• 제목/요약/키워드: Inflow Angle

검색결과 98건 처리시간 0.029초

흐름의 입사각이 점성토 지반의 수리저항성능에 미치는 영향 (Effect of Incidence Angle of Current on the Hydraulic Resistance Capacity of Clayey Soil)

  • 김영상;한병덕;강경오
    • 한국해안·해양공학회논문집
    • /
    • 제24권1호
    • /
    • pp.26-35
    • /
    • 2012
  • 지금까지 하천 및 해류에서의 지반의 수리저항 특성에 대한 연구는 흐름의 방향을 고려하지 않고 주 흐름방향에 대해서만 고려해 왔다. 최근 왕복류 흐름에 의한 지반의 수리저항특성에 대한 연구결과에 의하면 세립질 및 조립질 시료 모두에서 일방향 흐름보다 왕복류를 고려한 양방향 흐름에서 세굴률이 크게 발생 하는 것으로 나타났다. 그러나 해안구조물이 설치되는 해안 또는 협곡에서 흐름의 방향은 반드시 $180^{\circ}$를 이루지 않으므로 흐름의 입사각이 지반의 수리저항성능에 미치는 영향에 대한 검토가 반드시 필요하다. 이에 흐름방향을 고려할 수 있도록 개선된 수리저항성능 실험기를 이용하여 인공적으로 조성된 점성 세립질 및 점성 조립질 시료에 대하여 $0^{\circ}$, $90^{\circ}$, $135^{\circ}$, $180^{\circ}$의 입사각을 갖는 흐름에 대한 일방향 및 양방향 수리저항성능을 평가하였다. 실험결과 세립질 및 조립질 시료 모두에서 입사각이 커짐에 따라 수리저항성능은 감소하고 세굴률이 증가하는 것으로 나타났다. 압밀압력이 낮은 경우에는 세립토의 수리저항성능이 급격히 떨어지나 압밀압력이 큰 경우에는 조립토의 수리저항성능이 세립토에 비해 약간 더 빠르게 감소하는 것으로 나타났다. 최종적으로는 양방향 흐름일 경우 가장 큰 세굴률이 발생하므로 다양한 흐름방향에 노출되는 구조물의 경우는 양방향 흐름에 대해 수리저항성능을 평가하는 것이 타당한 것으로 판단된다.

Inflow Prediction and First Principles Modeling of a Coaxial Rotor Unmanned Aerial Vehicle in Forward Flight

  • Harun-Or-Rashid, Mohammad;Song, Jun-Beom;Byun, Young-Seop;Kang, Beom-Soo
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제16권4호
    • /
    • pp.614-623
    • /
    • 2015
  • When the speed of a coaxial rotor helicopter in forward flight increases, the wake skew angle of the rotor increases and consequently the position of the vena contracta of the upper rotor with respect to the lower rotor changes. Considering ambient air and the effect of the upper rotor, this study proposes a nonuniform inflow model for the lower rotor of a coaxial rotor helicopter in forward flight. The total required power of the coaxial rotor system was compared against Dingeldein's experimental data, and the results of the proposed model were well matched. A plant model was also developed from first principles for flight simulation, unknown parameter estimation and control analysis. The coaxial rotor helicopter used for this study was manufactured for surveillance and reconnaissance and does not have any stabilizer bar. Therefore, a feedback controller was included during flight test and parameter estimation to overcome unstable situations. Predicted responses of parameter estimation and validation show good agreement with experimental data. Therefore, the methodology described in this paper can be used to develop numerical plant model, study non-uniform inflow model, conduct performance analysis and parameter estimation of coaxial rotor as well as other rotorcrafts in forward flight.

Power and Trim Estimation for Helicopter Sizing and Performance Analysis

  • Laxman, Vaitla;Lim, Jae-Hoon;Shin, Sang-Joon;Ko, Kwang-Ho;Jung, Sung-Nam
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제12권2호
    • /
    • pp.156-162
    • /
    • 2011
  • The preliminary design stage of helicopters consists of various operations and in each operation design several detailed analysis tasks are needed. The analysis tasks include performance and the required power estimation. In helicopter design, those are usually carried out by adopting the momentum theory. In this paper, an explicit form of computational analysis based on the blade element theory and uniform/non-uniform inflow model is developed. The other motivation of the present development is to obtain trim and required power estimation for various helicopter configurations. Sectional and hub loads, power, trim, and flapping equations are derived by using a symbolic tool. Iterative computations are carried out till convergence is achieved in the blade response, inflow, and trim. The predictions regarding the trim and power estimation turn out to be correlated well with the experimental results. The effect of inflow is further investigated. It is found that the present prediction for the lateral cyclic pitch angle is improved with the non-uniform inflow model as compared to that by the uniform inflow model. The presently improved trim and power estimation will be useful for future helicopter sizing and performance analysis.

