• 한국태양에너지학회 논문집
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• 제23권2호
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• pp.99-105
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• 2003

This paper presents the effect of rotor geometry on the performance of a small-scale Wells turbine for wave energy conversion. In this study, four kinds the Wells turbine of blade profile were selected from previous studies. The types of blade profile included in the papers are as follows: NACA0020 ; NACA0015; CA9; and HSIM 15-262123-1576. The experimental investigations have been performed for two solidities by testing model under steady flow conditions. The effect of blade profile on the running and starting characteristics under sinusoidal flow conditions have also been investigated by a numerical simulation based on a quasi-steady analysis. In addition, the effect of sweep on the turbine characteristics has been studied for the cases of CA9 and HSIM 15-262123-1576. Based on the evaluation, a suitable choice of these design factors has been suggested. As a result, it seems that a suitable choice of the sweep ratio of 0.35 for the blade profile of the Wells turbine.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집D
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• pp.961-966
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• 2001

The Wells turbine is one of the simplest and most promising self-rectifying air turbines which are useful for the systems of alternative energy development in near future, and it is economically desirable from the point of view of the practical use, as well. To investigate the effect of blade sweep on the performance of the Wells turbine, computations of a fully 3-D Navier-Stokes are carried out under steady flow conditions of NACA0020 blade. It is known that the performance of the Wells turbine is considerably influenced by the blade sweep. An optimum blade sweep ratio(f=0.35) for the NACA0020 is found to be the most promising for the practical use, and this value is in good agreement with the previous experiments. It is also found that the overall turbine performance for the NACA0020 is better than that for the CA9.

• 전자공학회논문지D
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• 제35D권8호
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• pp.44-52
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• 1998

The theoretical modeling of transition energy and absorption coefficient for intersubband transitions in quantum wells in presented. We include, as well as hartree and exchange-correlation potentials, boht depolarization effect and exciton-like effect which play great roles in heavily doped cases where practically reasonable absorption coefficients are available. Also, the calculated results are compared with the existing experimental values for .delta.-doped Si quantum wells to check the validity of our theoretical calculation.

• 한국태양에너지학회 논문집
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• 제26권2호
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• pp.1-7
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• 2006

A numerical investigation was performed to determine the effect of airfoil on the optimum flap height using NACA0015 Wells turbine. The five double flaps which have 0.5% difference were selected. A Navier-Stokes code, CFX-TASCflow, was used to calculate the flow field of the Wells turbine. The basic feature of the Wells turbine is that even though the cyclic airflow produces oscillating axial forces on the airfoil blades, the tangential force on the rotor is always in the same direction. Geometry used to define the three dimension numerical grid is based upon that of an experimental test rig. This paper tries to disign the double flap of Wells turbine with the numerical analysis.

• 한국CDE학회논문집
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• 제9권3호
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• pp.253-259
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• 2004

A numerical investigation was performed to determine the effect of airfoil on the optimum flap height using NACA0015 Wells turbine. The five double flaps which have 0.5% difference were selected. A Navier-Stokes code, CFX-TASCflow, was used to calculate the flow field of the Wells turbine. The basic feature of the Wells turbine is that even though the cyclic airflow produces oscillating axial forces on the airfoil blades, the tangential force on the rotor is always in the same direction. Geometry used to define the three dimension numerical grid is based upon that of an experimental test rig. This paper tries In optimized disign the double flap of Wells turbine with the numerical analysis.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.616-621
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• 2001

A numerical investigation was performed to determine the effect of airfoil on the optimum flap height using NACA 0021 Wells turbine. The five double flaps which have 0.5% chord height difference were selected. A Navier-Stokes code, FLUENT, was used to calculate the flow field of the Wells turbine. The basic feature of the Wells turbine is that even though the cyclic airflow produces oscillating axial forces on the airfoil blades, the tangential force on the rotor is always in the same direction. Geometry used to define the 3-D numerical grid is based upon that of an experimental test rig. This paper tries to analyze the optimum double flap of Wells turbine with the numerical analysis.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.520-525
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• 2003

