• 제목/요약/키워드: viscous fluid flow

검색결과 332건 처리시간 0.024초

패널법과 전산유동해석법의 결합을 이용한 날개단면 주위 점성유동 해석 (Viscous Flow Analysis around a Blade Section by a Hybrid Scheme Combining a Panel Method and a CFD Method)

  • 오진안;이진태
    • 대한조선학회논문집
    • /
    • 제50권5호
    • /
    • pp.355-363
    • /
    • 2013
  • Panel methods are essential tools for analyzing a fluid-flow problem around complex three dimensional bodies, but they lack ability to solve viscous effects. On the other hand, CFD methods are considered as powerful tools for analyzing fluid-flow characteristics including viscosity. However, they also have short falls, requiring more computing time and showing different results depending on the selection of turbulence models and grid systems. In this paper a hybrid scheme combining a panel method and a CFD method is suggested. The scheme adopts a panel method for far-field solution where viscous effects are negligible and a CFD method for the solution of RANS equations in near-field where viscous effects are relatively strong. The intermediate region between the far-field and near-field is introduced where the calculated field point velocities by the panel method are given as boundary velocities for the CFD method. To verify the scheme, calculated results, by a panel method, a CFD method and the hybrid scheme, for a two dimensional foil section are compared. The suggested hybrid scheme gives reasonable results, while computation time and memory can be dramatically reduced. By using the hybrid scheme efforts can be concentrated for the local flow near the leading and trailing edges, by providing more dense grid system, where detailed flow characteristics are required.

평면 점성 정체 유동 응고 문제에 대한 이론적 해석 (A theoretical analysis on the viscous plane stagnation-flow solidification problem)

  • 유주식
    • 설비공학논문집
    • /
    • 제10권3호
    • /
    • pp.260-270
    • /
    • 1998
  • The viscous plane stagnation-flow solidification problem is theoretically investigated. An analytic solution at the beginning of solidification is obtained by expanding the temperature and thickness of solidified layer in powers of time. An exact expression for the steady-state thickness of solidified layer is also obtained. The .fluid flow toward the cold substrate inhibits the solidification process. As Stefan number becomes larger, or Prandtl number becomes smaller, the solidification is more strongly inhibited by the fluid flow. The transient heat flux at the liquid side of solid-liquid interface is increased, as Stefan number or Prandtl number is increased.

  • PDF

원심 펌프 회전차 내부의 저 운동량 유동특성에 관한 수치적 연구 (Numerical Analysis on the Low Momentum Fluid Flow Characteristics in Centrifugal Pump Impeller)

  • 김세진;김동원;김윤제
    • 한국에너지공학회:학술대회논문집
    • /
    • 한국에너지공학회 1999년도 춘계 학술발표회 논문집
    • /
    • pp.151-157
    • /
    • 1999
  • 원심 펌프내 3차원 유동 특성을 고찰하기 위하여 혼류형 원심펌프의 내부유동특성을 수치적 고찰하였다. 회전차 내의 유동현상에 대한 상세한 해석과 이해는 원심펌프의 주요 요소들에 대한 성능 예측에 있어 매우 중요하다. 회전차 내부의 유동은 3차원 점성효과가 지배적이기 때문에 펌프 성능에 중대한 영향을 준다. 회전차내의 3차원 점성유동은 주 영역인 등엔트로피 유동과 원심력과 Coriolis힘에 의한 경계층의 변화, 벽면의 전단응력, 2차 유동(secondary flow)등의 영향에 의한 비가역 영역으로 구분한다. 저 운동량 영역을 만드는 회진차 내부의 점성 유동은 정체영역(blockage)과 실속(stall)이라는 비가역 영역을 만들게 되는데, 결과적으로 펌프의 성능과 효율저하를 유발시킨다. 특히 Coriolis힘과 원심력은 비가역 영역을 증대시키는 가장 큰 힘이라는 사실을 알았다.

  • PDF

Slit 近傍의 Stokeslet 에 의한 2次元의 느린 粘性流動 (Two-Dimensional Slow Viscous Flow Due to a Stokeslet Near a Slit)

  • 고형종;김문언
    • 대한기계학회논문집
    • /
    • 제7권4호
    • /
    • pp.386-391
    • /
    • 1983
  • Two-dimensional slow viscous flow due to a stokeslet near a slit is investigated on the basis of Stokes approximation. Velocity fields and stream function are obtained in closed forms by finding two sectionally holomorphic functions which are determined by reducing the problem to Riemann-Hilbert problems. The force exerted on a small cylinder is calculated for the arbitrary position of the cylinder translating in an arbitrary direction. The features of fluid flow are also investigated.

형상 충전 기법을 이용한 자유표면의 비정상 점성 유동장의 유한 요소 해석 (Finite Element Analysis of Transient Viscous Flow with Free Surface using Filling Pattern Technique)

  • 김기돈;정준호;양동열
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2001년도 추계학술대회논문집B
    • /
    • pp.551-556
    • /
    • 2001
  • The filling pattern technique based on the finite element method and Eulerian mesh advancement approach has been developed to analyze incompressible transient viscous flow with free surfaces. The governing equation for flow analysis is Navier-Stokes equation including inertia and gravity effects. The penalty and predictor-corrector methods are used effectively for finite element formulation. The flow front surface and the volume inflow rate are calculated using the filling pattern technique to select an adequate pattern among four filling patterns at each triangular control volume. Using the proposed numerical technique, the collapse of a dam has been analyzed to predict flow phenomenon of fluid and the predicted front positions versus time have been compared with the reported experimental result.

