• 태양에너지
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• 제6권2호
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• pp.86-92
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• 1986

This paper presents the aerodynamic performances of horizontal axis wind turbines with non-twisted but taperd blades. Five configurations of blades, namely, one straight blade and four tapered blades with taper ratio of ranging from 0.1 to 0.7 have been simulated. The aerodynamic performances of the wind turbines have been determined over blade incidence angle of ranging from $2^{\circ}$ to $6^{\circ}$ and keeping same solidity and radius of them. The results are presented comparing straight blade from four tapered blades for maximum power coefficient and tip looses against variation of taper ratio. It also shows that the wind turbine with taper ratio of 0.5 has the highest maximum power coefficient than others. And wind turbines with taper ratio below 0.2 have lower values of maximum power coefficients than straight one. The tip loss of straight blade is the largest and reduces Slightly with the decrementation of taper ratio.

• 한국전산유체공학회지
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• 제14권2호
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• pp.19-24
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• 2009

A parametric study has been carried out to elucidate the characteristics of flow past a square cylinder inclined with respect to the main flow for Re$\leq$150. Reynolds number and angle of incidence are the key parameters which determine the flow characteristics. This study would be the first step towards understanding flow pattern past a cylindrical structure under a strong gust of wind from the viewpoint of wind hazards. A complete classification of flow pattern has been obtained in the laminar region.

• 대한원격탐사학회지
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• 제28권5호
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• pp.477-487
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• 2012

L밴드 ALOS SAR 자료를 활용하여 우리나라 동해 연안해역의 해상풍을 산출하고 오차의 특성을 분석하였다. 그 동안 인공위성 산란계를 이용한 해상풍 산출이 본질적으로 불가능하였던 연안 해역에 대하여 SAR 자료로부터 고해상도 해상풍을 산출할 수 있었다. 산출된 SAR 바람을 해양 부이 자료와 비교한 결과 0.67 m/s의 작은 오차로 잘 일치함을 보여주었다. 서로 다른 L밴드 ALOS PALSAR GMF 2007 모델과 2009 모델로 산출된 해상풍을 인공위성 산란계 해상풍과 비교한 결과, 풍속과 풍향 각각 2.16 m/s와 $19.24^{\circ}$, 3.62 m/s와 $28.02^{\circ}$의 제곱평균근오차를 보이며, 인공위성 산란계의 기대 오차보다 다소 큰 경향을 나타냈다. 또한 산출된 L밴드 SAR 바람장은 풍향과 입사각에 대하여 특징적인 의존성을 보였다. L밴드 GMF 2007 모델은 $21^{\circ}$ 보다 작은 입사각에 대하여 큰 오차를 보인 반면, L밴드 GMF 2009 모델은 입사각에 대한 효과를 선형함수가 아니라 이차함수로 고려하여 주었기 때문에 작은 입사각 범위에서 풍속 오차가 6.8 m/s에서 1.14 m/s로 크게 감소하는 결과를 보였다. 본 연구는 L밴드 SAR 바람장의 다양한 활용을 위해서는 풍향과 입사각 효과, 그리고 다른 잠재적인 오차의 요인을 집중적으로 연구하여야 함을 강조하였다.

• Wind and Structures
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• 제10권6호
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• pp.555-576
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• 2007

Statistical analysis on the measured responses of a suspension bridge deck (Law, et al. 2007) show that vibration response at the first torsional mode of the structure has a significant increase at and beyond the critical wind speed for vortex shedding as noted in the wind tunnel tests on a sectional model. This paper further analyzes the measured responses of the structure when under typhoon conditions for any possible vortex shedding events. Parameters related to the lifting force in such a possible event and the vibration amplitudes are estimated with a single-degree-of-freedom model of the system. The spatial correlation of vortex shedding along the bridge span is also investigated. Possible vortex shedding events are found at both the first torsional and second vertical modes with the root-mean-square amplitudes comparable to those predicted from wind tunnel tests. Small negative stiffness due to wind effects is observed in isolated events that last for a short duration, but the aerodynamic damping exhibits either positive or negative values when the vertical angle of wind incidence is beyond ${\pm}10^{\circ}$. Vibration of the bridge deck is highly correlated in the events at least in the middle one-third of the main span.

• Journal of Mechanical Science and Technology
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• 제20권4호
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• pp.561-568
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• 2006

CFD simulation for one of tilt-rotor UAV configurations, TR-E2S1, was performed to investigate its aerodynamic characteristics. Control surfaces such as elevator and rudder were deflected and wing incidence angle was changed. Also aerodynamic stabilities were analyzed with the variation of pitch and yaw angles. The comparison of CFD with wind tunnel test results reveals the same trends in the aerodynamic characteristics and stabilities. However 12% scale wind tunnel test model is too small for accurate data collection and should build a high fidelity model for quantitative data comparison.

• 대한기계학회논문집B
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• 제29권6호
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• pp.755-762
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• 2005

To evaluate the aerodynamic efficiency of TR-S2 configuration designed by SUDC, wind tunnel tests of $40\%$ scaled model were done in KARI LSWT. The aerodynamic characteristics of plain and Semi-Slotted Flaperon were compared, and vortex generators were installed to improve flow pattern along the wing surface. Effects of the control surface such as elevator, rudder, aileron, and incidence angle of horizontal tail are measured for various testing conditions. Test results showed that Semi-Slotted Flaperon produced more favorable lift, lift/drag, and stall margins and application of vortex generator would be best choice to enhance wing performance. Longitudinal, lateral and directional characteristics of TR-S2 were found to be stable for the pitch and yaw motions.