조류발전용 터빈 주위의 유동 특성에 관한 연구 (A Study on the Flow Characteristics around Tidal Current Turbine)

  • 김부기;양창조
    • 해양환경안전학회지
    • /
    • 제18권6호
    • /
    • pp.610-616
    • /
    • 2012
  • 세계는 지금 본격적인 에너지 기후시대로 도래했으며 녹색성장을 이끌 강력한 에너지 정책이 선진국가 진입의 초석으로 신재생에너지를 활용하여 미래의 에너지 자원으로 동력화하는 것이 21세기 에너지 수요를 충족시키는 개발 목표가 되고 있다. 최근 신재생에너지 개발의 필요성에 따라 해양에너지가 주목을 받고 있다. 해양에너지는 아직 개발되지 않은 가장 유망한 재생 및 청정에너지 자원 중 하나이다. 이에 따라 각 해역에 적합한 조류에너지 변환장치의 개발이 매우 필요하다. 본 연구에서는 조류발전용 터빈에 작용하는 유입각, 해저면 효과 및 공동현상 발생에 따른 효율의 변화를 후류유동특성을 통해 파악하였다. 계산 조건하에서 해저면 효과에 의한 효율저하는 크게 나타나지 않았고, 유입각은 10도 이상부터 효율 저하가 나타났고 45도에서는 출력계수가 7 % 낮게 계산되었다. 유입속도가 증가할수록 토크와 출력계수가 증가하였으나, 공동현상이 발생하는 3 m/s이상부터 오히려 출력저하가 나타났다. 또한 유동특성의 고찰을 통해 유입각이 크고 공동현상이 나타날수록 출력감소의 원인이 됨을 확인하였다.

하천 만곡률과 홍수량에 따른 수면경사도 산정 (Estimation of the Water Surface Slope by the River Bend Curvature and Flood Discharge)

  • 최한규;이문희;백효선;박수진
    • 한국방재학회 논문집
    • /
    • 제7권2호통권25호
    • /
    • pp.65-71
    • /
    • 2007
  • 본 연구는 만곡하천의 단면을 만곡률에 따라 1 2차원 수치해석을 실시하였다. 수치해석 결과 유 출입각에 따른 수위 편차가 발생하였으며, 홍수량 변동에 따른 편차가 증가하였다. 2차원 수치모형에 의한 수위편차를 보면 유 출입각 105도 일 때 홍수량 500CMS에서 최대경사가 6.67%가 나타났다. 우측은 90도를 초과하는 경우 1차원 수치모형과의 편차가 감소하였으며, 좌측의 수위는 105도를 초과하는 경우 1차원 수치모형과의 편차가 감소하는 것을 확인하였다. 이는 90도 이상의 만곡하천의 경우 수치해석보다는 수리모형실험을 통하여 검증하는 것이 바람직하겠다.

연락공 형상에 따른 와류실식 디젤기관의 유동 특성 수치해석 (Numerical Analysis of Flow Characteristics in Swirl Chamber Type Diesel Engine)

  • 권태윤;최경호
    • 한국자동차공학회논문집
    • /
    • 제13권4호
    • /
    • pp.49-57
    • /
    • 2005
  • In this study, in-cylinder flow of the swirl chamber type diesel engine numerically simulated by VECTIS code. The flow fields during the intake and compression process were also investigated in detail. Numerical results revealed that the generation and distortion of the swirling, tumbling vortices and those influences on turbulence kinetic energy by shape of the jet passage, angle and area. It was also found that flow characteristics were affected by inflow velocity that depends on change of the jet passage shape. Swirl ratio was increased according to decrease of jet passage area, and was affected by piston motion according to increase of jet passage angle. Tumbling vortices had the similar in various cases, but tumble ratio was increased with the inflow velocity. The generation of turbulence kinetic energy was considerably influenced by complex effects of swirling and tumbling vortices.

종합병원 병실 내 시환경 조성을 위한 광선반 길이 및 Slat각 제어에 따른 자연채광 유입 환경 연구 - 기상데이터 기반 동적 자연채광 시뮬레이션을 기반으로 - (Study on Daylight Inflow Environment Consequent on the Length of Light Shelf and Slat Angle Control for Fostering Visual Environment in Patient Rooms of Hospital - By Dynamic Daylight Simulation Using Weather Data -)

