• 제목/요약/키워드: viscous boundary

검색결과 304건 처리시간 0.027초

Boundary layer analysis of persistent moving horizontal needle in Blasius and Sakiadis magnetohydrodynamic radiative nanofluid flows

  • Krishna, Penem Mohan;Sharma, Ram Prakash;Sandeep, Naramgari
    • Nuclear Engineering and Technology
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    • 제49권8호
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    • pp.1654-1659
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    • 2017
  • The boundary layer of a two-dimensional forced convective flow along a persistent moving horizontal needle in an electrically conducting magnetohydrodynamic dissipative nanofluid was numerically investigated. The energy equation was constructed with Joule heating, viscous dissipation, uneven heat source/sink, and thermal radiation effects. We analyzed the boundary layer behavior of a continuously moving needle in Blasius (moving fluid) and Sakiadis (quiescent fluid) flows. We considered Cu nanoparticles embedded in methanol. The reduced system of governing Partial differential equations (PDEs) was solved by employing the Runge-Kutta-based shooting process. Computational outcomes of the rate of heat transfer and friction factors were tabulated and discussed. Velocity and temperature descriptions were examined with the assistance of graphical illustrations. Increasing the needle size did not have a significant influence on the Blasius flow. The heat transfer rate in the Sakiadis flow was high compared with that in the Blasius flow.

밀도 성층 유동 해석을 위한 가상경계법 (An Immersed-Boundary Method for Simulation of Density-Stratified Flows)

  • 윤동혁;양경수;황종연;이승수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1909-1914
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    • 2004
  • An immersed boundary method for simulation of density-stratified flows is developed and applied to computation of viscous flows over two-dimensional obstacles in a bounded domain under stable density stratification. Density sources/sinks are introduced on the body surface. Two obstacle shapes are used, a vertical barrier and a smooth cosine-shaped hill; weak stratification, defined by $K=ND/{\pi}U{\leq}1$, where U, N, and D are the upstream velocity, buoyancy frequency, and domain height, respectively, is considered. The results are consistent with other authors' calculations, and shed light on computation of density-stratified flows in complex geometries.

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레벨셋법을 이용한 이동 집중격자 생성법에 대한 연구 (A Study on a Moving Adaptive Grid Generation Method Using a Level-set Scheme)

  • 박일룡;전호환
    • 대한조선학회논문집
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    • 제39권3호
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    • pp.18-27
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    • 2002
  • Eulerian개념을 사용한 격자계 내 임의의 경계면 주위 점성유동 해석에서, 운동하며 변형하는 경계면 근방 해의 정도를 향상시키기 위해서 격자생성시 경계면으로 격자점들을 집중시켜주는 레벨셋법에 바탕을 둔 격자변형법을 도입하였다. 본 연구에서는 격자점들을 경계면 근방으로 집중되는 정도를 용이하게 조절할 수 있도록 새로운 형태의 모니터함수를 제시하였다. 집중격자계를 사용함으로 얻어지는 향상된 해의 정도의 검증을 위하여 바닥에 고정된 반원 실린더 주위 정상유동에 대하여 가상경계법을 함께 사용하여 해석하였다. 수치계산결과는 물체적합 격자계를 사용해서 얻은 결과와 매우 잘 일치하였으며, 집중격자법을 사용하지 않은 해석결과보다 향상된 결과를 보여주었다. 수치계산의 또 다른 예제로서 다수의 고정된 물체주위 유동해석으로 확장 적용하여 공학적 유용성을 검증하였다. 마지막으로 이동 집중격자계의 생성법의 적용을 위해서 움직이면서 변형을 일으키는 2차원 기포상승문제를 해석하였다. 수치해석결과에서 격자점들은 매시간 기포의 변형에 맞추어 적합하게 집중된 형태를 잘 보여주었으며, 고정된 격자계를 사용한 결과와 잘 일치하였다.

Three-dimensional numerical simulation of nonisothermal coextrusion process with generalized Newtonian fluids

  • Sunwoo, Ki-Byung;Park, Seung-Joon;Lee, Seong-Jae;Ahn, Kyung-Hyun;Lee, Seung-Jong
    • Korea-Australia Rheology Journal
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    • 제12권3_4호
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    • pp.165-173
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    • 2000
  • Three-dimensional numerical simulation of isothermal/nonisothermal coextrusion process of two immiscible polymers through a rectangular channel has been done using the finite element method. The encapsulation phenomenon with the less viscous layer encapsulating the more viscous layer was investigated with the generalized Newtonian fluids. The interface position around the symmetric plane obtained by numerical simulation nearly coincided with the one observed in experiments, but the degree of encapsulation was less than the one observed experimentally. Open boundary condition method was found to be applied to the simulation of nonisothermal coextrusion process, however, the results are not far from those using the fully developed boundary condition, because the temperature development along the downstream direction is very slow in the case of convection dominated flow. When the inlet velocity is increased, the interface profile does not change in isothermal flow, while it moves upward in nonisothermal situation. The degree of encapsulation decreases along the downstream direction in nonisothermal flow. When the inlet temperature increases compared to the wall temperature, the outlet interface moves downward and the degree of encapsulation increases. The difference of degree of encapsulation between the simulation and the experiments seems to arise from the viscoelastic effect of the materials. It was concluded that the nonisothermal effect alone does not explain the complex coextrusion process and the viscoelastic effect needs to be considered.

