• 제목/요약/키워드: boundary vortex potential

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와류입자법에 의한 비정상 박리흐름의 전산(I) -경계요소법과 정방형 실린더 주위의 와류강도- (Computation of Unsteady Separated Flow Using the Vortex Particle Method (I) - Boundary Element Method and Vortex Strength Around the Square Cylinder -)

  • 박외철
    • 한국안전학회지
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    • 제13권4호
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    • pp.3-8
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    • 1998
  • The vortex particle method, which includes viscous effects, consists of diffusion of boundary vorticity and creation of the vortex particles, convection, particle strength exchange, and particle redistribution. Accuracy of the boundary element method is very important since it creates the particles around the body at every time step. A boundary element method based on source panel was investigated as part of computation of unsteady separated flows by rising the vortex particle method. The potential flows were computed around a circular cylinder and a square cylinder. The results around the circular cylinder were compared with the exact solution, and the distribution of vorticity, in particular near the sharp comers of the square cylinder, is scrutinized for different number of panels.

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Oscillatory Josephson-Vortex Resistance in Stacks of $Bi_{2}Sr_{2}CaCu_{2}O_{8+x}$ Intrinsic Josephson Junctions

  • 최재현;배명호;이후종;김상제
    • Progress in Superconductivity
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    • 제7권1호
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    • pp.17-21
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    • 2005
  • We report the oscillation of the Josephson vortex-flow resistance in the rectangular stacks of $Bi_{2}Sr_{2}CaCu_{2}O_{8+x}$(Bi-2212) intrinsic Josephson junctions (IJJs). Apiece of Bi-2212 single crystal containing a few tens of IJJs was sandwiched between two gold electrodes and fabricated into a rectangular shape with the typical lateral size of about $1.5{\times}10\;{\mu}m^2$, using e-beam lithography and focused ion-beam etching techniques. In a tesla-range magnetic field applied in parallel with the junction planes, the oscillation of the Josephson vortex flow resistance was observed at temperatures near 60 K. The oscillation results from the interplay between the triangular Josephson vortex lattice and the potential barrier at the boundary of a single crystal. The oscillatory magnetoresistance for different bias currents, external magnetic fields, and the tilt-angles provides useful information on the dynamics of the coupled Josephson-vortex lattice system.

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Predicted Air Flow Around Objects Using the Discrete Vortex Method

  • Kim, Tae-Hyeung
    • Journal of Korean Society for Atmospheric Environment
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    • 제9권E호
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    • pp.347-357
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    • 1993
  • The Lagrangian grid-free numerical method, the discrete vortex method, was applied to solve the Navier-Stokes euqations. This method avoids the introduction of numerical viscosity swamping the real physical viscosity at high Reynolds number, unlike Eulerian method, e.g. finite difference and element methods. The boundary integral equation method for the potential flow solution was included to make the discrete vortex method more feasible for complex geometries. The fast adaptive multipole expansion method was incorporated to reduce the computational time from $O(N^2)$ to O(N) for the computations of vortex-vortex interactions. The test problems were air flow around one circular cylinder and two circular cylinders in tandem with various gaps. The numerical results were in excellent gareement with the experimental and other computational results. The applicabilty of the method was discussed with the indoor and the outdoor air pollution problems, especially the contaminant transport in the recirculation regions.

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B-Spline 고차 경계요소법을 이용한 3차원 수중익의 날개 끝 와류유동 수치해석 (Numerical Analysis of Tip Vortex Flow of Three-dimensional Hydrofoil using B-Spline Higher-order Boundary Element Method)

  • 김지혜;안병권;김건도;이창섭
    • 한국해양공학회지
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    • 제31권3호
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    • pp.189-195
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    • 2017
  • A three-dimensional higher order boundary element method based on the B-spline is presented. The method accurately models piecewise continuous bodies and induced velocity potentials using B-spline tensor product representations, and it is capable of obtaining accurate pointwise values for the potential and its derivatives, especially in the trailing edge and tip region of the lift generating body, which may be difficult or impossible to evaluate with constant panel methods. In addition, we implement a wake roll-up and examine the tip vortex formation in the near wake region. The results are compared with existing numerical results and the results of experiments performed out at the cavitation tunnel of Chungnam National University.

