• Title/Summary/Keyword: Velocity Deficit

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Experimental Study on the Effects of Upstream Periodic Wakes on Aerofoil-Boundary Layer and Loss (주기적 상류 후류의 익 경계층과 손실에 미치는 영향에 대한 실험적 연구)

  • Rim, In-Won;Cho, Kang-Rae;Joo, Won-Gu
    • Proceedings of the KSME Conference
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    • 2001.06e
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    • pp.661-667
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    • 2001
  • This paper is concerned with the effects of periodically approaching upstream wakes on cascade-flow and loss. The reduced frequency of the periodic wakes was varied in the narrow range from 0.5 to 0.7. According to a wake-passing through the cascade, two velocity deficits appear near the boundary layer contour in the downstream from about 60% chord-length. The first velocity deficit is caused by a periodic wake and the second one appears after some delayed time. The second velocity deficit may be interpreted as the results of reattachment of flow-separation. The higher reduced frequency decreases the duration time of separation appearance and the lesser loss of aerofoil is resulted.

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Experimental Study on the Effects of Upstream Periodic Wakes on Aerofoil-Boundary Layer and Loss (주기적 상류 후류의 익 경계층과 손실에 매치는 영향에 대한 실험적 연구)

  • Im, In-Won;Jo, Gang-Rae;Ju, Won-Gu
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.26 no.2
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    • pp.219-226
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    • 2002
  • This paper is concerned with the effects of periodically approaching upstream wakes on cascade-flow and loss. The reduced frequency of the periodic wakes was varied in the narrow range from 0.5 to 0.7 Corresponding to a wake-passing through the cascade, two velocity deficits appeared near the boundary layer contour in the downstream from about 60% chord-length. The first velocity deficit was caused by a periodic wake and the second one appeared after some delayed time. The second velocity deficit was interpreted as the results of reattachment of flow-separation. The higher reduced frequency decreased the duration time of separation appearance and the lesser losses of blade were resulted.

Validation of the Eddy Viscosity and Lange Wake Models using Measured Wake Flow Characteristics Behind a Large Wind Turbine Rotor (풍력터빈 후류 유동특성 측정 데이터를 이용한 Eddy Viscosity 및 Lange 후류모델의 예측 정확도 검증)

  • Jeon, Sang Hyeon;Go, Young Jun;Kim, Bum Suk;Huh, Jong Chul
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.1
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    • pp.21-29
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    • 2016
  • The wake effects behind wind turbines were investigated by using data from a Met Mast tower and the SCADA (Supervisory Control and Data Acquisition) system for a wind turbine. The results of the wake investigations and predicted values for the velocity deficit based on the eddy viscosity model were compared with the turbulence intensity from the Lange model. As a result, the velocity deficit and turbulence intensity of the wake increased as the free stream wind speed decreased. In addition, the magnitude of the velocity deficit for the center of the wake using the eddy viscosity model was overestimated while the turbulence intensity from the Lange model showed similarities with measured values.

Analytic Model for Concentration Deficit Profile Caused by a Large Vegetated Area (녹지의 대기정화효과 분석을 위한 해석적 대기확산모델의 유도)

  • 김석철
    • Journal of Korean Society for Atmospheric Environment
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    • v.16 no.5
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    • pp.539-544
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    • 2000
  • A simple analytic model is proposed here to analyze the concentration deficit field caused by a large area of vegetated area. With non-dimensional deposition velocity chosen as small parameter, the regular perturbation method is exploited to derive the mass balance equation and the dynamic equations for the concentration deficit field, Analytic solutions to those equations are obtained in a closed form for several cases of interest, assuming that the concentration field is stationary and the plume can be nicely approximated as Gaussian for a point source. The results suggest that quite a negligible fraction (less than 1%) of the gaseous air pollutants emitted into the air is removed by the vegetated area of which width is 4 km in wind-wise direction, the typical dimension of the Restricted Development Zones around the metropolitan regions in South Korea.

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Effects of Unilateral and Bilateral Movement on Muscle Strength and Activity During Maximum Contraction (최대 근수축시 외측운동과 양측운동이 근력과 근활동에 미치는 영향)

  • Kim, Yong-Woon
    • Korean Journal of Applied Biomechanics
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    • v.23 no.2
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    • pp.149-157
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    • 2013
  • In the present study, we aimed to elucidate how muscle strength and activity are affected by movement pattern(bilateral [BLM] & unilateral movement [ULM]) and movement velocity($0^{\circ}$/s, $60^{\circ}$/s, $120^{\circ}$/s) at maximum effort, and to elucidate the relationship between a left/right asymmetry and bilateral deficit. A total of 18 healthy males participated in the study. Each participant performed maximum knee extension bilaterally and unilaterally while the EMG and moment were recorded, and then the relationships between the asymmetry and bilateral deficit were analyzed. The peak moments for the isokinetic motion at $60^{\circ}$/s and $120^{\circ}$/s and overall muscle activities of lower extremity were significantly reduced for the BLM in comparison to the ULM. And though the asymmetry in ULM were maintained during BLM at all velocities, the bilateral deficits at the velocity of $0^{\circ}\acute{y}$/s and $120^{\circ}\acute{y}$/s were significantly correlated with increased asymmetries of muscle strength in ULM. In conclusion, the reduction in the muscle strength exhibited in bilateral knee extension was shown to arise partially from a reduction in muscle activity, and left/right asymmetry was found to be associated with mechanical reduction in bilateral movement. These findings suggest that training aimed at increasing muscle strength must involve methods and strategies intended to reduce left/right asymmetry.

