• 제목/요약/키워드: Stagger Angle

검색결과 38건 처리시간 0.023초

Influence of Blade Profiles on Flow around Wells Turbine

  • Suzuki, Masami;Arakawa, Chuichi
    • International Journal of Fluid Machinery and Systems
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    • 제1권1호
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    • pp.148-154
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    • 2008
  • The Wells turbine rotor consists of several symmetric airfoil blades arranged around a central hub, and the stagger angle is 90 degrees. These characteristics simplify the total construction of OWC type wave energy converters. Although the Wells turbine is simple, the turbine produces a complicated flow field due to the peculiar arrangement of blades, which can rotate in the same direction irrespective of the oscillating airflow. In order to understand these flows, flow visualization is carried out with an oil-film method in the water tunnel. This research aims to analyze the mechanism of the 3-D flows around the turbine with the flow visualization. The flow visualization explained the influence of attack angle, the difference between fan-shaped and rectangular wings, and the sweep angle.

축류형 팬의 저소음화에 관한 연구 (A Study on the Noise Reduction of Axial Flow Fan)

  • 오재응;이승종;이상환;이동익;김철환
    • 설비공학논문집
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    • 제7권1호
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    • pp.142-149
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    • 1995
  • Axial fans are very useful cooling devices being widely used in many electric and industrial machinery. However those are often accompanying annoying noise. Many efforts have been devoted in order to reduce the fan noise. In this study, the procedure was devided into two major parts in considering effects of design parameters of axial fan concerned with noise ; the fan theory and the Fukano's fan noise study. By using the fan theory we defined stagger angle, camber angle, blade inlet and outlet angle for studying low noise fan. Then the effects of such angles on the flow rate and static pressure were investigated. By using the Fukano's fan noise theory, the relations of the chord length, the rotational speed and the number of blades vs. fan noise are investigated.

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디퓨저 베인각의 변화에 따른 압축기 성능 특성 (Compressor Performance with Variation of Diffuser Vane Inlet Angle)

  • 배명형;신유환;김광호;김진형
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 1999년도 유체기계 연구개발 발표회 논문집
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    • pp.55-60
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    • 1999
  • A centrifugal compressor was tested with three different diffusers with plate vanes. The vane inlet angle was varied from 15 to 30 dog. The higher static pressure rises are obtained with lower vane stagger angle. In the stable region the static pressure field in vaneless space is very sensitive to flow rate. The impeller has a stabilizing effect over the whole stable operating range. The diffuser has a stabilizing effect at high flow rate but is destabilizing at low flow rate.

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케스케이드 날개 후단소음 특성에 관한 연구 (A Study on Trailing Edge Noise from a Blade Cascade in a Uniform Flow)

  • J. M. Son;Kim, H. K.;Lee, S.
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문초록집
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    • pp.366.1-366
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    • 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 turbulence, separation, and boundary layer 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 strong1y affected by them along with the flow coefficient. (omitted)

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Parametric Studies and Performance Analysis of a Biplane Micro Air Vehicle

  • Maqsood, Adnan;Go, Tiauw Hiong
    • International Journal of Aeronautical and Space Sciences
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    • 제14권3호
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    • pp.229-236
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    • 2013
  • This paper presents the experimental investigation of a biplane micro air vehicle. The effects of geometric parameters, gap, stagger, and decalage angle are investigated at low Reynolds number (~150,000) in a low-speed wind tunnel. A rigid flat plate with an aspect ratio of one and square planform shape is used to evaluate all three geometric parameters. The side dimension of the single flat plate is 0.15 m. The goal is to find an optimal biplane configuration that should exceed monoplane performance by generating high lift and flying as slow as possible, in order to capture high-quality visual recordings. This configuration will directly help to fly at a lower velocity and to make tighter turns that are advantageous in restricted environments. The results show that the aerodynamic performance of the biplane MAV is significantly enhanced through the combination of gap and stagger effects. A performance comparison demonstrates the superiority of the optimal biplane configuration compared to a monoplane in cruise and glide phases. Moreover, no significant compromise is found for the range, endurance, and climb performance.

