• 대한기계학회논문집B
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• 제28권7호
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• pp.809-817
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• 2004

In this paper, the unsteady behavior of the viscous flow field past an impulsively started elliptic cylinder is studied numerically. In order to analyze flow field, we introduce vortex particle method. The vorticity transport equation is solved by fractional step algorithm which splits into convection term and diffusion term. The convection term is calculated with Biot-Savart law, the no-through boundary condition is employed on solid boundaries. The diffusion term is modified based on the scheme of particle strength exchange. The particle redistributed scheme for general geometry is adapted. The flows around an elliptic cylinder are investigated for various attack angles at Reynolds number 200. The comparison between numerical results of present study and experimental data shows good agreements.

• 대한조선학회논문집
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• 제41권1호
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• pp.23-30
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• 2004

In the Lagrangian vortex particle method based on the vorticity-velocity formulation for solving the incompressible Navier-Stokes equations, a numerical scheme for calculating pressure fields is presented. Implementation of the numerical method is directly connected with the well-established surface panel methods, just by dealing with the dynamic coupling among vorticity field. Assuming the vorticity and the velocity fields are to be calculated in time domain analysis, the pressure calculation for a complete set of solution at present time step is performed in a similar way to the one used in the Eulerian description. For a validation of the present method, we illustrate the early development of the viscous flow about an impulsive started circular cylinder for Reynolds number 550. The comparative study with the Eulerian finite Volume method provides an extensive understanding and application of the mesh-free Lagrangian vortex methods for numerical simulation of viscous flows around arbitrary bodies of general shape.

• 대기
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• 제30권4호
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• pp.347-360
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• 2020

The automatic algorithm optimized for the Korean Peninsula was developed to detect and track the center of typhoon based on a geometrical method using high-resolution retrieved WISSDOM (WInd Syntheses System using DOppler Measurements) wind and reflectivity data. This algorithm analyzes the center of typhoon by detecting the geometric circular structure of the typhoon's eye in radar reflectivity and vorticity 2D field data. For optimizing the algorithm, the main factors of the algorithm were selected and the optimal thresholds were determined through sensitivity experiments for each factor. The center of typhoon was detected for 5 typhoon cases that approached or landed on Korean Peninsula. The performance was verified by comparing and analyzing from the best track of Korea Meteorological Administration (KMA). The detection rate for vorticity use was 15% higher on average than that for reflectivity use. The detection rate for vorticity use was up to 90% for DIANMU case in 2010. The difference between the detected locations and best tracks of KMA was 0.2° on average when using reflectivity and vorticity. After the optimization, the detection rate was improved overall, especially the detection rate more increased when using reflectivity than using vorticity. And the difference of location was reduced to 0.18° on average, increasing the accuracy.

• 대한기계학회논문집B
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• 제27권9호
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• pp.1262-1272
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• 2003

A two-dimensional direct numerical simulation is performed to investigate the dynamic behaviors of a single vortex in counter reacting and non-reacting flow field. A predictor-corrector-type numerical scheme with a low Mach number approximation is used in this simulation. A 16-step augmented reduced mechanism is adopted to treat the chemical reaction. The budget of the vorticity transport equation is examined to reveal a mechanism leading to the formation, destruction and transport of a single vortex according to the direction of vortex generation in reacting and non-reacting flows. The results show that air-side vortex has more larger strength than that of fuel-side vortex in both non-reacting and reacting flows. In reacting flow, the vortex is more dissipated than that in non-reacting flow as the vortex approach the flame. The total circulation in reacting flow, however, is larger than that in non-reacting flow because the convection transport of vorticity becomes much large by the increased velocity near the flame region. It is also found that the stretching and the convection terms mainly generate vorticity in non-reacting and reacting flows. The baroclinic torque term generates vorticity, while the viscous and the volumetric expansion terms attenuate vorticity in reacting flow. Furthermore, the contribution of volumetric expansion term on total circulation for air-side vortex is much larger than that of fuel-side vortex. It is also estimated that the difference of total circulation near stagnation plane according to the direction of vortex generation mainly attributes to the convection term.

• Journal of Astronomy and Space Sciences
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• 제25권4호
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• pp.405-414
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• 2008