Investigation of vortex core identification method for wind turbine wake (터빈 후류를 관찰하기 위한 와류 코어 식별 기법 연구)

  • Ko, Seungchul;Na, Jisung;Lee, Joon Sang
    • Journal of the Korean Society of Visualization
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    • v.15 no.1
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    • pp.19-24
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    • 2017
  • In this study, we conduct a numerical experiment of the single 5MW NREL wind turbine and compare the performance of various vortex core identification for the wake behind the wind turbine. In the kinetic analysis of wind turbine, 20% velocity deficit at 200 s is observed, showing wake which contains tip vortex near blade tip and rotor vortex at the center of the wind turbine. Time series of velocity and turbulent intensity show numerical simulation converge to a quasi-steady state near 200 s. In the comparison between methods for vortex identification, ${\lambda}_2$-method has good performance in terms of tip vortex, rotor vortex, vortex during its cascade process compared to vorticity magnitude criteria, ${\Delta}$-method. We conclude that ${\lambda}_2$-method is suitable for vortex identification method for wake visualization.

The Effects of Lower Extremity Asymmetry on Performance of Vertical Jumping (하지의 비대칭성이 수직점프의 수행력에 미치는 영향)

  • Kim, Yong-Woon
    • Korean Journal of Applied Biomechanics
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    • v.18 no.1
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    • pp.179-190
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    • 2008
  • The purpose of this study was to identify whether or not in one-leg vertical jump of each limb asymmetry between both sides is present and to identify how the discrepancies between both limbs affect two-leg jumping performance, that is bilateral deficit. We had 13 healthy subjects perform one-leg jump for both sides and two-leg countermovement jump. The result of biomechanical analysis showed significantly difference of 4-7% in net impulses and work output between dominant and non-dominant one-leg jump and bilateral deficit of 24% when sum of those of each one-leg jump was compared with two-leg jump. But asymmetry in lower extremity was not significantly correlated with bilateral deficit. Two-leg jump could be characterized by relatively short propulsion time, long propulsion distance and high joint angular velocity compared with one-leg jump. These factors seemed to contribute to decreased performance in two-leg jump. Furthermore bilateral deficit was attributed to lower activities of extensor muscles found in two-leg jump.

Investigation of wake characteristics in turbulence of stable atmospheric boundary layer (안정경계층 난류에서의 터빈 후류 특성 연구)

  • Na, Jisung;Ko, Seungchul;Lee, Joon Sang
    • Journal of the Korean Society of Visualization
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    • v.14 no.3
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    • pp.28-31
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    • 2016
  • In this study, we investigate the wake characteristics in two cases which are laminar inflow and turbulent inflow. To solve the flow with wind turbines and its wake, we use large eddy simulation (LES) technique with actuator line method (ALM) and turbulent inflow of Turbsim. Turbulent inflow which contains the characteristic of the stable atmospheric boundary layer is used. We perform the quantitative analysis of velocity deficit and turbulence intensity in two cases. Time series of velocity deficit at the first, the second column in two cases are compared to observe the performance of wind turbine. The performance in the first column in laminar inflow is overestimated compared to that in turbulent inflow. And we observe that wake in the case with turbulent inflow drive to the span-wise direction and wake recovery in turbulent inflow is more effective. In quadrant analysis of Reynolds stress, the ejection and the sweep motion in turbulent inflow case are bigger than those in laminar inflow case.

PIV Velocity Field Analysis of Inflow ahead of a Rotating Marine Propeller (회전하는 선박 프로펠러 전방 유입류에 대한 PIV 속도장 해석)

  • 이상준;백부근
    • Journal of the Society of Naval Architects of Korea
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    • v.41 no.4
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    • pp.30-37
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    • 2004
  • Flow characteristics of the inflow ahead of a rotating propeller attached to a container ship model were investigated using a two-frame PIV (Particle Image Velocimetry) technique. Ensemble-averaged mean velocity fields were measured at four different blade phases. The mean velocity fields show the acceleration of inflow due to the rotating propeller and the velocity deficit in the near-wake region. The axial velocity distribution of inflow in the upper plane of propeller is quite different from that in the lower plane due to the thick hull boundary layer. The propeller inflow also shows asymmetric axial velocity distribution in the port and starboard side. As the inflow moves toward the propeller, the effect of phase angle variation of propeller blade on the inflow becomes dominant. In the upper plane above the propeller axis the inflow has very low axial velocity and large turbulent kinetic energy, compared with the lower plane. The boundary layer developed along the bottom surface of stern hull forms a strong shear layer affecting vortex structure of the propeller near-wake.

Prediction of Aerodynamic Performance on Wind Turbines in the Far Wake (후류 영향을 고려한 풍력 발전 단지 성능 예측 연구)

  • Son, Eunkuk;Kim, Hogeon;Lee, Seungmin;Lee, Soogab
    • 한국신재생에너지학회:학술대회논문집
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    • 2011.05a
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    • pp.59.2-59.2
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    • 2011
  • Although there are many activities on the construction of wind farm to produce amount of power from the wind, in practice power productions are not as much as its expected capabilities. This is because a lack of both the prediction of wind resources and the aerodynamic analysis on turbines with far wake effects. In far wake region, there are velocity deficits and increases of the turbulence intensity which lead to the power losses of the next turbine and the increases of dynamic loadings which could reduce system's life. The analysis on power losses and the increases of fatigue loadings in the wind farm is needed to prevent these unwanted consequences. Therefore, in this study velocity deficits have been predicted and aerodynamic analysis on turbines in the far wake is carried out from these velocity profiles. Ainslie's eddy viscosity wake model is adopted to determine a wake velocity and aerodynamic analysis on wind turbines is predicted by the numerical methods such as blade element momentum theory(BEMT) and vortex lattice method(VLM). The results show that velocity recovery is more rapid in the wake region with higher turbulence intensity. Since the velocity deficit is larger when the turbine has higher thrust coefficient, there is a huge aerodynamic power loss at the downstream turbine.

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