실시간 자동화 진단을 위한 전차선 검측시스템 (Catenary Measurement System for Real-Time Automated Diahnosis)

  • 김정연;박종국;이병곤;홍현표
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2011년도 정기총회 및 추계학술대회 논문집
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    • pp.1020-1026
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    • 2011
  • 전차선은 철도 전기차량에 전기를 안정적으로 공급하기 위한 시설물로서, 차량이나 외부요인에 의한 전차선의 변형 및 파손을 검지하여 전기철도 시설물 규정에 따라 최적의 상태로 유지해야 할 필요성이 있다. 본 논문에서는 전차선 마킹을 위한 라인레이저와 고속카메라 간에 기하학적 구성을 이용하여 3차선 거리측정방식으로 전차선 높이와 편위를 측정하기 위한 시스템 개발에 관하여 기술하였다. 전차선 거리 측정방법은 이미지 상에 마킹된 전차선 프로파일의 픽셀위치를 삼각함수 기법을 적용하여 카메라와의 전차선간에 각도를 계산하였으며, 카메라는 랜즈 왜곡 및 심도, 원금감 등에 따라 측정대상에 대한 픽셀 해상도가 다르므로 전차선 위치변화에 따른 픽셀당 각도 분해능을 적용하였다. 또한 전차선은 조가선과 급전선등과 같은 다른 전기배선보다 가장 아래에 설비되어 있는 특징을 이용하여 FPGA 상에서 전차선에 마킹된 레이저 프로파일 데이터를 고속으로 추출하여 처리하였다. 개발시스템은 전차선 시설물 평가기준에 따라 전차선 높이, 편위 측정데이터를 실시간 분석하여 이상구간에 대한 실시간 자동화 진단기능을 수행토록 하였다.

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받음각이 큰 평판 채널 내의 역류 유동 가시화 (Reverse Flow Characteristics in a channel with fixed angle of attack following variable width and stagger)

  • 최승;손창현;고다
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2006년도 추계학술대회 논문집
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    • pp.11-16
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    • 2006
  • Reverse flow occurs in a channel when there is an obstruction at the entry, However it has been shown recently that reverse flow can be realized without an obstruction, by staggering the sides of the channel and placing it at an angle of attack to the oncoming flow. In this study the latter flow is computationally investigated. And the mechanism is investigated using PIV (Particle Image Velocimetry) method. The results have captured all the essential features of this complex phenomenon and show the time dependent pumping mechanism which leads to the occurrence of reverse flow.

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해류발전 로터의 개발 (Development of Current Generation Rotor)

  • 조철희;김경수;민경훈;정광식
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2002년도 춘계학술대회 논문집
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    • pp.75-79
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    • 2002
  • In this research, a design guideline of current generating rotor and acceptable field rotor in offshore environment is proposed. To design rotor model, wind mill rotor design principles and turbine theories were applied based on a field rotor experimental data. To verify the compatibility of the rotor design method and to analyze the properties of design factors, 3 rotor models were designed and experimented in a circular water channel. Three rotor models were designed according to different blade numbers and blade shapes. With various flow velocities and rotor rpm, the rotor power and efficiency were measured and the properties of rotor were estimated. The results can be effectively applied to the design of current generation rotor.

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수평축 해류발전 로터의 설계와 성능해석 (Study on HAT Current Generation Rotor)

  • 조철희;김경수;민경훈;양태열;이현상
    • 한국해양공학회지
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    • 제16권1호
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    • pp.58-63
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    • 2002
  • In this research, a design guideline of current generating HAT rotor and acceptable field rotor in offshore environment is proposed. To design HAT rotor model, wind mill rotor design principles and turbine theories were applied based on a field HAT rotor experimental data. To verify the compatibility of the rotor design method and to analyze the properties of design factors, 3 rotor models were designed and experimented in a circular water channel. Three rotor models were designed according to different blade numbers and blade shapes. By changing flow velocity, rotor rpm, the rotor power and efficiency were measured and the properties of rotor were estimated. The results can be effectively applied to the design of current generation rotor.

Performance Improvement of High Speed Jet Fan

  • Choi, Young-Seok;Kim, Joon-Hyung;Lee, Kyoung-Yong;Yang, Sang-Ho
    • International Journal of Fluid Machinery and Systems
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    • 제3권1호
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    • pp.39-49
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    • 2010
  • In this paper, a numerical study has been carried out to investigate the influence of jet fan design variables on the performance of a jet fan. In order to achieve an optimum jet fan design and to explain the interactions between the different geometric configurations in the jet fan, three-dimensional computational fluid dynamics and the DOE method have been applied. Several geometric variables, i.e., hub-tip ratio, meridional shape, rotor stagger angle, number of rotor-stator blades and stator geometry, were employed to improve the performance of the jet fan. The objective functions are defined as the exit velocity and total efficiency at the operating condition. Based on the results of computational analyses, the performance of the jet fan was significantly improved. The performance degradations when the jet fan is operated in the reverse direction are also discussed.