• Proceeding of EDISON Challenge
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• 2015.03a
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• pp.627-631
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• 2015

유동 교란에 의하여 균일유동이 아닌 자유류가 항공기 날개 표면을 지나면 공력 계수들이 균일 자유류 유동과는 달라진다. 예를 들어, 항공기들의 편대 비행에서 앞의 항공기가 생성한 후류가 뒷 항공기에 영향을 주고, 두 개의 주익을 가지는 Tandem Wing 항공기의 경우 첫 번째 주익에서 발생된 후류가 두 번째 주익의 공력에 영향을 미친다. 본 연구는 NACA0012 익형의 앞쪽에 또 다른 익형을 배치하여 앞 쪽의 익형에서 발생한 후류가 뒤의 익형에 미치는 영향을 익형 사이의 거리에 따라 분석하였다. 앞쪽의 익형에서 발생한 압력계수와 뒤쪽에서 발생한 압력계수의 비교를 통해 후류의 효과가 어떤 영향을 끼치는지 확인 하였고, 두 익형 사이의 거리가 2c일 때 후류의 영향이 거의 없음을 확인 하였다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.41 no.7
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• pp.469-480
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• 2017

For accurate AEP prediction in a wind farm, it is necessary to effectively calculate the wind speed reduction and the power loss due to the wake effect in each wind direction. In this study, a computer program for AEP prediction considering directional wake effect was developed. The results of the developed program were compared with the actual AEP of the wind farm and the calculation result of existing commercial software to confirm the accuracy of prediction. The applied equations are identical with those of commercial software based on existing theories, but there is a difference in the calculation process of the detection of the wake effect area in each wind direction. As a result, the developed program predicted to be less than 1% of difference to the actual capacity factor and showed more than 2% of better results compared with the existing commercial software.

• Proceeding of EDISON Challenge
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• 2014.03a
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• pp.614-618
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• 2014

본 연구에서는 디퓨저의 압력회복을 높이기 위해 디퓨저 입구에 실린더를 설치하여 후류가 압력회복에 어떤 영향을 미치는지 알아보았다. 2D-Incomp-2.1-P 해석자를 이용하여 속도, 압력에 따른 유동가시화를 통해 내부유동을 분석하였고, 압력회복계수를 비교하여 디퓨저 입구에 설치된 실린더의 후류가 디퓨저 성능에 어떤 영향을 주는지 비교하였다. 그결과 실린더를 설치하였을 때 확대부에서의 박리영역이 더 작아졌고 압력회복계수가 더 높아졌다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.11 no.6
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• pp.877-883
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• 1987

A new improved inviscid separation model to calculate the mean flow past circular cylinders is proposed. The wake region is modeled by a pair of vortex sheets which emerge from the separation points and are allowed to move freely with the local stream. The vortex strength assumes a constant value for some initial distance which is related to the pressure drag and gradually decreases to zero as the sheet moves farther away from the body. This vorticity distribution automatically takes care of the length parameter which has been one of the deficiencies in the existing models. The procedure is tested against various experimental data and the agreement is quite good for both sub and super-critical regimes. The comparison with an existing model is also given.

• 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.

• Journal of the Society of Naval Architects of Korea
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• v.35 no.1
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• pp.24-31
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• 1998

Unsteady propeller blade forces arising from shaft inclination have been found to be an important contribution tn total blade forces. The position of the wake relative to a blade oscillates with the first blade frequency, thus giving rise to unsteady blade forces which is significant relative to the forces produced directly by flow inclination. In order to find a wake geometry due to shaft inclination, a non-axisymmetric wake model is developed and applied to a specific case, which has experimental values. Predicted cavity shapes and unsteady forces acting on the blades of an inclined shaft propeller are compared to those predicted by other numerical methods, as well as those measured in experiments.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.27 no.4
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• pp.273-279
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• 2014

In this paper, wind tunnel tests of a scaled wind turbine have been performed to investigate the effects of turbulent intensity of oncoming flow on turbine wake field. The scaled turbine model was carefully designed to satisfy the similarity conditions. The wind velocities and turbulent intensities were measured using hotwire anemometer in order to compare with existing wake model. It was found from the tests that the existing wake models well fit with test results at turbulent flow rather than at uniform flow. Finally modified wake model has been proposed based on the measured data.

• Journal of the Korean Solar Energy Society
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• v.31 no.5
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• pp.19-26
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• 2011

복잡지형에서의 풍력단지 CFD 모델링을 통한 시뮬레이션 결과가 이 논문에 주어졌다. 이 연구를 위하여 작은 산(오름)들로 둘러싸인 제주도 성산 풍력단지가 선택되었고, 두 개의 주풍향에 대하여 ANSYS CFX로 시뮬레이션 하였다. 격자생성을 위하여 실제 지형데이터가 사용되었고, 풍력발전기와 복잡지형으로부터 발생하는 후류효과를 예측하기 위하여 SST 난류모델 및 액추에이터 디스크 모델이 적용되었다. 그 결과, 성산 풍력단지 주변에 있는 작은 산 및 풍력발전기에서 발생하는 후류의 영향은 3~7 km 계속된다고 예측되었다. 또한 그 후류는 풍속 및 난류강도에 상당한 영향을 미치고 있다고 예측되었다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.10
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• pp.1-11
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• 2004

An experimental study was carried out to investigate the influence of flow conditions of a boundary layer on the near-wake of a flat plate. Various attaching positions of tripping wires were selected to change flow conditions on a boundary layer. Laminar, transitional, and turbulent boundary layer conditions at 0.98C from the leading edge are imposed to investigate the evolution of symmetric and asymmetric wake. An x-type hot-wire probe(55P61) is employed to measure at 8 stations of the near-wake region. Measured mean velocity distributions are presented in terms of similarity parameter. It is found that the symmetric wake collapses well to the universal profile in the central part of the wake. However, the universal profile is not suitable in describing an asymmetric wake.

• 한국항공운항학회:학술대회논문집
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• 2015.11a
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• pp.63-67
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• 2015

항공기는 공중에서 양력을 발생시키는 과정에서 wake vortex를 생성하며, 항공기 중량과 항공기 주위의 기상(특히 바람 vector)에 따라 wake vortex의 크기와 그 소산속도가 결정된다. 이러한 Raw data 정보는 항공기에 장착된 FMS와 Sensor를 통해 수집될 수 있으며, 이를 ADS-B를 이용하여 지상관제기관과 주변항공기에 전파하면, 실시간으로 매우 정확한 후류크기와 영향범위를 확인할 수 있고, 이로써 보다 안전하고 효율적인 항공기 후류분리가 가능할 것으로 볼 수 있다. 본 자료는, 이러한 맥락에서 ICAO(ASBU)의 후류분리기준 축소를 통한 활주로사용증진 동향과, RTCA DO-260B의 부록(V) "Potential wake vortex and Arrival management ADS-B Application" 요지를 소개한다.