• 대한기계학회논문집B
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• 제22권5호
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• pp.573-583
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• 1998

Effects of the oscillating incoming flow on vortex shedding and lock-on behind a square cylinder are investigated using numerical simulations at a Reynolds number of 100. Vortex shedding occurred at low forcing frequencies of the incoming flow similar to the natural vortex shedding. As the forcing frequency further increases, the shedding frequency decreases to the half of the forcing freqnency. For a sufficiently large frequency, vortex shedding returns to the natural vortex shedding irrespective of the forcing amplitude. Also, the lock-on region becomes wider with higher forcing amplitudes. The phase diagram between the drag and lift shows a simple periodic behavior in the lock-on region, while a complicated periodic phase relation is observed when there is no lock-on.

• 한국전산유체공학회지
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• 제7권1호
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• pp.1-9
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• 2002

In this paper, a modification of PISO algorithm based on standard k-ε turbulence model was proposed. The numerical technique used in this research is finite volume method, hybrid scheme for discretizing convection term, Euler implicit scheme for discretizing time term, and non-staggered grid. The basic idea of the modification of PISO algorithm is to perform an additional corrector stage for turbulence kinetic energy and dissipation rate to correct the inconsistence of flow and turbulence. In order to validate this algorithm, simulation of flow around a square cylinder (Re=3000) was performed in two-dimensional case. The results obtained from the proposed scheme show better agreement with those from the experiment than using original PISO algorithm in coherent velocity field.

• 한국전산유체공학회지
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• 제20권3호
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• pp.47-53
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• 2015

This study performed numerical simulation to elucidate the characteristics of flow past a rectangular cylinder with various values of the aspect ratio(AR) of the cylinder. We calculated the flow field, force coefficients and Strouhal number of vortex shedding depending on the Reynolds number(Re) and the aspect ratio. The $AR{\approx}1$ is preferred for drag reduction, and 0.375$AR{\approx}0$ is recommended if suppression of the lift-coefficient fluctuation and the shedding frequency is desirable. Furthermore the criticality of the Hopf bifurcation is also reported for each AR.

• 한국방송∙미디어공학회:학술대회논문집
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• 한국방송공학회 2013년도 하계학술대회
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• pp.40-42
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• 2013

본 논문에서는 사각 평면이 아닌 실린더나 구 형태의 비평면 스크린에 고품질 파노라마 영상을 렌더링 하기 위해 스틸 카메라를 이용한 자동 캘리브레이션과 멀티 프로젝터를 이용한 파노라마 렌더링 시스템을 제안한다. 스틸 카메라를 이용한 비평면 스크린 캘리브레이션은 특정 패턴을 스크린에 투사하고 이를 촬영하여 프로젝터의 투사 왜곡을 보정하고 멀티 프로젝터간의 중첩 영역에 대한 보정을 자동 수행한다. 캘리브레이션이 완료된 이후에 멀티 프로젝터를 이용하여 고품질의 파노라마 비디오를 렌더링 하기 위해서 본 논문에서는 복수의 멀티 시스템과 동기화 카드를 이용하여 렌더링 시스템간의 재생 동기화를 수행 하였다. 제안하는 렌더링 시스템을 적용하면 기존의 전문가의 수동작업에 의한 인력 및 보정 시간을 줄일 수 있으며, 시스템 환경이 변하더라도 쉽게 적응적으로 렌더링 환경을 구축하는 것이 가능하고 고품질의 파노라마 비디오를 렌더링 하는 것이 가능하다.

• 설비공학논문집
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• 제30권2호
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• pp.58-67
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• 2018

This study investigated the effect of variation in the angle of the elliptic cylinder as well as the presence of circular cylinder on natural convection inside a square enclosure. The Rayleigh number was varied between $10^3$ and $10^6$, and the Prandtl number was fixed to 0.7. In the present study, the angle of the elliptic cylinder was changed from $0^{\circ}$ to $90^{\circ}$, and the perimeter of the elliptic cylinder was same as that of the circular cylinder. The immersed boundary method was used to capture the virtual wall boundary of the inner cylinder. With the increasing angle of the elliptic cylinder, the surface-averaged Nusselt numbers on the cylinder and the enclosure increased. In the Rayleigh number range considered in the present study, the surface-averaged Nusselt number on the elliptic cylinder over = $45^{\circ}$ was higher than that of the circular cylinder. The effect of elliptic cylinder's angle on natural convection in the enclosure was analyzed according to the flow and thermal fields, and the distributions of the Nusselt number.

• 대한기계학회논문집B
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• 제40권11호
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• pp.717-726
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• 2016

본 연구는 밀폐계 내부에 고온의 원형 실린더가 존재할 때, 밀폐계의 종횡비 변화에 따른 밀폐계 내부의 3차원 자연대류 현상에 대해 수치해석을 수행하였다. 밀폐계 내부의 원형 실린더는 유한체적법(FVM)에 기초한 가상 경계법(IBM)을 사용하여 구현하였다. 본 연구에서 고려한 Rayleigh 수의 범위는 $10^5{\leq}Ra{\leq}10^6$이며, Prandtl 수는 0.7이다. 밀폐계의 폭을 변화하여 밀폐계의 종횡비를 증가시켰으며, 밀폐계의 종횡비는 $1{\leq}W/L{\leq}4$ 범위에서 1 간격으로 고려하였다. 본 연구에서 고려한 모든 Rayleigh 수와 밀폐계의 종횡비 범위에서 열유동장은 x=0 단면을 기준으로 좌우 대칭을 이루며 정상상태에 도달하였다. 또한 밀폐계의 종횡비가 증가할수록 원형 실린더의 표면 평균 Nusselt수는 증가하는 반면, 밀폐계 벽면의 표면 평균 Nusselt수는 감소하였다.