  • PDF

비압축성 점성유체에 관한 유선상류화 유한요소 해석 (Streamline Upwind FE Analysis for Incompressible Viscous Flow Problem)

  • 최창근;유원진;김윤석
    • 한국전산구조공학회:학술대회논문집
    • /
    • 한국전산구조공학회 1996년도 봄 학술발표회 논문집
    • /
    • pp.54-61
    • /
    • 1996
  • This paper deals with finite element analysis for incompressible viscous flow problem By formulating the governing equation based on the streamline upwind concept , the wiggle phenomenon of fluid flow is minimized in spite of a few number of finite element used. The penalty function method which can reduce the number of independent variables is adopted for the purpose of computational efficiency and the selected reduced integral is carried out for the convection and pressure terms to reserve the stability of solution. In time-history analysis of fluid flow, the accuracy and reliability of an obtained solution are established by using the predictor-corrector method. Finally, correlation studies between analytical and experimental results are conducted wi th the object ive to establish the validity of the proposed numerical approach.

  • PDF

Two-way fluid-structure interaction simulation for steady-state vibration of a slender rod using URANS and LES turbulence models

  • Nazari, Tooraj;Rabiee, Ataollah;Kazeminejad, Hossein
    • Nuclear Engineering and Technology
    • /
    • 제51권2호
    • /
    • pp.573-578
    • /
    • 2019
  • Anisotropic distribution of the turbulent kinetic energy and the near-field excitations are the main causes of the steady state Flow-Induced Vibration (FIV) which could lead to fretting wear damage in vertically arranged supported slender rods. In this article, a combined Computational Fluid Dynamics (CFD) and Computational Structural Mechanic (CSM) approach named two-way Fluid-Structure Interaction (FSI) is used to investigate the modal characteristics of a typical rod's vibration. Performance of an Unsteady Reynolds-Average Navier-Stokes (URANS) and Large Eddy Simulation (LES) turbulence models on asymmetric fluctuations of the flow field are investigated. Using the LES turbulence model, any large deformation damps into a weak oscillation which remains in the system. However, it is challenging to use LES in two-way FSI problems from fluid domain discretization point of view which is investigated in this article as the innovation. It is concluded that the near-wall meshes whiten the viscous sub-layer is of great importance to estimate the Root Mean Square (RMS) of FIV amplitude correctly as a significant fretting wear parameter otherwise it merely computes the frequency of FIV.

진동하는 2차원 날개 단면 주위에 대한 점성 유동장 계산( Part 2. 동적실속이 발생하는 경우 ) (Computation of Viscous Flows around a Two-dimensional Oscillating Airfoil ( Part 2. with Dynamic Stall ))

  • 이평국;김형태
    • 대한조선학회논문집
    • /
    • 제44권1호
    • /
    • pp.16-25
    • /
    • 2007
  • Studies of unsteady-airfoil flows have been motivated mostly by efforts to avoid. or reduce such undesirable effects as flutter, noise and vibrations, dynamic stall. In this paper, we carry out a computational study of viscous flows around a two-dimensional oscillating airfoil to investigate unsteady effects in these important and challenging flows. A fully implicit incompressible RANS solver has been used for calculating unsteady viscous flows around an airfoil. The cell-centered End order finite volume method is utilized to discretize governing equations. in order to ease the flow computation for fluid region changing in time, improve the qualify of solution and simplify the grid generation for an oscillating airfoil flow, the computational method adopts a moving and deforming grid generation technique based on the multi-block grid topology. The numerical method is applied for calculating viscous flows of an oscillating NACA 0012 in uniform flow. The computational results are compared with available experimental data. Computed results are compared with experimental data and flow characteristics of the experiment are reproduced well In the computed results.

동심원내에서 진동하는 내부 실린더에 작용하는 유체유발력의 근사적 해법 (An Approximate Analytical Method for Hydrodynamic Forces on Oscillating Inner Cylinder in Concentric Annulus)

  • 심우건
    • 소음진동
    • /
    • 제7권5호
    • /
    • pp.861-869
    • /
    • 1997
  • An approximate analytical method has been developed for estimating hydrodynamic forces acting on oscillating inner cylinder in concentric annulus. When the rigid inner cylinder executes translational oscillation, fluid inertia and damping forces on the oscillating cylinder are generated by unsteady pressure and viscous skin friction. Considering the dynamic-characteristics of unsteady viscous flow and the added mass coefficient of inviscid fluid, these hydrodynamic forces including viscous effect are dramatically simplified and expressed in terms of oscillatory Reynolds number and the geometry of annular configuration. Thus, the viscous effect on the forces can be estimated very easily compared to an existing theory. The forces are calculated by two models developed for relatively high and low oscillatory Reynolds numbers. The model for low oscillatory Reynolds number is suitable for relatively high ratio of the penetration depth to annular space while the model for high oscillatory Reynolds number is applicable to the case of relatively low ratio. It is found that the transient ratio between two models is approximately 0.2~0.25 and the forcea are expressed in terms of oscillatory Reynolds number, explicity. The present results show good agreements with an existing numerical results, especially for high and low penetration ratios to annular gap.

  • PDF