• 대한조선학회논문집
• /
• 제30권2호
• /
• pp.76-85
• /
• 1993

자유표면과 수면하 vortex 유동과의 상호작용으로 생기는 수면위의 특이 형상을 실험과 수치해석으로 얻어진 결과에 근거하여 논하였다. 먼저 2차원적인 실험이나 해석적인 연구로 이해될 수 있는 "striation"의 발생을 살펴 본다. "Scar"라 불리우는 striation과 수직한 형상은 2차원 vortex filament와 vortex pair 생성시 생겨나는 residual vortex의 상호작용으로 설명하였다. 간단하면서도 중요한 상호작용의 역학을 연구할 목적으로 vortex ring이 자유표면과 수직하게 충돌할 경우에 나타나는 현상들을 실험적으로 논하였고 이때 상호작용의 초기단계를 축대칭 문제로 하여 수치해석적으로 얻어진 결과와 비교하였다. 상호작용의 후기단계는 vortex reconnection을 포함하는 복잡한 과정인데 이때 수면에서의 짧은파 생성을 vortex ring의 수면과의 경사진 충돌로 설명하였다. 또한 위의 수면과 생성을 간단한 해석적 model로 재구성하여 비교해 보았다. 끝으로 수면위에 존재하는 오염물질이 수면하 vortex 유동에 미치는 영향을 수치해석적인 방법으로 free slip및 rigid wall 조건의 경우와 비교하여 살펴보았다.

• 한국수자원학회:학술대회논문집
• /
• 한국수자원학회 2005년도 학술발표회(2)
• /
• pp.951-951
• /
• 2005

The characteristics of Boussinesq starting forced plumes were investigated in this study. Two distinct periods in the transient plume penetration were identified, namely the Period of Flow Development (PFD) and Period of Developed Flow (PDF). PFD refers to the time period whereby the penetration rate is governed by the complex vortex dynamics initiated by the exit conditions that can include vortex coalescence, vortex leapfrogging, pinching off of the head vortex from the trailing stem and the eventual reconnection. The pinch-off and reconnection leads to an overshoot of the plume front which is a common observation reported in previous studies. The penetration rate in PDF is more predictable and depends on the continuous feeding of buoyancy and momentum into the head vortex by the trailing buoyant-jet stem. Similarity solutions are developed for PDF to describe the temporal variation of the penetration rate, by incorporating the behavior of an isolated buoyant vortex ring and recent laboratory results on the trailing buoyant jet. In particular, the variations of velocity ratios between the head vortex and trailing buoyant jet are analytically computed. To verify the similarity solutions, experiments were conducted on vertical starting forced plumes using planar laser induced fluorescence (PLIF).

• 대한기계학회논문집B
• /
• 제23권7호
• /
• pp.918-927
• /
• 1999

In the fully developed internal flow fields, there are complex transition flows caused by interaction of the cross flow and jet when jet is Injected Into the flow. These interactions are studied by means of the flow visualization methods. An instantaneous laser tomographic method is used to reveal the physical mechanism and the structure of vortices formation in the branch pipe flow. The velocity range of cross flow of the pipe is 0.7m/s and the corresponding Reynolds number $R_{cf}$, based on the duct height is $5.6{\times}10^3$, diameter/height ratios(d/H) 0.14 and velocity ratios 3.0. Oil mist with the size of $10{\mu}m$ diameter is used for the scattering particle. The instantaneous topological features of the vortex ring roll-up of the jet shear layer and characteristics of this flow are studied in detail by performing flow visualization in rectangular duct flow. It is found that the formation and roll-up of ring vortices is a periodic phenomenon. The detailed topology of the vortices in the near field of a cross -flow jet and the mechanism associated with them give enforced hints of vortex breakdown within the vortex system due to the interaction of the jet and the cross-flow.

• 대한기계학회논문집
• /
• 제12권5호
• /
• pp.1175-1188
• /
• 1988

본 연구에서는 조건와류를 추출하려면 우선 속도상관관계를 알아야 하는데, 이를 위하여 실험적 데이타와 이론적 모델을 모두 적용하였다. 전자는 Van Atta와 Chen의 그리드 난류에서의 등방성에 가까운 속도상관관계 데이터를 취하여 이용하였으 며, 후자는 Driscoll과 Kennedy의 난류에너지 스펙트럼 모델을 해석하여 적용하였다. 이 이론적 모델은 레이놀즈수를 변화시킬 수 있는 장점이 있으며, 특히 벽면근처에서 의 와동구조해석을 위해서는 레이놀즈수가 작은 조건와류가 필요하다. 조건와류의 반지모양의 와동은 이방성분포인 평균전단유동에 중첩되어 전체 와동장을 구성하는데, 난류유동의 vortex stretching과정에서 중요한 역할을 하는 머리핀 와동(hairpin vor- tex)과 비슷한 구조를 이 전체 와동에서 구할 수 있다. 이는 조건와류의 와동장의 크기와 평균전단에 의한 평균 와동장의 상호크기에 따라 결정되는데, 실제 난류유동장 에서 난류전달과 레이놀즈 응력과 밀접한 관계가 있다.