• 대한기계학회논문집B
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• 제28권7호
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• pp.800-808
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• 2004

Wind tunnel test of an airplane model with forward swept wing was done in KARI LSWT to evaluate and measure the aerodynamic characteristics of initially designed configuration. Since the given wing planform did not fully satisfy the design requirements, local flow control devices such as vortilon, vortex generator and flow fence were used to delay separation and to enhance aerodynamic characteristics. Also decision making processes of design parameters such as vertical tail boom length, the location, size and the incidence angle of horizontal tail were discussed. The general aerodynamic characteristics of forward swept wing for various control surface deflection conditions of flap, aileron and elevator were also given.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2000년도 춘계 학술대회 논문집 통권 3호 Proceedings of the 2000 KSRS Spring Meeting
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• pp.79-84
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• 2000

해양 영역에 대한 SAR(Synthetic Aperture Radar) 자료는 좋은 해상도로 기상조건이나 주야에 상관없이 wind vector를 구할 수 있는 장점이 있다. 해안지역의 scatterometer 자료는 육지의 영향으로 인하여 정확한 자료를 얻을 수 없지만, SAR자료를 이용하면, Scatterometer에 비해 좋은 해상도로 해안지역의 wind vector 추출이 가능하다. 본 연구에서는 SAR 자료로부터 풍속을 추출할 수 있는 CMOD_4와 CMOD_IFR2 알고리즘을 사용하였다. 이 알고리즘들은 정확한 sigma-naught 값과, 풍향, 그리고 local incidence angle을 입력변수로 요구한다. CMOD 알고리즘들은 ERS-1/2와 같이 C-band, VV-polarization을 위해 개발된 알고리즘이므로, C-band, HH-polarization을 가진 RADARSAT 자료에 바로 적용할 수가 없다. 이것을 해결하기 위해 본 연구에서는 두 CMOD 알고리즘을 몇 가지 polarization ratio와 같이 적용하여 보았다. 각 연구지역에 해당하는 자료에는 제주도 주변의 Fine mode 자료, 서해안과 제주도 근해의 Standard mode 자료, 그리고 동해안 지역의 ScanSAR 자료 등이다. 여러 가지 Polarization ratio와 CMOD 알고리즘의 조합, 그리고 2-DFFT로부터 추출된 풍향으로부터 각 연구지역의 풍속은 가까운 기상관측소 및, 부이의 관측값과 비교하였다. 그 결과 Fine mode 자료로부터 추출된 풍속은 실제 관측 값보다 항상 상당히 높게 나타났지만, Standard mode 나 ScanSAR 자료로부터 추출된 풍속은 현지 기상관측소 관측 값과 잘 일치한다.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 1999년도 Proceedings of International Symposium on Remote Sensing
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• pp.485-490
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• 1999

Wind vector information over the ocean is currently obtained using multiple beam scatterometer data. The scatterometers on ERS-1/2 generate wind vector information with a spatial resolution of 50km and accuracies of $\pm$2m/s in wind speed and $\pm$20$^{\circ}$ in wind direction. Synthetic aperture radar (SAR) data over the ocean have the potential of providing wind vector information independent of weather conditions with finer resolution. Finer resolution wind vector information can often be useful particularly in coastal regions where the scatterometer wind information is often corrupted because of the lower resolution system characteristics which is often contaminated by the signal returns from the coastal areas or ice in the case of arctic environments. In this paper we tested CMOD_4 and CMOD_IFR2 algorithms for extracting the wind vector from SAR data. These algorithms require precise estimation of normalized radar cross-section and wind direction from the SAR data and the local incidence angle. The CMOD series algorithms were developed for the C-band, VV-Polarized SAR data, typically for the ERS SAR data. Since RADARSAT operates at the same C-band but with HH-Polarization, the CMOD series algorithms should not be used directly. As a preliminary approach of resolving with this problem, we applied the polarization ratio between the HH and VV polarizations in the wind vectors estimation. Two test areas, one in front of Inchon and several sites around Jeju island were selected and investigated for wind vector estimation. The new results were compared with the wind vectors obtained from CMOD algorithms. The wind vector results agree well with the observed wind speed data. However the estimation of wind direction agree with the observed wind direction only when the wind speed is greater than approximately 3.0m/s.

• Wind and Structures
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• 제34권1호
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• pp.15-27
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• 2022

This work comes within the framework of the "Benchmark on the Aerodynamics of a Rectangular Cylinder" that investigates a rectangular cylinder of length-to-depth ratio equal to 5. The present study reports and discusses velocity fields acquired using planar Particle Image Velocitmetry for several angles of attack and Reynolds numbers. In particular, for a cylinder depth-based Reynolds number of 2 × 10⁴ and zero incidence angle, the flow features along the lateral (parallel to the freestream) upper and lower surfaces of the cylinder are reported. Using first and second order statistics of the velocity field, the main flow features are discussed, especially the size and location of the time-averaged flow structures and the distribution of the Reynolds stresses. The variation of the flow features with the incidence is also studied considering angles of attack up to 6°. It is shown that the time-averaged flow is fully detached for incidence higher than 2°. For an angle of attack of 0°, the effects of the Reynolds number varying between 5 × 10³ and 2 × 10⁴ are investigated looking at flow statistics. It is shown that the time-averaged location of the reattachment point and the shape and position of the time-averaged main vortex are mostly constant with the Reynolds number. However, the size of the inner region located below the time-averaged shear layer and just downstream the leading edge corner appears to be strongly dependent on the Reynolds number.