• 제목/요약/키워드: wake field

검색결과 318건 처리시간 0.022초

Prediction of nominal wake of a semi-displacement high-speed vessel at full scale

  • Can, Ugur;Bal, Sakir
    • Ocean Systems Engineering
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    • 제12권2호
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    • pp.143-157
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    • 2022
  • In this study, the nominal wake field of a semi-displacement type high-speed vessel was computed at full scale by using CFD (Computational Fluid Dynamics) and GEOSIM-based approaches. A scale effect investigation on nominal wake field of benchmark Athena vessel was performed with two models which have different model lengths. The members of the model family have the same Fr number but different Re numbers. The spatial components of nominal wake field have been analyzed by considering the axial, radial and tangential velocities for models at different scales. A linear feature has been found for radial and tangential components while a nonlinear change has been obtained for axial velocity. Taylor wake fraction formulation was also computed by using the axial wake velocities and an extrapolation technique was carried out to get the nonlinear fit of nominal wake fraction. This provides not only to observe the change of nominal wake fraction versus scale ratios but also to estimate accurately the wake fraction at full-scale. Extrapolated full-scale nominal wake fractions by GEOSIM-based approach were compared with the full-scale CFD result, and a very good agreement was achieved. It can be noted that the GEOSIM-based extrapolation method can be applied for estimation of the nominal wake fraction of semi-displacement type high-speed vessels.

Wake Field Effect from the Undulator Vacuum Chamber in PAL-XFEL

  • 박용운
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2014년도 제46회 동계 정기학술대회 초록집
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    • pp.151.1-151.1
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    • 2014
  • Wake field effect on the electron beam from the undulator chamber in PAL-XFEL is analyzed. The wake field takeover some energy from the electron beam which will increase the energy spread of the electron beam. This will cause the degradation of the radiation power in PAL-XFEL. To decrease the effect, the surface of the undulator vacuum chamber should be fabricated with 200 nm surface roughness and 5 nm oxidation layer. In this presentation, the numerical calculation of the wake will be shown. Simulation results of the radiation generation in PAL-XFEL also will be presented.

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잔류내 응집 구조 와류의 생성에 관한 연구 (A Study of Generation of Coherent Vortex in Late Wake)

  • 이승수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.443-446
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    • 2002
  • Wake downstream of an object in the stratified flow has been of long-standing interest in fluid dynamics because of its similarity to geophysical flow over topographical terrains and more recently, concerns about the wake left behind a body moving through the ocean thermocline. Decades of studies of geophysical flow have unveiled that the flow downstream of obstacles in stratified flow consists of attached wake and strong internal waves, or separated, fluctuating wake and persistent late wakes, all of which depend on the flow conditions. Among unique and interesting characteristics of the stratified flow past obstacles is the generation of coherent vortex structure in the late wake far downstream of the object. Without the density stratification, the flow field downstream becomes undisturbed after relatively fast diminishing of the near wake. However, no matter how small the stratification is, the flow field downstream self-develops coherent vortex structures even after diminishing of the near wake. This paper present a computational approach to simulate the generation mechanism of the coherent vortex and analysis of the vortical structure.

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로터 제자리비행에 적용된 CFD/FreeWake 연계방법의 원거리 경계조건에 대한 연구 (A Study on the Far-Field Boundary Condition of Tightly Coupled CFD/FreeWake Method in Hover)

  • 위성용;이재훈;권장혁;이덕주;정기훈;김승범
    • 한국항공우주학회지
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    • 제35권11호
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    • pp.957-963
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    • 2007
  • 본 논문에서는 CFD/FreeWake 연계해석방법을 이용하여 헬리콥터 로터의 공력을 해석하였다. 연계해석방법은 CFD를 이용하여 로터주변의 공력을 얻고, 후류의 거동은 FreeWake를 이용하여 모사한다. FreeWake 모델은 CFD의 경계조건을 제공하고, CFD는 후류형성을 위한 로터블레이드 양력변화율을 제공하는 방법으로 연계된다. CFD/FreeWake 연계해석방법은 다른 로터공력해석 방법에 비하여 높은 정확도와 계산 시간 절감으로 효율적인 계산을 가능하도록 한다.

해상 환경을 고려한 수상함 항적 모델 연구 (A Study on the Ship Wake Model under the Ocean Environment)

  • 배호석;김원기;손수욱;김우식;박정수
    • 한국군사과학기술학회지
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    • 제24권1호
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    • pp.22-30
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    • 2021
  • The ship wake generated by rotation of the propeller yields changes of characteristics of sound wave such as attenuation and scattering. To develope a battle field environment simulator for military purposes, it is very important to understand acoustical properties of ship wake. Existing research results have limitations in direct application because they performed under simple conditions or model ships were applied. In this study, we developed a ship wake generation model based on the ship's geometric wake distribution theory. The model can provide spatial distribution and void fraction with various marine environments as well as ship size. Through the developed model, geometric distribution features of ship wake according to the ship's maneuvering conditions were successfully simulated. In addition, changes of the bubble void fraction with time at any location within the battle field environment were identified. Therefore, the developed model is expected to be used in the development of a simulator to measure the acoustic characteristics of the ship wake.