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.

A Numerical Study on the Bubble Noise and the Tip Vortex Cavitation Inception

  • Park, Jin-Keun;Georges L. Chahine
    • Journal of Ship and Ocean Technology
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    • 제7권3호
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    • pp.13-33
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    • 2003
  • This paper presents a numerical study on tip vortex cavitation inception predictions based on non-spherical bubble dynamics including splitting and jet noise emission. A brief summary of the numerical method and its validation against a laboratory experiment are presented. The behavior of bubble nuclei is studied in a tip vortex flow field at two Reynolds numbers, provided by a viscous flow solver. The bubble behavior is simulated by an axisymmetric potential flow solver with the effect of surrounding viscous flow taken into account using one way coupling. The effects of bubble nucleus size and Reynolds number are studied. An effort to model the bubble splitting at lower cavitation numbers is also described.

선미부에 유동제어판을 부착한 선박에 대한 포텐셜 유동해석 (Potential Flow Analysis for a Ship with a Flow Control Plate near the Stern)

  • 최희종;전호환;윤현식;이인원;박동우;김동진
    • 대한조선학회논문집
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    • 제46권6호
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    • pp.587-594
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    • 2009
  • In the paper the effect of a stern-plate attached to a ship was taken into account. The relationship between the trim angle of a ship and the wave-resistance coefficient induced by the a stern-plate was studied using the potential flow analysis method. Numerical algorithm was described using the panel method and the vortex lattice method(VLM) to simulate the flow phenomena around a ship. The non-linearity of the free surface boundary conditions were considered using the iterative method and the IGE-GMRES(Incomplete Gaussian Elimination-The Generalized Minimal RESidual) algorithm was adopted to solve the linear equation at each iterative step. Numerical calculations were carried out to investigate the validity of the adopted algorithm using KCS(KRISO 3600 TEU Container) hull. Possible cases for attachment of the plate were checked. The results showed that the numerical algorithm could be physically appropriate.

고차 스펙트럴 / 경계적분법에 의한 수중익과 자유표면의 비선형 상호작용 계산 (Calculation of Nonlinear Interactions between Hydrofoil and Free-Surface by the High-Order Spectral/Boundary-Integral Method)

  • 김용직;하영록
    • 수산해양기술연구
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    • 제39권1호
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    • pp.27-32
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    • 2003
  • 본 논문에서는 수중익주위의 비선형/비정상 자유표면 유동을 다룰 수 있는 시간영역 수치해법으로 고차 스펙트럴법과 경계적분법을 조합한 고차 스펙트럴/경계적분법을 이용하였다. 이 수치해법은 자유표면 요소수를 N이라 할 때 그 산술 계산량이 NlogN에 비례하여 증가하므로 N 이 클 때는 거의 선형적으로 증가한다. 따라서, 이 수치해법은 자유표면 유통의 계산에 있어 매우 효율적인 방법이다. 적용예로서 균속전진하는 수중익에 의한 발생파형 계산결과를 Duncan/sup 3)/의 실험결과와 비교하였고 대체로 좋은 일치를 보이고 있다. 또한, 전진하며 상하동요하는 수중익에 의한 발생파형과 양력, 후류 보오텍스 둥을 시간영역에서 시뮬레이션하여 본 방법이 수중익주위 자유표면 유동의 다양한 문제들에 적용될 수 있는 강력한 수단임을 보였다.

Streamline Tracing of Marine Propeller Blade -A Formulation of an Indirect Problem-

  • Hun-Chol,Kim
    • 대한조선학회지
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    • 제12권1호
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    • pp.77-82
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    • 1975
  • An analytical formulation of obtaining propeller sections for a given vortex system of radial and chordwise distribution is given as an indirect problem of tracing the propeller surface. The formulation satisfies the boundary condition of potential flow exactly rather than previous approximate use of induced streamline curvatures at the zero camber line.

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