행하였다. 덕트와 노즐 면적비 계산에서는 먼저 효율적인 2차 유동의 유입을 위한 최적의 면적비가 있음을 볼 수 있었다. 높은 면적비에서는 입구 자유유동의 적절한 혼합없이 mixing duct를 그대로 통과하는 것을 볼 수 있었고, 낮은 면적비에서는 제트의 경계가 유입 유동에 장애물로 작용하는 것을 볼 수 있었다. 노즐 압력비의 계산에 있어서는 shroud 벽면과 shock cell structure 간에 상호작용이 작다면 유입유량은 압력비에 따라 증가하는 것을 볼 수 있었다.

CFD 기반 유체충격 해석에서 공기 압축성 효과 (Air Compressibility Effect in CFD-based Water Impact Analysis)

  • 찬후피;안형택
    • 대한조선학회논문집
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    • 제48권6호
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    • pp.581-591
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    • 2011
  • This paper describes the air compressibility effect in the CFD simulation of water impact load prediction. In order to consider the air compressibility effect, two sets of governing equations are employed, namely the incompressible Navier-stokes equations and compressible Navier-Stokes equations that describe general compressible gas flow. In order to describe violent motion of free surface, volume-of-fluid method is utilized. The role of air compressibility is presented by the comparative study of water impact load obtained from two different air models, i.e. the compressible and incompressible air. For both cases, water is considered as incompressible media. Compressible air model shows oscillatory behavior of pressure on the solid surface that may attribute to the air-cushion effect. Incompressible air model showed no such oscillatory behavior in the pressure history. This study also showed that the CFD simulation can capture the formation of air pockets enclosed by water and solid surface, which may be the location where the air compressibility effect is dominant.

설계유량을 변수로 한 원심다익송풍기의 최적설계 (Design Optimization of A Multi-Blade Centrifugal Fan With Variable Design Flow Rate)

  • 서성진;김광용
    • 대한기계학회논문집B
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    • 제28권11호
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    • pp.1332-1338
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    • 2004
  • This paper presents the response surface optimization method using three-dimensional Navier-Stokes analysis to optimize the shape of a forward-curved blades centrifugal fan. For numerical analysis, Reynolds-averaged Navier-Stokes equations with k-$\varepsilon$ turbulence model are discretized with finite volume approximations. In order to reduce huge computing time due to a large number of blades in forward-curved blades centrifugal fan, the flow inside of the fan is regarded as steady flow by introducing the impeller force models. Three geometric variables, i.e., location of cut off, radius of cut off, and width of impeller, and one operating variable, i.e., flow rate, were selected as design variables. As a main result of the optimization, the efficiency was successfully improved. And, optimum design flow rate was found by using flow rate as one of design variables. It was found that the optimization process provides reliable design of this kind of fans with reasonable computing time.

3차원 동수역학모형-유류확산모형 연계를 통한 유출유 거동 모의 (Oil Spill Simulation by Coupling Three-dimensional Hydrodynamic Model and Oil Spill Model)

  • 정태화;손상영
    • 한국해양공학회지
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    • 제32권6호
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    • pp.474-484
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    • 2018
  • In this study, a new numerical modeling system was proposed to predict oil spills, which increasingly occur at sea as a result of abnormal weather conditions such as global warming. The hydrodynamic conditions such as the flow velocity needed to calculate oil dispersion were estimated using a three dimensional hydrodynamic model based on the Navier-Stokes equation, which considered all of the physical variations in the vertical direction. This improved the accuracy compared to those estimated by the conventional shallow water equation. The advection-diffusion model for the spilled oil was combined with the hydrodynamic model to predict the movement and fate of the oil. The effects of absorption, weathering, and wind were also considered in the calculation process. The combined model developed in this study was then applied to various test cases to identify the characteristics of oil dispersion over time. It is expected that the developed model will help to establish initial response and disaster prevention plans in the event of a nearshore oil spill.

AN ENERGY-STABLE AND SECOND-ORDER ACCURATE METHOD FOR SOLVING THE INCOMPRESSIBLE NAVIER-STOKES EQUATIONS

  • KIM, JEONGHO;JUNG, JINWOOK;PARK, YESOM;MIN, CHOHONG;LEE, BYUNGJOON
    • Journal of the Korean Society for Industrial and Applied Mathematics
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    • 제23권2호
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    • pp.93-114
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    • 2019
  • In this article, we introduce a finite difference method for solving the Navier-Stokes equations in rectangular domains. The method is proved to be energy stable and shown to be second-order accurate in several benchmark problems. Due to the guaranteed stability and the second order accuracy, the method can be a reliable tool in real-time simulations and physics-based animations with very dynamic fluid motion. We first discuss a simple convection equation, on which many standard explicit methods fail to be energy stable. Our method is an implicit Runge-Kutta method that preserves the energy for inviscid fluid and does not increase the energy for viscous fluid. Integration-by-parts in space is essential to achieve the energy stability, and we could achieve the integration-by-parts in discrete level by using the Marker-And-Cell configuration and central finite differences. The method, which is implicit and second-order accurate, extends our previous method [1] that was explicit and first-order accurate. It satisfies the energy stability and assumes rectangular domains. We acknowledge that the assumption on domains is restrictive, but the method is one of the few methods that are fully stable and second-order accurate.

