• Journal of Mechanical Science and Technology
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• 제14권9호
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• pp.1013-1019
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• 2000

A numerical investigation was performed to determine the effect of the Gurney flap on a NACA 23012 airfoil. A Navier-Stokes code, RAMPANT, was used to calculate the flow field about the airfoil. Fully-turbulent results were obtained using the standard ${\kappa}-{\varepsilon}$ two-equation turbulence model. The numerical solutions showed that the Gurney flap increased both lift and drag. These results suggested that the Gurney flap served to increase the effective camber of the airfoil. The Gurney flap provided a significant increase in the lift-to-drag ratio relatively at low angle of attack and for high lift coefficient. It turned out that 0.6% chord size of flap was the best. The numerical results exhibited detailed flow structures at the trailing edge and provided a possible explanation for the increased aerodynamic performance.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2000년도 춘계학술대회논문집 - 한국공작기계학회
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• pp.607-612
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• 2000

A slitter, also called a roll slitter or rewinding machine, is a sort of machinery to cut sheet materials in rolls continuously in the longitudinal direction. Recently slitter line users have requiring higher wuality and precision in products in addition to high productivity. In this paper, on effect of clearance on shear planes in slitting of S.K.B(shrinkage Bnad) is performed by using finite element method. The results obtained are as follows: (1)Load stroke curves show decreasing maximum force when increasing the clearance. (2)Effective strain decreases when the clearance increases. (3)Deformation is concentrated along the very narrow shear band.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 춘계학술대회논문집; 경주코오롱호텔; 22-23 May 1997
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• pp.594-601
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• 1997

Propeller fans are commonly equipped in outdoor units of air-conditioners to provide effective cooling in a dried heat exchanger. A new design technique was developed to satisfy requirements of aerodynamic and aeroacoustic performance, which employs the intersection method of two cylinders for mean camber line. Three proto-types of propeller fan including Palm-Shaped, Highly-Swept(PSHS) fan (proto 3)were not only to provide low lift forces for dipole sound, but also to reduce the organized tip vortices interacting with the fan guide causing narrow-banded rotating instabilities. Cross-correlation technique was applied to study flow noise source characteristics for three proto-type fans designed. The cross-correlations between a microphone at far field and a hot-wire sensor at near field show that flows near hub region of proto 3 fan are less organized and the flow structures especially at high flow rate coefficients for proto 3 fan are less correlated with noise generated than other proto-types fans.

• 산업기술연구
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• 제20권B호
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• pp.71-76
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• 2000

A numerical investigation was performed to determine the effect of the Gurney flap on NACA 0015 airfoil. A Navier-Stokes code. FLUENT, was used to calculate the flow field about the airfoil. The fully-turbulent results were obtained using the standard ${\kappa}-{\varepsilon}$ two-equation turbulence model. The numerical solutions showed the Gurney flap increased both lift and drag. These results suggested that the Gurney flap served to increase the effective camber of the airfoil. Gurney flap provided a significant increase in lift-to-drag ratio relatively at low angle of attack and for high lift coefficient. It turned out that 0.75% chord size of flap was best. The numerical results exhibited detailed flow structures at the trailing edge and provided a possible explanation for the increased aerodynamic performance.

• International Journal of Fluid Machinery and Systems
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• 제6권2호
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• pp.105-112
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• 2013

The application of contra-rotating rotors for higher specific speed pump has been proposed in our studies, which is in principle effective for reducing the rotational speed and/or the pump size under the same specification of conventional axial flow pump. In the previous experiments of our prototype, the cavitation inception at the tip region of the rear rotor rather than that of the front rotor and the strong potential interaction from the suction surface of the rear rotor blade to the pressure surface of the front one were observed, indicating the possibility to further improve the pump performance by optimizing rotational speed combination between the two rotors. The present research aims at the design of rear rotor with lower rotational speed. Considering the fact that the incoming flow velocity defects at the tip region of the rear rotor, an integrated inflow model of 'forced vortex' and 'free vortex' is employed. The variation of maximum camber location from hub to tip as well as other related considerations are also taken into account for further performance improvement. The ideas cited above are separately or comprehensively applied in the design of three types of rear rotor, which are subsequently simulated in ANSYS CFX to evaluate the related pump performance and therefore the whole low speed design idea. Finally, the experimental validation is carried out on one type to offer further proofs for the availability of the whole design method.