풍력블레이드 비정상 공력하중 해석을 위한 자유후류기법 개발 및 실험적 연구 (New Free Wake Method Development for Unsteady Aerodynamic Load on HAWT Blade and Experimental Analysis)

  • 신형기;박지웅;김호건;이수갑
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2005년도 춘계학술대회
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    • pp.33-36
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    • 2005
  • A critical issue in the field of the rotor aerodynamics is the treatment of the wake. The wake is of primary importance in determining overall aerodynamic behavior, especially, a wind turbine blade includes the unsteady air loads problem. In this study, the wake generated by blades are depicted by a free wake model to analyse unsteady loading on blade and a new free wake model named Finite Vortex Element(FVE hereafter) is devised in order to include a wake-tower interact ion. In this new free wake model, blade-wake-tower interaction is described by cutting a vortex filament when the filament collides with a tower. This FVE model is compared with a conventional free wake model and verified by a comparison with NREL and SNU wind tunnel model. A comparison with NREL and SNU data shows validity and effectiveness of devised FVE free wake model and an efficient.

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후류와 타워의 영향을 고려한 수평축 풍력발전기 블레이드의 비정상 하중 예측을 위한 새로운 자유후류기법의 연구 (Development of a new free wake model considering a waketower interaction for a horizontal axis wind turbine)

  • 신형기;박지웅;이수갑;김주언
    • 신재생에너지
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    • 제1권1호
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    • pp.54-63
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    • 2005
  • A critical issue in the field of the rotor aerodynamics is the treatment of the wake. The wake is of primary importance in determining overall aerodynamic behavior, especially, a wind turbine blade includes the unsteady airloads problem. In this study, the wake generated by blades are depicted by a free wake model to analyse unsteady loading on blade and a new free wake model named Finite Vortex Element(FVE hereafter) is devised in order to include a wake-tower interaction. In this new free wake model, blade-wake-tower interaction is described by cutting a vortex filament when the filament collides with a tower. This FVE model is compared with a conventional free wake model and verified by a comparison with NRELand SNU wind tunnel model. A comparison with NREL and SNU data shows validity and effectiveness of devised FVE free wake model and an efficient.

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대형 풍력터빈 모형의 공력 성능 및 후류 유동장에 대한 비교 연구 (Comparison Study on Aerodynamic Performance and Wake Flow Field for a MW-Class Wind Turbine Model)

  • 정두원;원영수;강승희
    • 한국가시화정보학회지
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    • 제17권2호
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    • pp.32-38
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    • 2019
  • A comparison study between computational-fluid-dynamics simulation and wind tunnel test for a megawatt-class wind turbine is conducted. For the study, flow-field in wake, basic aerodynamic performance, and effect of the yaw error for a 1/86 scaled-down model of the NREL offshore 5 MW wind turbine are numerically calculated using commercial software "FloEFD" with $k-{\varepsilon}$ turbulence model. The computed results are compared to the wind tunnel test performed by the constant-velocity mode for the model. It is shown that discrepancy are found between the two results at lower tip-speed ratio and higher yaw angle, however, the velocity-defection distribution in the wake, the torque coefficient at moderated and high tip-speed ratios are in good agreement with the wind tunnel test.

PIV를 이용한 선박 프로펠러 후류의 속도장 계측 (PIV Velocity Field Measurements of Flow around a Ship with Rotating Propeller)

  • 이상준;백부근
    • 대한조선학회논문집
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    • 제40권5호
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    • pp.17-25
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    • 2003
  • Velocity field behind a container ship model with a rotating propeller has been investigated using PIV (particle image velocimetry) system. Four hundred instantaneous velocity fields were measured at 4 different blade phases and ensemble-averaged to investigate the spatial evolution of vortical structure of near wake within one propeller diameter downstream. The phase-averaged mean velocity fields show the potential wake and the viscous wake formed due to the boundary layers developed on the blade surfaces. The interaction between bilge vortex developed along the hull surface and the tangential velocity component of incoming flow causes to have asymmetric flow structure in the transverse plane.

SUBOFF 모형 후방 난류항적의 수치 시뮬레이션 (Numerical Simulation of Turbulent Wake Behind SUBOFF Model)

  • 나영인;방형도;박종천
    • 대한조선학회논문집
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    • 제47권4호
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    • pp.517-524
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    • 2010
  • This paper covers the numerical studies performed to investigate the characteristics of turbulent wake generated by a submarine, SUBOFF model. A SUBOFF model assumed as an axial-symmetric body was used to generate wake. The numerical simulation was performed by using a commercial S/W, FLUENT, with the same condition as the experiments by Shin et al.(2009). Mainly the cross-sectional distribution of the time-averaged mean wake and turbulent kinetic energy was compared with the experiments. Both results are agreed well with each other in the propeller wake section, but the agreement between both is not so satisfied in the far wake field. It means that more numerous number of grid points and their concentration should be required in that field.