• 한국항공운항학회지
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• 제14권4호
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• pp.1-10
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• 2006

A computational study was carried out in order to investigate the ground effect of a circular cylinder in the presence of a moving wall at a Reynolds number of 2.0${\times}$104. The viscous-incompressible Navier-Stokes equations and Spalart-Allmaras turbulent model of the commercial CFD code were adopted for this numerical analysis. The moving wall was set parallel with the freestream, and the speed of motion was equal to the freestream velocity. The gap ratio is defined as the distance ratio between the circular cylinder diameter and the height from the moving wall. The numerical results show that there are the differences among the each of the stages in evidence of the vorticity contours and the polar diagrams of $C_l$ vs. $C_d$. The 4 stages of the gap ratio are defined according to the flow features, whose stages are divided into small, intermediate, large and convergence gap ratios, respectively.

• 전자공학회논문지B
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• 제33B권2호
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• pp.56-64
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• 1996

In the previous paper of this study, an incoherent intensity pattern of a conducting cylinder is obtained by averaging out the multi-frequency intensities of the time-harmonic fields scattered from this cylinder. in this paper, an incoherent imaging of a conducting cylinder is obtained via the back-projection of the incoherent intensity patterns calculated from the circular rotational measurement configuration. This imaging method is vlaidated by imaging a conducting circular and a conducting elliptic cylinder and the measurement conditions to get better image are investigated.

• 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.

• International Journal of Naval Architecture and Ocean Engineering
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• 제6권3호
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• pp.529-561
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• 2014

The two-phase turbulent flow past an interface-piercing circular cylinder is studied using a high-fidelity orthogonal curvilinear grid solver with a Lagrangian dynamic subgrid-scale model for large-eddy simulation and a coupled level set and volume of fluid method for air-water interface tracking. The simulations cover the sub-critical and critical and post critical regimes of the Reynolds and sub and super-critical Froude numbers in order to investigate the effect of both dimensionless parameters on the flow. Significant changes in flow features near the air-water interface were observed as the Reynolds number was increased from the sub-critical to the critical regime. The interface makes the separation point near the interface much delayed for all Reynolds numbers. The separation region at intermediate depths is remarkably reduced for the critical Reynolds number regime. The deep flow resembles the single-phase turbulent flow past a circular cylinder, but includes the effect of the free-surface and the limited span length for sub-critical Reynolds numbers. At different Froude numbers, the air-water interface exhibits significantly changed structures, including breaking bow waves with splashes and bubbles at high Froude numbers. Instantaneous and mean flow features such as interface structures, vortex shedding, Reynolds stresses, and vorticity transport are also analyzed. The results are compared with reference experimental data available in the literature. The deep flow is also compared with the single-phase turbulent flow past a circular cylinder in the similar ranges of Reynolds numbers. Discussion is provided concerning the limitations of the current simulations and available experimental data along with future research.

• 대한기계학회논문집B
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• 제22권3호
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• pp.346-359
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• 1998

The aerodynamic forces and wake structure of the non-rotating downstream circular cylinder, of which the uniform freestream flow is interfered with another spinning upstream cylinder having the same diameter that is located upstream in a line have been investigated experimentally. When the spin rate of the downstream cylinder defined as the ratio of tangential surface velocity of the spinning cylinder to the freestream velocity increases gradually from zero to 1.4, the change of surface pressure distribution, aerodynamic forces of the non-rotating downstream cylinder were measured in case of several distance ratios of 1.5, 3.0, and 4.5 defined as the ratio of distance between the centers of two cylinders to the diameter. The wake flow patterns behind the cylinder were also investigated in each case. From the present experiments, it has been found that the spin rate significantly influences the aerodynamic forces and near-wake flow phenomena of the downstream cylinder in such a way that the drag increases as the spin rate and distance ratio increase and the wake width increases as the distance ratio increases.

