• 제목/요약/키워드: Wake capturing characteristics

검색결과 5건 처리시간 0.017초

비정상 후류가 선형터빈익렬의 유동 및 열전달에 미치는 영향에 관한 연구 (Influence of the Unsteady Wake on the Flow and Heat Transfer in a Linear Turbine Cascade)

  • 윤순현;심재경;김동건
    • 대한기계학회논문집B
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    • 제25권2호
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    • pp.164-170
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    • 2001
  • The influence of unsteady wake on the flow and heat transfer characteristics in a four-vane linear cascade was experimentally investigated. The unsteady wake was generated with four rotating rectangular plates located upstream of the cascade. Tested inlet Reynolds number based on chord length was set to 66,000 by controlling free-stream velocity. A hot-wire anemometer system was employed to measure turbulent velocity components. For the convective heat transfer coefficients measurement on turbine blade surface, thermochromic liquid crystal and gold film Intrex were used. It was found that the unsteady wake enhances the turbulent motion in the cascade passage and accordingly promotes the development and transition of boundary layer. It was found that the heat transfer coefficients on the blade surface increase as the plate rotating speed increases. However, the increasing of heat transfer coefficients is not significant in the case that Strouhal number is higher than 0.503.

사각주 후류가 선형터빈익렬의 유동 및 열전달에 미치는 영향에 관한 연구 (Influence of the Wake Behind Rectangular Bars on the Flow and Heat Transfer in the Linear Turbine Cascade)

  • 윤순현;심재경;우창수;이대희
    • 대한기계학회논문집B
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    • 제23권7호
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    • pp.864-870
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    • 1999
  • An experimental study Is conducted in a four-vane linear cascade in order to examine the influence of the wake behind rectangular bars on the flow and heat transfer characteristics. Flow and heat transfer measurements are made for the inlet Reynolds number of 66000(based on chord length and free-stream velocity). Turbulent intensity and stress are measured using a hot-wire anemometer, and to measure the convective heat transfer coefficients on the blade surface liquid crystal/gold film Intrex technique is used. Each of experimental cases is characterized by the unsteadiness measured at the entrance of the cascade. The wake behind the rectangular bars enhances the turbulent motion of the flow in the cascade passage. It also promotes the boundary layer development and transition. The results show that heat transfer coefficients on the blade surface increase with increasing unsteadiness.

정지 비행하는 로터 블레이드의 전산 유체-구조 결합 해석 (Computational analysis of coupled fluid-structure for a rotor blade in hover)

  • 김해동
    • 한국항공우주학회지
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    • 제36권12호
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    • pp.1139-1145
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    • 2008
  • 로터 블레이드의 구조변형을 포함한, 제자리 비행하는 로터 블레이드의 공력해석을 수행하였다. 와류포획능력을 향상시킨 전산유체 코드와 간단한 오일러-베르누이 보 모델에 기반을 둔 구조역학 방정식을 결합시켜 회전익 유동에 대한 연계 계산을 수행하였으며 계산결과 타당한 로터블레이드 구조변형 및 공력특성을 얻었다.

원주 후미에 부착된 와동발생기의 영각 변화에 따른 유동 및 열전달 특성 (Flow and Heat Transfer Characteristics due to the Variations of the Angle of Attack at the Vortex Generators located behind a Circular Cylinder)

  • 하홍영;홍철현;양장식;이기백
    • Journal of Advanced Marine Engineering and Technology
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    • 제26권4호
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    • pp.439-449
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    • 2002
  • Experimental investigations of the flow structure and heat transfer enhancement in a channel with a built-in circular cylinder and a wing-let type vortex generator are presented. Without any vortex generators, relatively low heat transfer takes place in the downstream of the circular cylinder where is a recirculation region with low velocity fluid is formed. However with a wing-let type longitudinal vortex generator in the wake region behind the cylinder, heat transfer in the region can be enhanced. In order to control the strength of longitudinal vortices, the angle of attack of the vortex generators is varied from $20^{circ} to 45^{\circ}$, but spacings between the vortex generations are fixed to be 5 mm. The 3-dimensional mean velocity field downstream of the vortex generator is measured by a five-hole pressure probe, and the hue-capturing method using thermochromatic liquid crystals has been used to provide the local distribution of the heat transfer coefficient. The vorticity field and streamwise velocity contour are obtained from the velocity field. Streamwise distributions of averaged Stanton number on the measurement planes show very similar trends for all the experimental cases($\beta=20^{circ}, 30^{circ} and 45^{\circ}$). Circulation strength and heat transfer coefficient have the maximum values when the angle of attack($\beta$) is $30^{\circ}$.

풍력 발전기의 Rotor-Blades 회전체 시스템 공력 해석 (Analysis of Flows around the Rotor-Blades as Rotating Body System of Wind Turbine)

  • 김동진;곽승현;이경호
    • 한국해양공학회지
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    • 제23권5호
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    • pp.25-31
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    • 2009
  • The most important component of wind turbine is rotor blades. The developing method of wind turbine was focused on design of rotor blade. By the way, the design of a rotating body is more decisive process in order to adjust the performance of wind turbine. For instance, the design allows the designer to specify the wind characteristics derived by topographical map. The iterative solver is then used to adjust one of the selected inputs so that the desired rotating performance which is directly related to power generating capacity and efficiency is achieved. Furthermore, in order to save the money for manufacturing the rotor blades and to decrease the maintenance fee of wind power generation plant, while decelerating the cut-in speed of rotor. Therefore, the design and manufacturing of rotating body is understood as a substantial technology of wind power generation plant development. The aiming of this study is building-up the profitable approach to designing of rotating body as a system for the wind power generation plant. The process was conducted in two steps. Firstly, general designing and it’s serial testing of rotating body for voltage measurement. Secondly, the serial test results above were examined with the CFD code. Then, the analysis is made on the basis of amount of electricity generated by rotor-blades and of cut-in speed of generator.