• Title/Summary/Keyword: wind incidence angle

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Wind Tunnel Test of the Straight and Forward Swept Canards

  • Chung, Jin-Deog;Sung, Bong-Zoo;Lee, Jang-Yeon;Kim, Eung-Tai
    • International Journal of Aeronautical and Space Sciences
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    • v.4 no.1
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    • pp.19-25
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    • 2003
  • A low speed wind tunnel test for the canard airplane model was conducted in KARI LSWT. To measure the required level of accuracy, the image system was applied for all elevator deflection and different canard incidence conditions. By doing so, the difference in aerodynamic characteristics between the forward swept and straight canards can be precisely evaluated, and the pros and cons of both canards arrangements can be discussed. Compared with both canard configurations at the same incidence angle setting, the straight canard has benefits in lift and drag, and the slope of pitching moment increases more moderately than the forward swept canard. The listed data and discussion would be useful to whom wants to design a canard airplane.

Aerodynamic Performance of a Wind-Turbine Affected by Blade Configuration (브레이드 외형(外形)이 풍력(風力) 터어빈의 공력(空力) 성능(性能)에 미치는 영향)

  • Son, Byung-Chan
    • Solar Energy
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    • v.6 no.2
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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.

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NUMERICAL STUDY OF FLOW PATTERNS PAST AN INCLINED SQUARE CYLINDER (기울어진 정방형 실린더를 지나는 유동패턴의 수치해석적 연구)

  • Yoon, Dong-Hyeog;Yang, Kyung-Soo;Choi, Choon-Bum
    • Journal of computational fluids engineering
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    • v.14 no.2
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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.

L-band SAR-derived Sea Surface Wind Retrieval off the East Coast of Korea and Error Characteristics (L밴드 인공위성 SAR를 이용한 동해 연안 해상풍 산출 및 오차 특성)

  • Kim, Tae-Sung;Park, Kyung-Ae;Choi, Won-Moon;Hong, Sungwook;Choi, Byoung-Cheol;Shin, Inchul;Kim, Kyung-Ryul
    • Korean Journal of Remote Sensing
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    • v.28 no.5
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    • pp.477-487
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    • 2012
  • Sea surface winds in the sea off the east coast of Korea were derived from L-band ALOS (Advanced Land Observing Satellite) PALSAR (Phased Array type L-band Synthetic Aperture Radar) data and their characteristics of errors were analyzed. We could retrieve high-resolution wind vectors off the east coast of Korea including the coastal region, which has been substantially unavailable from satellite scatterometers. Retrieved SAR-wind speeds showed a good agreement with in-situ buoy measurement by showing relatively small an root-mean-square (RMS) error of 0.67 m/s. Comparisons of the wind vectors from SAR and scatterometer presented RMS errors of 2.16 m/s and $19.24^{\circ}$, 3.62 m/s and $28.02^{\circ}$ for L-band GMF (Geophysical Model Function) algorithm 2009 and 2007, respectively, which tended to be somewhat higher than the expected limit of satellite scatterometer winds errors. L-band SAR-derived wind field exhibited the characteristic dependence on wind direction and incidence angle. The previous version (L-band GMF 2007) revealed large errors at small incidence angles of less than $21^{\circ}$. By contrast, the L-band GMF 2009, which improved the effect of incidence angle on the model function by considering a quadratic function instead of a linear relationship, greatly enhanced the quality of wind speed from 6.80 m/s to 1.14 m/s at small incident angles. This study addressed that the causes of wind retrieval errors should be intensively studied for diverse applications of L-band SAR-derived winds, especially in terms of the effects of wind direction and incidence angle, and other potential error sources.

Experimental study on possible vortex shedding in a suspension bridge - Part II - Results when under typhoon Babs and York

  • Law, S.S.;Yang, Q.S.;Fang, Y.L.
    • Wind and Structures
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    • v.10 no.6
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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.

Aerodynamic Analysis of Tilt-Rotor Unmanned Aerial Vehicle with Computational Fluid Dynamics

  • Kim Cheol-Wan;Chung Jin-Deog
    • Journal of Mechanical Science and Technology
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    • v.20 no.4
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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.

Static Wind Tunnel Test of Smart Un-manned Aerial Vehicle(SUAV) for TR-S2 Configuration (스마트 무인기 TR-S2 형상의 정적 풍동시험)

  • Choi Sungwook;Cho Taehwan;Chung Jindeog
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.29 no.6 s.237
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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.

Wind Tunnel Test to Enhance Aerodynamic Characteristics of Forward Swept Wing Airplane (전진익형 항공기 공력특성 증진을 위한 풍동시험)

  • Chung, Jin-Deog;Lee, Jang-Yeon;Sung, Bong-Zoo;Lee, Jong-Won
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.7
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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.

RADARSAT 자료를 이용한 Wind Vector 추출기법 연구

  • 김덕진;강성철;문우일
    • Proceedings of the KSRS Conference
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    • 2000.04a
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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.

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Estimation of Sea Surface Wind Speed and Direction From RADARSAT Data

  • Kim, Duk-Jin;Wooil-M. Moon
    • Proceedings of the KSRS Conference
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    • 1999.11a
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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.

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