• 대한기계학회논문집B
• /
• 제28권6호
• /
• pp.652-658
• /
• 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 shown to compare well with the experimental results for the case of infinity Rossby number. The satisfactory agreement between the two results was possible when in the numerics the free surface was treated as a solid wall so that a no-slip condition was applied on the surface. The numerical solutions reveal that inertial oscillation plays an important role at small Rossby numbers, or at a larger background rotation.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2003년도 추계학술대회
• /
• pp.640-645
• /
• 2003

In this paper, we report the numerical and experimental solutions of the vortical flows 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 shown to compare well with the experimental results for the case of infinity Rossby number. The satisfactory agreement between the two results was possible when in the numerics the free surface was treated as a solid wall so that a no-slip condition was applied on the surface. The numerical solutions reveal that inertial oscillation plays an important role at small Rossby numbers, or at a large background rotation.

• Journal of Ship and Ocean Technology
• /
• 제7권2호
• /
• pp.40-47
• /
• 2003

LDV measurements in large cavitation tunnel around a propeller in operation are carried out to provide valuable information for more accurate wake-adapted propeller design and to study hull-propeller interactions. Effective velocities are computed by both the simplified vortex ring method and by RANS solver with the body force representing the propeller load. The former method uses the nominal velocities measured at the propeller plane as an input data of the numerical method and shows a better agreement with experimental data. The latter shows the qualitative agreement and may be used as an alternative design tools in the preliminary design stage.

• 한국군사과학기술학회지
• /
• 제10권1호
• /
• pp.130-143
• /
• 2007

Using steady state aerodynamic theories, it has been claimed that insects and birds cannot fly. To make matters worse, insects and birds fly at low Reynolds numbers. Therefore, a recurring theme in the literature is the importance of understanding unsteady aerodynamic effect and how the vortices behave when they separate from the moving surface that created them. In flapping flight, birds and insects can modify wing beat amplitude, stroke angle, wing planform area, angle of attack, and to a lesser extent flapping frequency to optimize the generation of lift force. Some birds are thought to employ two different gaits(a vortex ring gait and a continuous vortex gait) and unsteady aerodynamic effect(Clap and fling, Delayed stall, Wake capture and Rotational Circulation) in flapping flight. Leading edge vortices may produce an increase in lift. The trailing edge vortex could be an important component in gliding flight. Tip vortices in hovering support the body weight of the hummingbirds. Thus, this study investigated how insects and birds generate lift at low Reynolds numbers. This research is written to further that as yet incomplete understanding.

• 대한기계학회논문집B
• /
• 제22권7호
• /
• pp.1013-1021
• /
• 1998

Various vortical structures are investigated by using three kinds of flow visualization methods in branch pipe flows. There are two typical flow patterns when a jet from the branch pipe with various angles is injected to the main pipe cross flow. The velocity range of cross flow of the main pipe is 0.2 m/s ~ 1.2 m/s and the corresponding Reynolds number, R$_{p}$ is of the range 1.5 * 10$^{3}$ ~ 9.02 * 10$^{3}$. The velocity ratio(R), jet velocity/cross flow velocity, is chosen from 1.3 to 4. The subsequent behavior and development of the ring vortices which are created at the jet boundary mainly depend on the velocity ratio. An empirical relation for the shedding frequency of the ring vortices is derived. It is also found that there are two different vortex shedding mechanism in the mixing of two fluid streams.s.

• International Journal of Aeronautical and Space Sciences
• /
• 제18권1호
• /
• pp.17-27
• /
• 2017

The treatment of rotor wake has been a critical issue in the field of the rotor aerodynamics. This paper presents a new free wake model for the unsteady analysis for a wind turbine. A blade-wake-tower interaction is major source of unsteady aerodynamic loading and noise on the wind turbine. However, this interaction can not be considered in conventional free wake model. Thus, the free wake model named Finite Vortex Element (FVE hereafter) was devised in order to consider the interaction effects. In this new free wake model, the wake-tower interaction was described by dividing one vortex filament into two vortex filaments, when the vortex filament collided with a tower. Each divided vortex filaments were remodeled to make vortex ring and horseshoe vortex to satisfy Kelvin's circulation theorem and Helmholtz's vortex theorem. This model was then used to predict aerodynamic load and wake geometry for the horizontal axis wind turbine. The results of the FVE model were compared with those of the conventional free wake model and the experimental results of SNU wind tunnel test and NREL wind tunnel test under various inflow velocity and yaw condition. The result of the FVE model showed better correlation with experimental data. It was certain that the tower interaction has a strong effect on the unsteady aerodynamic load of blades. Thus, the tower interaction needs to be taken into account for the unsteady load prediction. As a result, this research shows a potential of the FVE for an efficient and versatile numerical tool for unsteady loading analysis of a wind turbine.