• 대한기계학회논문집B
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• 제39권4호
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• pp.325-333
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• 2015

본 연구에서는 층류 점성유동에서 원형 실린더를 기준으로 홈을 이용한 실린더의 형상변화가 유동 특성에 미치는 영향 분석을 2차원 수치 해석으로 수행하였다. 사용한 좌표계는 직교 좌표계로서 가상경계법과 표시 입자 기법을 사용하여 실린더를 구현하였다. 홈의 개수와 위치를 변수로 Re=40, 50에서 계산하였으며, 홈의 수와 위치에 의한 유동 불안정성을 해석하여 임계 레이놀즈 수를 구하였다.

• 대한기계학회논문집B
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• 제20권8호
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• pp.2601-2610
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• 1996

Surface protrusions have been attached on a cylinder surface to reduce the flow-induced structural vibration by controlling the wake flow. Wind tunnel tests on the near wake of a circular cylinder with surface protrusions were carried out to investigate the flow characteristics of the controlled wake. Three experimental models were used in this experiment; one plain cylinder of diameter D and two cylinders wrapped helically by three small wires of diameter d=0.075D with pitches of 5D and 10D, respectively. Free stream velocity was ranged to have Reynolds number from 5000 to 50,000. Streamwise and vertical velocity components of the wake were measured by a hot-wire anemometry. The spanwise velocity component measured by a one-component fiber optic LDV revealed that time-averaged wake field has a nearly two-dimensional structure. It was found that the surface protrusions elongate the vortex formation region, which decrease the vortex shedding frequency. The suppression of vortices caused by the surface protrusions increases the velocity deficit in the center of wake region.

• 대한기계학회논문집B
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• 제25권7호
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• pp.915-922
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• 2001

A new phase-average technique using instantaneous velocity fields obtained by a PIV method has been developed. The technique tracks vorticity centers and estimates the value of circulation for a chosen domain. The locations of vortex-centers and the magnitudes of circulation are matched together then showing a sine wave feature due to the periodic vortex shedding from the circular cylinder. Ensemble averaged and phase averaged velocity fields are successfully measured for the circular cylinder wake where Reynolds number is 3900 based on free stream velocity and cylinder diameter. The convection velocities of the vortices center and the vortex shedding frequency were measured by a single hot-wire probe.

• 대한기계학회논문집
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• 제9권5호
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• pp.555-563
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• 1985

본 논문에서는 원주(circular cylinder)가 균일속도장에 놓였을 때의 2차원적 인 난류후류유동 특성을 실험에 의해 조사하고, 근접후류에서의 주기적인 대규모 운동 에 의한 코히어런트구조가 하류에서 자체유사(selfpreserving)로 되어 가는 데 있어서 의 난류변동성분에 관한 해석을 위해 확률밀도함수, 자기상관계수, 파워스펙트럼 등과 같은 통계적 처리기법을 도입하고자 한다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2003년도 추계학술대회
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• pp.804-809
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• 2003

In this study, 2D computations of the Aeolian tones for some obstacles (circular cylinder, square cylinder and NACA0012 airfoil) are simulated. First of all, we calculate the flow noise generated by a uniform flow around a two-dimensional circular cylinder at Re=150 are simulated by applying the finite difference lattice Boltzmann method (FDLBM). The third-order-accurate up-wind scheme (UTOPIA) is used for the spatial derivatives, and the second-order-accurate Runge-Kutta scheme is applied for the time marching. The results show that we successively capture very small acoustic pressure fluctuation with the same frequency of the Karman vortex street compared with the pressure fluctuation around a circular cylinder. The propagation velocity of the acoustic waves shows that the points of peak pressure are biased upstream due to the Doppler effect in the uniform flow. For the downstream, on the other hand, it is faster. To investigate the effect of the lattice dependence, furthermore, simulations of the Aeolian tones at the low Reynolds number radiated by a square cylinder and a NACA0012 airfoil with a blunt trailing edge at high incidence are also investigated.