A STABILITY RESULT FOR THE COMPRESSIBLE STOKES EQUATIONS USING DISCONTINUOUS PRESSURE

  • Kweon, Jae-Ryong
    • 대한수학회지
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    • 제36권1호
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    • pp.159-171
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    • 1999
  • We formulate and study a finite element method for a linearized steady state, compressible, viscous Navier-Stokes equations in 2D, based on the discontinuous Galerkin method. Dislike the standard discontinuous galerkin method, we do not assume that the triangle sides be bounded away from the characteristic direction. the unique stability follows from the inf-sup condition established on the finite dimensional spaces for the (incompressible) Stokes problem. An error analysis having a jump discontinuity for pressure is shown.

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HOMOGENIZATION OF THE NON-STATIONARY STOKES EQUATIONS WITH PERIODIC VISCOSITY

  • Choe, Hi-Jun;Kim, Hyun-Seok
    • 대한수학회지
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    • 제46권5호
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    • pp.1041-1069
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    • 2009
  • We study the periodic homogenization of the non-stationary Stokes equations. The fundamental homogenization theorem and corrector theorem are proved under a very general assumption on the viscosity coefficients and data. The proofs are based on a weak formulation suitable for an application of classical Tartar's method of oscillating test functions. Such a weak formulation is derived by adapting an argument in Teman's book [Navier-Stokes Equations: Theory and Numerical Analysis, North-Holland, Amsterdam, 1984].

축류송풍기의 저소음 설계에서 수치최적화기법들의 평가 (Assessment of Numerical Optimization Algorithms in Design of Low-Noise Axial-Flow Fan)

  • 최재호;김광용
    • 대한기계학회논문집B
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    • 제24권10호
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    • pp.1335-1342
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    • 2000
  • Three-dimensional flow analysis and numerical optimization methods are presented for the design of an axial-flow fan. Steady, incompressible, three-dimensional Reynolds-averaged Navier-Stokes equations are used as governing equations, and standard k- ${\varepsilon}$ turbulence model is chosen as a turbulence model. Governing equations are discretized using finite volume method. Steepest descent method, conjugate gradient method and BFGS method are compared to determine the searching directions. Golden section method and quadratic fit-sectioning method are tested for one dimensional search. Objective function is defined as a ratio of generation rate of the turbulent kinetic energy to pressure head. Two variables concerning sweep angle distribution are selected as the design variables. Performance of the final fan designed by the optimization was tested experimentally.

SMAC 음해법에 의한 큰 곡률를 갖는 정사각형 덕트내의 비압축성 층류 입구유동 (Incompressible Laminar Entry Flows in a Square Duct of Strong Curvature Using an Implicit SMAC Scheme)

  • 신병록;정소추 이 명
    • 한국전산유체공학회지
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    • 제1권1호
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    • pp.35-46
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    • 1996
  • 원심형 임펠러 내부 유로등 큰 곡률을 수반하는 터보기계 요소의 유동해석을 위한 계산코드를 개발하였다. 이 코드에서는 곡선좌표계에 유도된 3차원 비압축성 Navier-Stokes의 운동 방정식을 SMAC 음해법으로 푼다. 이 코드를 이용하여 유로의 단면이 정사각형이고 90도로 굽은 덕트내부의 층류 입구유동을 해석하고, 굽은 관 특유의 유동현상을 수치모사하였다 또한 곡관부 입구에서 충분히 발달한 유동, 또는 발달중인 유동이 유입될 경우에 이것이 곡관부 내부의 유동에 미치는 영향을 상·하류의 계산영역이 서로 다를 몇몇 유동장에 대하여 조사하고, 본 계산에서 얻어진 결과와 실형결과와의 비교로 본 3차원 유동해석 코드의 유효성을 검토 하였다.

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비압축성 Navier-Stokes 방정식에 대한 Krylov 부공간법의 적용 (Application of the Krylov Subspace Method to the Incompressible Navier-Stokes Equations)

  • 맹주성;최일곤;임연우
    • 대한기계학회논문집B
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    • 제24권7호
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    • pp.907-915
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    • 2000
  • The preconditioned Krylov subspace methods were applied to the incompressible Navier-Stoke's equations for convergence acceleration. Three of the Krylov subspace methods combined with the five of the preconditioners were tested to solve the lid-driven cavity flow problem. The MILU preconditioned CG method showed very fast and stable convergency. The combination of GMRES/MILU-CG solver for momentum and pressure correction equations was found less dependency on the number of the grid points among them. A guide line for stopping inner iterations for each equation is offered.