• 사물인터넷융복합논문지
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• 제8권2호
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• pp.1-6
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• 2022

본 논문은 Wake-up radio를 활용한 지역화 Time Slotted Channel Hopping (TSCH) 슬롯프레임 기반 항공 데이터 수집 기법을 제안한다. 제안하는 기법은 무인항공기가 대규모 서비스 영역 내 배치된 센서 기기들의 데이터를 수집할 때 소요되는 지연 시간 및 소모 에너지를 최소화하는 것을 목표로 한다. 이를 위해, 제안 기법은 서비스 영역을 다수의 지역으로 분할하고, 각 지역 내 센서 기기들이 요구하는 셀의 수에 따라 지역별로 TSCH 슬롯프레임의 길이를 결정한다. 이후, 각 지역 내 센서 기기들의 ID를 활용하여 TSCH 슬롯프레임 내 데이터 전송 전용 셀을 할당한다. 에너지 효율적인 데이터 수집을 위해, 센서 기기는 Wake-up radio를 활용한다. 구체적으로, 센서 기기는 Wake-up radio를 활용하여 비콘 수신 및 데이터 전송을 위해 할당된 셀에서만 네트워크 인터페이스를 활성화한다. 시뮬레이션 결과는 제안 기법이 기존 기법 대비 지연 시간 및 에너지 소모 측면에서 더 우수한 성능을 가지는 것을 보여주었다.

• 한국해양공학회지
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• 제22권5호
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• pp.1-6
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• 2008

A kinematics model of a ship wake in the presence of surface waves generated by wind is presented. It was found that a stationary wave structure behind a ship covered a wedge region with the angle at the top of the wake and that only divergent waves were present in a ship wake instead of both the longitudinal and cross-waves, which are known as the Kelvin model. Ship motion at some angle to wind waves can cause an essential asymmetry of the wake, compressing its windward half.

• 풍력에너지저널
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• 제4권1호
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• pp.68-74
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• 2013

Offshore wind farm is being increased since there are much trouble to develop onshore wind farm. But in the offshore, wind turbine wake does not dissipate less than onshore wind turbine because of low turbulence level. Thus this remained wake interacted to other wind turbine. This interaction reduces energy production in wind farm and have a bad influence on fatigue load of wind turbine. In this research, CFD model was constructed to analyze wake effect in offshore wind farm. A method that wind turbine rotor region was modelled in porous media was devised to reduce computation load and validated by comparison with Horns Rev measurement. Then wake interaction between two wind turbine was analyzed by devised porous model.

• 대한기계학회논문집B
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• 제28권2호
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• pp.181-188
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• 2004

The frequency characteristics in an axial flow fan operating at a design and three off-design operating conditions have been investigated by measuring the velocity fluctuation of a tip leakage vortex and a wake flow. Two hot-wire probe sensors rotating with the fan rotor. a fixed and a moving ones, were introduced to obtain a cross-correlation coefficient between two sensors as well as the fluctuating velocity. The results show that the spectral peaks due to the fluctuating velocity near the rotor tip are mainly observed in the reverse flow region of higher flow rates than those in the peak pressure operating condition. However, no peak frequency presents near the rotor tip for near stall condition. Detailed wake flow just downstream of the rotor blade was also measured by the rotating hot-wire sensor. The peak frequency of a high velocity fluctuation due to Karman vortex shedding in the wake region is mainly observed at the higher flow rate condition than that in the design point.

• 대한기계학회논문집
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• 제18권5호
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• pp.1310-1321
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• 1994

Turbulent coherent structures in the intermediate wake of a stationary and rotating cylinder, spin rate S=0.7, situated in a uniform were experimentally investigated using a conditionalphase average technique. Measurements were carried out at a section of 8.5 diameters downstream form the center of cylinder and a Reynolds number of $Re=6.5{\times}10^{3}.$/TEX> The phase averaged velocity and velocity vector fields, contours of vorticity, turbulent intermittency function and velocity fluctuation energy are presented and discussed in relation to the large scale coherent structures by Karman vortices that shed periodically from the cylinder. Coherent wake structures of the rotating cylinder is almost identical with stationary cylinder, but the lateral displacement and shrinkage of turbulent wake region is occured by rotation. Rotation of the cylinder result in that the deflection of wake center to deceleration region(Y/D${\simeq}-0.3)$ and the decrease of mean velocity defect(10%), vorticity strength of large scale structures(19%), total velocity fluctuation energy(12%).

