• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.307-310
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• 2002

A two-dimensional numerical method for inviscid two-fluid flows with evolution of density interface is developed, and an initially stationary two-dimensional fluid sheet surrounded by another fluid is studied. The Interface between two fluids is modeled as a vertex sheet, and the flow field u÷th the evolution of interface is solved by using vortex-in-cell/front-tracking method. The edge of the sheet Is pulled back into the sheet due to surface tension and a blob is formed at the edge. This blob and fluid sheet are connected by a thin neck. In the inviscid limit, such process of the blob and neck formation is examined in detail and their kinematic characteristics are summarized with dimensionless parameters. The edge recedes at $V=1.06({\sigma}/{\rho}h)^{0.5}$ and the capillary wave Propagating into the fluid sheet must be considered for bettor understanding of the edge receding.

• 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.

• 대한조선학회지
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• 제27권4호
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• pp.27-31
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• 1990

양력면(揚力面)의 양력계산(揚力計算)에 흔히 쓰이고 있는 방법(方法)을 크게 나누면 Vortex Lattice 법(法)과 Mode Function법(法)이 있다. 잘 알려진 것 처럼, Vortex Lattice법(法)은 해(解)의 수렴성(收斂性)은 좋으나 계산시간(計算時間)이 많이 걸리는 문제점(問題點)이 있고, Mode Function법(法)은 계산시간(計算時間)은 짧으나 해(解)가 특이(特異)해 지는 경우가 있다. 그러므로 본(本) 논문(論文)에서는 양방법(兩方法)의 장점(長點)들을 살리도록, 양력면(揚力面)을 Span 방향(方向)으로 분할(分割)하고 각(各) Strip Mode Function을 사용하여 Vortex를 분포(分布)시켜, 양력면이론(揚力面理論)으로 양력(揚力)을 계산(計算)하였다. 우선 Horn Type의 반균형타(半均衡舵)에 본(本) 계산법(計算法)을 적용(適用)하여 타직압력(舵直壓力)을 계산(計算)하고 타(舵) 단독시험(單獨試驗)을 병행(竝行)하여 계산법(計算法)의 유용성(有用性)을 검증(檢證)하였다. 그 결과(結果), Stall과 같은 비선형적(非線形的) 유체현상(流體現象)이 일어나지 않는 한(限), 본(本) 계산법(計算法)은 유용(有用)하다는 결론(結論)을 얻었다. 끝으로, 본(本) 계산법(計算法)을 평행(平行)하게 늘어선 한척(隻)의 장방형타(長方形舵)에 적용(適用)하여 두 타(舵) 사이의 상호간섭(相互干涉)도 계산(計算)하였다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.1466-1471
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• 2004

In this paper, we report the numerical and experimental solutions of the axi-symmetric flows in the axial plane driven by an impingement of fluid from the bottom wall of a circular cylinder. We managed to visualize successfully the flow pattern shown on the vertical plane through the container axis. The numerical results are not show to compare well with the experimental results for the case of the Rossby number 3. Because the numerical results calculate on the assumption that vortex flows are axi-symmetric flow on the other hand real experimental results are show asymmetric flow. The numerical solutions reveal that inertial oscillation plays an important role at small Rossby numbers, or at a larger background rotation.

• International Journal of Fluid Machinery and Systems
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• 제2권4호
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• pp.418-425
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• 2009

A vertical bulb turbine unit with elbow type draft tube has been developed due to avoidance of complicated assembling and long standstill period at overhaul in comparison with conventional horizontal bulb turbine unit. Before designing the prototype vertical bulb unit, a hydrographic model test was carried out to establish the ideal design concept for this innovative generating unit. Froude similarity is not available for vortex occurrence. Consequently, an intake structure without air entraining vortices under all the flow conditions is developed, and it is confirmed that the surge wave at load rejection is not affected harmful influence for other constructions.

• Wind and Structures
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• 제9권2호
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• pp.109-124
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• 2006

This paper describes the characteristics of the fluctuating lift forces when a circular cylinder vibrates in the cross-flow direction. The response characteristics on elastically supported the circular cylinder was first examined by a free-vibration test. Next, flow-induced vibrations obtained by the free-vibration test were reproduced by a forced-vibration test, and then the characteristics of the fluctuating lift forces, the work done by the fluctuating lift, the behavior of the rolling-up of the separated shear layers were investigated on the basis of the visualized flow patterns. The main findings were that (i) the fluctuating lift forces become considerably large than those of a stationary circular cylinder, (ii) negative pressure generates on the surface of the circular cylinder when the rolling-up of separated shear layer begins, (iii) the phase between the fluctuating lift force and the cylinder displacement changes abruptly as the reduced velocity $U_r$ increases, and (iv) whether the generating cross-flow vibration becomes divergent or convergent can be described based on the work done by the fluctuating lift force. Furthermore, it was found that the generation of cross-flow vibration can be perfectly suppressed when the small tripping rods are installed on the surface of the circular cylinder.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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• pp.263-270
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• 1997

For a cylinder in a uniform flow stream, sound is generated by the fluctuating pressure on the cylinder surface due to the vortex shedding behind the cylinder. It is known that the major parameters to predict the sound pressure are the characteristic length of the flow along the cylinder axis and the fluctuating lift coefficient. These parameters strongly depend on the Reynolds number and the yaw angle of the cylinder to the free stream. In this experimental study the effects of yaw on the flow parameters, and consequently on the generated sound are investigated. The surface pressure and the radiated sound are measured simultaneously for different yaw angles and showed that the reduced normal velocity component to the cylinder axis reduces the unsteady lift fluctuation which results in lowered sound press-are level, However, experimental result shows that "the cosine law" which uses the normal velocity component as a characteristic velocity for noise Generation from a yawed cylinder needs to be carefully reviewed. reviewed.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년도 춘계학술대회논문집
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• pp.568-571
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• 2008

The computation of moving interface by the level set method typically requires reinitializations of level set function. An inaccurate estimation of level set function ${\phi}$ results in incorrect free-surface capturing and thus errors such as mass gain/loss. Therefore, accurate and robust reinitialization process is essential to the free-surface flows. In the present paper, we pursue further development of the reinitialization process, which evaluates directly level set function ${\phi}$ using a normal vector in the interface without solving the re-distancing equation of hyperbolic type. The Taylor-Galerkin approximation and P1P1splitting FEM are adopted to discretize advection equation of the level set function and the Navier-Stokes equation, respectively. Advection equation of free surface and re-initialization process are validated with benchmark problems, i.e., a broken dam flow and time-reversed single vortex flow. The simulation results are in good agreement with the existing results.

• 대한기계학회논문집B
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• 제32권10호
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• pp.754-760
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• 2008

Computation of moving interface by the level set method typically requires the reinitialization of level set function. An inaccurate estimation of level set function $\phi$ results in incorrect free-surface capturing and thus errors such as mass gain/loss. Therefore, an accurate and robust reinitialization process is essential to the simulation of free-surface flows. In the present paper, we pursue further development of the reinitialization process, which evaluates level set function directly using a normal vector on the interface without solving there-distancing equation of hyperbolic type. The Taylor-Galerkin approximation and P1P1 splitting/SUPG (Streamline Upwind Petrov-Galerkin) FEM are adopted to discretize advection equation of the level set function and the incompressible Navier-Stokes equation, respectively. Advection equation and re-initialization process of free surface capturing are validated with benchmark problems, i.e., a broken dam flow and timereversed single vortex flow. The simulation results are in good agreement with the existing results.

• 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.