• 수산해양기술연구
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• 제42권4호
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• pp.217-227
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• 2006

This research aims at establishing the application of canvas kite to the fishing gear through the analysis of the lift/drag tests of the kites have been performed in our previous finding. Now that several methodologies were designed to find the most effective triangular model as a buoyancy device applied to the fishing gear. Comparisons of drag/lift were made by installing the model in an installation frame instead of the prototype. Also, we have considered the application of canvas kite to the prototypic fishing gear by calculation using the result of this test. The results obtained from the above approaches are summarized as follows, where attack angle, lift coefficient, maximum lift coefficient and drag coefficient are denoted as $B,\;C_L,\;C_Lmax\;and\;C_D$ respectively. The camber showed a gradual increase with an increase of fluid velocity. There was a big discrepancy in B=20 unlike B=30. Even if the kite retreats along the fluid flow, there is little relationship with the velocity variation. Lifts calculated with the kites were bigger and drags were smaller than those of the calculations with the float only. The kite as the buoyancy device will be very useful when the appropriate applications and the stability are met.

• 콘크리트학회논문집
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• 제26권3호
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• pp.267-275
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• 2014

최근 곡선교 사용이 증가함에 따라 기존 곡선 교량의 한계점을 극복하고자 PSC 곡선 주형을 이용한 곡선교에 대한 해석적 연구가 활발히 진행되고 있다. 그러나 기존의 프레임 요소를 이용한 격자해석방법으로는 PSC 곡선교에 대한 정밀해석이 어렵다. 이에 따라 이 연구에서는 PSC 곡선교의 정밀 유한 요소 해석을 실시하여 프리캐스트 PSC 곡선교의 설계를 위한 참고자료로 사용하고자 한다. 이를 위하여 3차원 솔리드 요소를 사용한 모델링을 실시하고, 거더 수, 하중 재하 위치, 단면 변화, 긴장력 변화 및 편긴장력 도입 여부와 같은 매개변수에 대한 거동을 평가하였다. 해석 결과 경간장 50 m 3주형 교량의 항복하중과 파괴 하중이 경간장 40 m 2주형 교량에 비해 200% 이상의 성능을 보였고, 외측거더에 하중을 가하였을 경우 도심의 위치에 따라 하중저항력 및 거더 간의 처짐 편차가 낮게 평가되는 것으로 나타났다. 또한 거더 단면을 변화시킨 경우 단면의 증가에 따라 구조성능이 향상되는 것으로 나타났으나 PS도입량의 변화에 의한 효과에 비해 경제성과 시공성에서 불리한 것으로 나타났다. PS 도입량 변화에 따른 영향을 분석한 결과 PS 도입량이 증가함에 따라 솟음량과 하중저항력이 비례하여 증가하였으며 거더 간 처짐 편차가 줄어드는 경향을 보였다. 또한, 편긴장력을 도입하였을 시 도입량 증가에 비례하여 내외측 거더 모두에서 하중저항력이 증가하며, 특히 외측거더에 편긴장력이 도입되었을 때 더 우수한 성능을 보이는 것으로 나타나, PSC 곡선교의 경제성 및 안정성을 확보하는데 효율적인 것으로 나타났다.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2010년도 춘계 학술대회 제22권1호
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• pp.39-40
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• 2010

건물이 대형화 고층화되어 감에 따라서 층고를 절감시킴과 동시에 장스팬을 구현할 수 있는 부재에 대한 요구가 늘어가고 있다. 비록 많은 연구자에 의해서 층고절감과 장스팬에 대한 요구를 만족시키기 위한 연구가 진행되고 있지만, 여전히 두 가지 요구사항을 동시에 만족시키는 효율적인 시스템이 부족한 실정이다. 본 연구에서 제안하는 파형웨브를 가진 프리스트레스 합성보는 시공성과 구조적인 성능을 동시에 향상시킬 수 있다. 시공과정에서 발생할 수 있는 비대칭 하중에 상대적으로 작은 부재를 가지고 강한 저항성을 발휘하여 시공성을 높일 수 있으며, 또한 동바리와 서포트 등의 가설부재를 줄임으로써 경제성도 확보할 수 있다. 파형웨브는 아코디언효과를 만들기 때문에 프리스트레스의 도입효율이 좋아져 더 큰 상향치올림를 유발시켜 부재의 처짐을 줄일 수 있다. 5개의 실험체를 제작하여 제안한 합성보의 효율성을 검토하였는데 그 주요한 변수로는 웨브와 플렌지에 용접된 형태와 drape point의 개수이다. 실험을 통하여 제안한 프리스트레스 합성보가 기존에 프리스트레스를 도입하지 않은 합성보 보다 큰 휨강성과 휨강도를 발휘한다는 것을 증명하였다.