이 연구에서는 고위도 하부 열권 역학을 좌우하는 물리적 과정을 이해하기 위하여, 상이한 행성간 자기장(Interplanetary Magnetic Field, IMF)에 따른 남반구 고위도 하부 열권에서의 소용돌이도(vorticity)와 발산(divergence)을 분석하였다. 이 연구를 위하여 미국립대기연구소(National Center for Atmospheric Research, NCAR)의 열권-이온권 전기역학적 대순환 모델(Thermo sphere-Ionosphere Electrodynamic General Circulation Model, TIEGCM)을 이용하였다. 소용돌이도와 발산 분석은 전체 수평 바람장을 최종적으로 결정하는 운동량원(momentum source)을 밝히는데 도움을 주는 근원적인 흐름을 파악할 수 있게 해주며, 운동량원들의 상대적인 강도를 분석해내는데 좋은 도구가 된다. 고위도 하부 열권의 평균 바람장은 태양 복사와 쥴가열에 의해 유발되는 발산운동 보다는 이온대류에 의해 유발되는 회전운동에 의해 주로 지배된다는 것이 확인되었다. $IMF{\neq}0$와 IMF=0인 경우의 고위도 열권 하부에서의 소용돌이도 차이(difference vorticity)가 모든 IMF 조건에서 발산장 차이(difference divergence)에 비해 훨씬 더 크게 나타났다. 이는 IMF가 발산적인 흐름보다 회전적인 흐름에 더 강하게 영향을 끼치며, 나아가 IMF가 발산운동을 유발하는 에너지 유입보다는 회전운동을 유발하는 운동량 유입에 더 강하게 영향을 끼침을 의미한다. IMF의 방향에 따라 고위도 하부 열권에서의 소용돌이도 차이의 양상이 매우 달랐다 $B_y$가 음일 때는 지자기 위도 $-70^{\circ}$ 이상의 고위도에서 극을 중심으로 양의 소용돌이도 차이가 나타나고 $B_y$가 양일 때는 음의 소용돌이도 차이가 나타났다. $B_z$가 음인 경우 소용돌이도 차이가 저녁 영역에는 양이고 새벽 영역에는 음이며, $B_z$가 양인 경우에는 반대의 분포를 보였다. $B_z$가 음일 때가 양일 때보다 소용돌이도 차이가 더 큰 것으로 확인되었는데, 이는 IMF $B_z$가 남쪽으로 향할 때가 북쪽으로 향할 때보다 고위도 이온권의 이온대류를 더 강화시켜 열권 중성대기의 회전적인 흐름을 더 강하게 유발시킴을 의미한다.

• 대한토목학회논문집
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• 제36권6호
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• pp.1037-1048
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• 2016

본 연구에서는 Navier-Stokes 방정식과 자유수면 추적에 VOF법을 채용하는 CADMAS-SURF를 이용하여 파랑과 흐름의 비선형 상호간섭현상을 연구하였다. 파-흐름 공존장에서의 유체거동 해석을 위해 CADMAS-SURF를 수정 및 확장하였고, 계산치를 실험치와 비교하여 본 연구의 타당성을 확인할 수 있었다. 본 연구의 수치수로를 파랑-흐름 공존장에서 주어지는 복잡한 물리 현상 규명과 파-흐름-잠제의 상호간섭해석에 적용하여, 유속장, 와도장, 자유수면과 와도와의 관계 등을 논의하였다.

• 한국가시화정보학회지
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• 제3권2호
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• pp.45-50
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• 2005

Electro-osmotic flow (EOF) instability in a microchannel has been experimentally investigated using a micro-PIV system. The micro-PIV system consisting of a two-head Nd:Yag laser and cooled CCD camera was used to measure instantaneous velocity fields and vorticity contours of the EOF instability in a T-shape glass microchannel. The electrokinetic flow instability occurs in the presence of electric conductivity gradients. Charge accumulation at the interface of conductivity gradients leads to electric body forces, driving the coupled flow and electric field into an unstable dynamics. The threshold electric field above which the flow becomes unstable and rapid mixing occurs is about 1000V/cm. As the electric field increases, the flow pattern becomes unstable and vortical motion is enhanced. This kind of instability is a key factor limiting the robust performance of complex electrokinetic bio-analytical devices, but can also be used for rapid mixing and effective flow control fer micro-scale bio-chips.

• 소음진동
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• 제7권2호
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• pp.215-222
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• 1997

The flow and acoustic fields due to a vortex ring interaction with a rigid sphere are simulated numerically. The flow field is regarded as three-dimensional inviscid and incompressible. The vorticity is assumed to be concentrated inside the finite core of vortex filament. The vortex filament curve, described by parabolic blending curve function, is used to effectively solve the modified Biot-Savart equation. The interaction between a vortex ring and a rigid sphere using the parabolic blending curve is calculated. The trajectory of the vortex ring is obtained with several different initial positions between the ring and the sphere. The force variations acting on the sphere are calculated by using the boundary integral method. Finally, we can also obtain the acoustic signals at the far field observation positions from the force variations acting on the rigid surface. We can find that the dipole axis of the directivity patterns are rotated during the interacting phenomena.

• 충청수학회지
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• 제27권4호
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• pp.635-641
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• 2014

The existence and the regularity of the particle trajectory flow X(x, t) along a velocity field u on $\mathbb{R}^n$ are discussed under the BMO-blow-up condition: $${\int}_{0}^{T}{\parallel}{\omega}({\tau}){\parallel}_{BMO}d{\tau}<{\infty}$$ of the vorticity ${\omega}{\equiv}{\nabla}{\times}u$. A comment on our result related with the mystery of turbulence is presented.

• 한국연소학회:학술대회논문집
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• 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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• pp.185-193
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• 2003

Basic flow fields of two dimensional V flames were examined as a preliminary work to study the instability of premixed flame with vorticity generation. Laminar premixed propane and methane flame were anchored by electrically heated wire to make two dimensional V flames. Flow fields were measured mainly by PIV(Particle Image Velocimetray) and the results were compared with those obtained by LDV(Laser Doppler Velocimetry) to confirm their reliability. Because the curvatures of V flames are so small, V flames were locally assumed to be inclined planar flames in gravitational field. The measured flow fields were locally compared with those of analytical solutions, which showed the qualitatively similar results. In downstream region, the vorticity fields were nearly constant except region near the center line, which support the assumption of locally one dimensional flame. Besides it was tried to find experimentally the similarity of flow fields in downstream region. Finally, stability diagram of propane and methane flames were drawn for the equivalence ratio less than one and the wide range of mean velocity.