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건선(乾癬)환자의 임상(臨床) 치험례(治驗例) 보고 (Report on the Clinical Treatment of Psoriasis Patients)

  • 원영호;장안수;홍요한
    • 한방안이비인후피부과학회지
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    • 제21권2호
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    • pp.165-175
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    • 2008
  • Psoriasis, which is characterized by the covering of silver-white scaliness and various Sizes of redness with clear boundary, is an intractable skin disease that repeats aggravation and remission. The objective of the present clinical report is to demonstrate that oriental medical treatment after differentiation of syndromes is effective in treating psoriasis, an intractable skin disease. For this purpose, we identified the pattern of three psoriasis patients based on blood heat and viscous blood, and applied acupuncture and herbal medicine to them. The effect of treatment was evaluated using PASI (psoriasis area and severity index). In all of the three cases, the results of treatment were satisfactory. Thus, oriental medical treatment after differentiation of syndromes, which is highly effective without side effect, is considered to make a great contribution to the treatment of psoriasis in the future.

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PIV를 이용한 선박 프로펠러 후류의 속도장 계측 (PIV Velocity Field Measurements of Flow around a Ship with Rotating Propeller)

  • 이상준;백부근
    • 대한조선학회논문집
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    • 제40권5호
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    • pp.17-25
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    • 2003
  • Velocity field behind a container ship model with a rotating propeller has been investigated using PIV (particle image velocimetry) system. Four hundred instantaneous velocity fields were measured at 4 different blade phases and ensemble-averaged to investigate the spatial evolution of vortical structure of near wake within one propeller diameter downstream. The phase-averaged mean velocity fields show the potential wake and the viscous wake formed due to the boundary layers developed on the blade surfaces. The interaction between bilge vortex developed along the hull surface and the tangential velocity component of incoming flow causes to have asymmetric flow structure in the transverse plane.

모든 속도영역의 점성유동에 적용 가능한 새로운 압력기반 유한요소법 (A New Pressure-Based Finite Element Method Applicable to Viscous Flows at All Speed Ranges)

  • 심은보;장근식
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1995년도 추계 학술대회논문집
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    • pp.169-174
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    • 1995
  • A finite element scheme using the concept of PISO method has been developed to solve the viscous flow problems in all speed range. In this study, new pressure equation is proposed such that both the hyperbolic term related with the density variations and elliptic term reflecting the incompressibility constraint are included. Present method has been applied to incompressible flow in two-dimensional driven cavity(Re=100, 400 and 1,000), and its computed results are compared with other's. Also, Carter plate problem(M=3 and Re=1,000) is computed and the comparison is made with Carter's results. Finally, we simulate a shock-boundary layer interaction problem(M=2 and $Re=2.96{\times}10^5$) to illustrate the shock capturing capability of the present solution algorithm.

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급 출발하는 반원형 실린더에 의한 초기 후류거동의 시뮬레이션 (Simulations of the early wake behavior induced by an impulsively started a semicircualr cylinder)

  • 조지영;이상환;진동식
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.349-352
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    • 2002
  • The time-development of the wake vortices of the unsteady viscous flow past a semicircular cylinder is simulated using the vortex particle methods for direct numerical simulations(DNS). The early wake behaviour of the flow behind an impulsively started a semicircualr cylinder is evaluated for a range of Reynolds numbers between 60 and 200 with opposite body configurations respectively. The diffusion scheme based on the particle strength exchange(PSE) is used to account far the viscous effect accurately. And the vorticity generation algorithm to enforce the no-slip boundary conditions is employed. In order to redistribute particles efficiently on the distorted Lagrangian grid the particle distribution technique is adaptively revised, while maintaining the uniform resolution. The results of the simulations are compared to other experimental results.

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박리유동장에서 저속 익형의 공기역학적 성능해석 (An Aerodynamic Performance Analysis of the Low-Speed Airfoils in Seperated Flow Field)

  • 유능수
    • 산업기술연구
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    • 제15권
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    • pp.153-168
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    • 1995
  • The purpose of this study is to develop a method for predicting the aerodynamic performance of the subsonic airfoils in the 2-dimensional, steady and viscous flow. For this study, the airfoil geometry is specified by adopting the longest chord line system and by considering local surface curvature. In case of the inviscid-incompressible flow, the analysis is accomplished by the linearly varying strength vortex panel method and the Karman-Tsien correction law is applied for the inviscid-compressible flow analysis. The Goradia's integral method and the Truckenbrodt integral method are adopted for the boundary layer analysis of the laminar flow and the turbulent flow respectively. Viscous and inviscid solutions are converged by the Lockheed iterative calculating method using the equivalent airfoil geometry. And the analysis of the seperated flow is performed using the Dvorak and Maskew's method as the basic method. The wake effect is also considered and its geometry expressed by the formula of Summey & Smith when no seperation occurs. A computational efficiency is verified by the comparison of the computational results with experimental data and by the shorter execution time.

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Three-dimensional incompressible viscous solutions based on the unsteady physical curvilinear coordinate system

  • Lee S. H.
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1998년도 춘계 학술대회논문집
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    • pp.43-48
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    • 1998
  • The development of unsteady three-dimensional incompressible viscous solver based on unsteady physical curvilinear coordinate system is presented. A 12-point finite analytic scheme based on local uniform grid spacing is extended for nonuniform grid spacing. The formulation of a condition is suggested to avoid the oscillation of the series summations produced by the application of the method of separation of variables. SIMPLER and pressure Poisson equation techniques are used for solving a velocity-pressure coupled problem. The matrix is solved using the Generalized Minimal RESidual (GMRES) method to enhance the convergence rate of unsteady flow solver and the Kinematic boundary condition of a free surface flow. It is demonstrated that the numerical solutions of these equations are less mesh sensitive.

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