• 한국방송∙미디어공학회:학술대회논문집
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• 한국방송∙미디어공학회 2019년도 추계학술대회
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• pp.233-234
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• 2019

We propose a novel algorithm for detecting ship wake trails in optical images of the maritime environment. The proposed algorithm first removes the sky region by localizing the horizon to prevent false wake trails detection. Then, a feature map is computed by employing brightness distortion and chromatic distortion. The feature map is thresholded to obtain a rough estimate of wake trails. Finally, the wake map is refined using the shape prior information. Experimental results show that the proposed algorithm can effectively detect wake trails in images.

• 대한기계학회논문집B
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• 제27권12호
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• pp.1708-1715
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• 2003

An experimental study was made of turbulent separated and reattaching flow over a backward-facing step, where unsteady wake was generated by a spoked-wheel type wake generator with cylindrical rods in front of the separated flow. The influence of unsteady wake was scrutinized in terms of the rotating speed of the wake generator (0$\leq$S $t_{H}$$\leq$0.4). A conditional averaging technique in corporation with SBF was employed to elucidate the influence of the unsteady wake on the large-scale vortical structures of the separated flow. Special attention was made during two-dimensional measurements of wall-pressure with or without unsteady wake. The wall-pressure fluctuations were used to predict dipole sound source by Curie's integral formula. It was found that the reduction of the dipole sound source was due to the reduction of turbulent kinetic energy by unsteady wake in the recirculation region.n.

• 한국유체기계학회 논문집
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• 제7권5호
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• pp.36-42
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• 2004

The effect of tip clearance height on the three-dimensional flow and aerodynamic loss in the wake region of a high-turning turbine rotor cascade has been investigated with a miniature cone-type five-hole probe. Distributions of velocity magnitude, secondary velocity vectors, and total-pressure loss coefficient are presented for three tip gap-to-span ratios of h/s = 0.0, 0.5 and 1.0 percent. The result shows that with the increment of h/s, tip leakage vortex tends to be intensified and aerodynamic loss due to the leakage vortex is increased as well. In the case of h/s = 1.0 percent, aerodynamic loss in the tip-leakage flow region is found dominant in comparison with that in the passage vortex region. With increasing h/s, mass-averaged secondary loss coefficient has a greater portion in the mass-averaged total-pressure loss coefficient.

• 대한조선학회논문집
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• 제42권6호
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• pp.619-630
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• 2005

A two-frame PIV (Particle Image Velocimetry) technique is used to investigate the wake characteristics behind a marine propeller with 4 blades at high Reynolds number. For each of 9 different blade phases from $ 0^{\circ} $ to $ 80^{\circ} $, one hundred and fifty instantaneous velocity fields are measured. They are ensemble averaged to study the spatial evolution of the propeller wake in the region ranging from the trailing edge to one propeller diameter (D) downstream location. The phase-averaged mean velocity shows that the trailing vorticity is related to radial velocity jump, and the viscous wake is affected by boundary layers developed on the blade surfaces and centrifugal force. Both Galilean decomposition method and vortex identification method using swirling strength calculation are very useful for the study of vortex behaviors En the propeller wake legion. The slipstream contraction occurs in the near-wake region up to about X/D : 0.53 downstream. Thereafter, unstable oscillation occurs because of the reduction of interaction between the tip vortex and the wake sheet behind the maximum contraction point.

• 한국해안·해양공학회논문집
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• 제26권3호
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• pp.113-119
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• 2014

콘크리트와 강재로 제작된 상자형 어초의 흐름응답과 구조응답 수치해석을 수행하였다. 흐름해석으로부터 대상 어초의 후류역과 항력계수를 평가하였으며 압력장을 외력으로 재하하여 구조해석을 수행하고 대상어초의 응력과 변형을 평가하였다. 후류역 평가를 위하여 후류체적 개념을 도입하였고 이로부터 유향과 유속에 따른 후류역의 변동을 정량적으로 제시하였다. 해석결과로부터 흐름응답은 유향에 지배적인 영향을 받으나 유속과는 무관하며 구조응답은 유향과 유속에 영향을 받지만 그 크기가 매우 작고, 단일어초의 최적 설치 조건(유향 $30^{\circ}$)에서 대상어초의 후류체적은 공용적의 3.52배임을 알 수 있었다.