• 한국가스학회지
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• 제17권1호
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• pp.26-34
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• 2013

상 변화(phase change)를 수반한 다상 유동 연구(multiphase flow analysis)는 증발, 응축과 같은 많은 분야에 적용, 응용될 수 있고 현상의 복잡성 때문에 많은 연구의 관심을 받고 있는 분야이다. 본 연구에서는 극저온 유체인 액화질소가 다양한 밀도의 글라스 울 내부 다공성 매질속으로 스며들면서 나타나는 거동을 살펴보았다. 유동에 영향을 미치는 투과성 계수에 대해서, 외부 압력의 영향성에 대한 실험을 진행하였고 논의하였다. 극저온 유체인 액화질소를 실험유체로 사용하여 사각 기둥 실린더 내부의 유체의 유동에 대한 실험으로 유체의 유동을 살펴보았다. 그 결과 벌크 밀도가 커짐에 따라 투과성 계수가 작아지고, 거리에 따른 압력변화의 비선형성이 커짐을 보였다. 마지막으로 CFD 전산유동 프로그램으로 실험결과와 동일한 상황을 모사하였으며, 이를 실험결과와 비교 분석하였다. 이에 대한 검증결과, 시뮬레이션 결과가 실험결과와 유사한 경향과 결과를 보여주었다.

• Journal of Advanced Marine Engineering and Technology
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• 제25권5호
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• pp.1076-1085
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• 2001

Experimental investigations of the longitudinal vortices, which are produced by wing type vortex generators set up behind a circular cylinder in a rectangular channel, are presented. When the circular cylinder is set up in the rectangular channel, a horseshoe vortex is formed just upsteam of the circular cylinder. It generates a turbulent wake region behind the circular cylinder. Therefore, the region of the pressure loss behind the circular cylinder in increased and the size of the wake is small. These problems can be achieved by longitudinal vortices which are generated by wing-type vortex generator. In order to control the strength of longitudinal vortices, the angle of attack of the vortex generators is varied from 20 degree to 45, but the spacing between the vortex generators is fixed 6cm. The 3-dimensional mean velocity measurements are made using a five-hole probe. The vorticity field and streamwise velocity contour are obtained from the velocity field. The following results are obtained. Circulation strength is the maximum value when the angle of attack($\beta$) is $30^{\circ}$, and the vorticity field and streamwise velocity contour in case of $\beta$=$20^{\circ}$ show the trend similar to these in case of $\beta$=$30^{\circ}$, but do not in case of $\beta$=$45^{\circ}$.

• 대한기계학회논문집B
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• 제25권11호
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• pp.1527-1534
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• 2001

Phase averaged velocity fields in the near wake region behind a square cylinder have been (successfully) obtained using randomly sampled PIV data sets. The Reynolds number based on the flow velocity and the vertex height was 3,900. To identify the phase information, we examined the magnitude of circulation and the center of peak vorticity. The center of vorticity was estimated from lowpass filtered vorticity contours (LES decomposition) adopting a sub-pixel searching algirithm. Due to the sinusoidal nature of firculation which is closely related to the instantaneous vorticity, the location of peak voticity fits well with a sine curve of the circulation magnitude. Conditionally-averaged velocity fields represent the barman vortex shedding phenomenon very well within 5 degrees phase uncertainty. The oscillating nature of the separated shear layer and the separation bubble at the top surface are clearly observed. With the hot-wire measurements of Strouhal frequency, we found thats the convection velocity changes its magnitude very rapidly from 25 to 75 percent of the free stream velocity along the streamwise direction when the flow passes by the recirculation region.

• 한국소음진동공학회논문집
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• 제24권12호
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• pp.962-968
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• 2014

The lattice Boltzmann method(LBM) has attracted attention as an alternative numerical algorithm for solving fluid mechanics since the end of the 90's. In these days, its intrinsic unsteadiness and rapid increase in computing power make the LBM be more applicable for computing flow-induced noise as well as fluid dynamics. The lattice Boltzmann method is a weakly compressible scheme, so we can get information about both aerodynamics and aeroacoustics from single simulation. In this paper, numerical analysis on Aeolian tone noise generated by tandem-twin square cylinders in duct is performed using the LBM. For simplicity, laminar two-dimensional fluid models are used. To verify the validity and accuracy of the current numerical techniques, numerical results for the laminar duct and the cylinder flows are compared with the analytical solution and the measurement, respectively. Then, aerodynamic noise of the twin tandem square cylinders is investigated. It is shown that the aerodynamic noise from the twin tandem square cylinders can be reduced by controlling the distance between the cylinders.