  • 조주영;이기호;이효원
    • KIEAE Journal
    • /
    • 제12권6호
    • /
    • pp.113-121
    • /
    • 2012
  • A hospital is the most important infra-facility of the places which take care of people's body in social environment. There exist several environmental factors in the ways to heal the human body in hospital ward, but this study tried to look into the improvable pleasant sickroom environment with focus on light environment among the factors. In other words, this study aims at the research on proper daylight inflow into sickroom space as basic data for understanding the link between healing environment and natural lighting. In the simulation analysis through this research, this study completed the initial simulation using Autodesk Revit 2011 with focus on two types of individual multi-bed room units of the two general hospitals located in Gwangju City. This study made a simulation analysis of The two multi-bed rooms looking to the west using the weather data on Gwangju district, which is the strong point of ECOTECT2011. Conclusively, looking into the analysis of the simulation model in time of attaching the length of in & outside light shelf, the angle controlling of light shelf, the daylight factor and DA were found to show the tendency to decrease in the numerical value due to the decrease in sunlight inflow as the simulation model moved more toward the room from the window in comparison with the existing analysis of multi-bed rooms. Particularly, this study was able to read that the daylight factor and DA were more decreasing to improve at the light shelf than the existing bedrooms; conclusively, this study judges that the natural lighting simulation analysis could be helpful in improving the healing environment as basic data.

Separation Performance of a Low-pressure Hydrocyclone for Suspended Solids in a Recirculating Aquaculture System

  • Lee, Jin-Hwan
    • Fisheries and Aquatic Sciences
    • /
    • 제13권2호
    • /
    • pp.150-156
    • /
    • 2010
  • The separation performance of a low-pressure hydrocyclone (LPH) was evaluated for suspended-solids removal in a recirculating aquaculture system (RAS). The dimensions of the LPH were 335 mm cylinder diameter, 575 mm cylinder height, 60 mm overflow diameter, 50 mm underflow diameter, and $68^{\circ}$ cone angle. The inflow rate varied (400, 600, 800, and 1,000 mL $s^{-1}$) with 25%, 25%, 20%, and 10% of bypass ($R_f$), respectively. The maximum total separation efficiency (Et) and reduced separation efficiency (E't) for suspended solids from the effluent of the second settlement tank (before biofiltration) were 58.9% and 45.2%, respectively, at an inflow rate of 600 mL $s^{-1}$ and 25% of $R_f$. The maximum Et and E't for suspended solids from the water supply channel (after biofiltration) were 24.4% and 16%, respectively, at an inflow rate of 1,000 mL $s^{-1}$ and 10% of $R_f$. The maximum grade efficiency (Ei) was 51.6% for a 300 ${\mu}m$ particle size at an inflow rate of 600 mL $s^{-1}$ with 23% of $R_f$. The maximum reduced grade efficiency (E'i) was 37.6% for a 300 ${\mu}m$ particle size at an inflow rate of 1,000 mL $s^{-1}$ with 11% of $R_f$. The results indicate that the separation performance of the LPH for suspended solids removal was size selective and that maximum removal occurred at particle sizes ranging from 300 to 500 ${\mu}m$.

축류 송풍기 허브측 불균일 유입유동 현상 및 성능 특성 (Performance Characteristics Due to the Inflow Distortion near Hub in an Axial Flow Fan)

  • 장춘만;최승만;김광용
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
    • /
    • pp.663-669
    • /
    • 2005
  • Performance characteristics of an axial flow fan having distorted inlet flow have been investigated using numerical analysis as well as experiment. Two kinds of hub-cap, round shape and right-angled front shape, are tested to investigate the effect of inlet flow distortion on the fan performance. In case of right-angled front shape, axisymmetric distorted inflow is induced by flow separation at the sharp edge of hub-cap, and the characteristics of the inflow depends on the distance between hub-cap and blade leading edge. Flow analysis of the blade passage is peformed by solving the three-dimensional Reynolds-averaged Navier-Stokes equations. numerical solutions are validated in comparison with experimental data measured by a five-hole probe downstream of the fan rotor. It is found from the numerical results that non-uniform axial inlet velocity profile near the hub results in the change of inlet flowangle. The changed inlet flow angle near the hub invokesa flow separation on the blade surfaces, thus deteriorating the fan efficiency. The effect of the distance between hub-cap and blade leading edge on the efficiency is also discussed.

  • PDF

익렬 날개 후단소음의 저감 (Trailing Edge Noise Modification in a Blade Cascade)

  • 손정민;김휘중;이승배;조성민
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.116-122
    • /
    • 2002
  • It is addressed that the turbulent broadband sound power from a sirocco fan can be modeled by the trailing edge noise. The trailing edge noise is usually influenced by inflow turbulenca separation, and boundary layer thickness on the blade. The design parameters such as solidity (c/s) and stagger angle are specified to predict performance and noise level because the separation and slip velocity are strongly affected by them along with the flow coefficient. This paper reports the effects of the stagger angle upon the trailing edge noise for various trailing edge shapes. It is believed that the serrated trailing edge provides break-up mechanism for organized convecting vortices, thereby reduce the overall noise level for every case of stagger angle.

  • PDF