A numerical investigation was performed to determine the effect of airfoil on the optimum flap height using NACA0015 Wells turbine. The five double flaps which have 0.5% chord height difference were selected. A Wavier-Stokes code, CFX-TASCflow, was used to calculate the flow field of the Wells turbine. The basic feature of the Wells turbine is that even though the cyclic airflow produces oscillating axial forces on the airfoil blades, the tangential force on the rotor is always in the same direction. Geometry used to define the 3-D numerical grid is based upon that of an experimental test rig. This paper tries to analyze the optimum double flap of Wells turbine with the numerical analysis.

• 한국태양에너지학회 논문집
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• 제23권3호
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• pp.55-61
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• 2003

This paper represents the effect of rotor geometry on the performance of a small-scale Wells turbine for wave energy conversion. In this study, four kinds of blade profile were selected from previous studies with regard to the blade profile of the Wells turbine. The experimental investigations have been performed for two solidities by model testing under steady flow conditions, and then the effect of blade profile on the running and starting characteristics under sinusoidal flow conditions have been investigated by a numerical simulation using a quasi-steady analysis. In addition, the effect of sweep on the turbine characteristics has been investigated for the cases of CA9 and HSIM 15-262123-1576. As a result, a suitable choice of these design factors has been suggested.

• 한국심리학회지 : 문화 및 사회문제
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• 제19권2호
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• pp.159-178
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• 2013

본 연구의 목적은 배심원 제도를 사용하는 미국의 민사 모의배심 상황에서 발견된 웰스효과(Wells effect, Niedermeier, Kerr & Messé,1999; 배심원들이 통계적 증거에 기초하여 피고가 사건의 책임이 있을 주관적 확률을 높게 추론하였음에도 불구하고,유죄 평결 내리기를 주저하는 현상)가 우리나라의 민사 모의배심 상황에서도 나타나는지를 반복 검증하고, 이 효과에 대한 새로운 설명기제의 하나로서 '평결 오류 위험성 지각' 가설의 적절성을 검증하는데 있다. 먼저, 실험 1에서는 Wells(1992)의 실험에서 사용된 실험조건별 시나리오들인 '타이어자국' 조건 시나리오와 '타이어자국-믿음' 조건 시나리오를 우리나라 실정에 맞게 번안 및 수정하여 대학생 46명에게 실시하였다. 실험 1에서, 모의배심원들은 두 조건 모두에서 비슷한 정도로 피고의 유죄에 대한 주관적 확률을 높게 추정하였으나, 타이어자국-믿음 조건에 비해 타이어자국 조건에서 유죄 평결을 현저히 주저하였다. 이 결과는 실험 1이 한국 참가자를 대상으로 웰스효과를 반복 검증하였음을 의미한다. 실험 2는 웰스효과에 대한 새로운 대안적 설명을 제안하고 검증하기 위해 실시되었다. 이를 위해 실험 1에서 사용한 '타이어자국' 조건의 시나리오에 '평결 오류 위험성 지각'을 높거나 낮게 조작하는 문구를 추가한 두 시나리오를 만들어 조건별로 비교하였다. 대학생 70명을 대상으로 실험 2가 실시되었고, 그 결과로 평결 오류 위험성 지각이 낮거나 높게 조작된 조건 간에 유죄의 주관적 확률에서는 차이가 없었지만, 평결 오류 위험성 지각이 낮은 조건보다 높은 조건에서 유죄평결 비율이 유의하게 낮았다는 것을 보여 주었다. 이 실험 2의 결과는 오판으로 인해 피고가 입게 될 피해의 크기를 배심원들이 작게 지각하는 경우보다 크게 지각하는 경우에 배심원들이 유죄 평결 내리기를 꺼려하는 웰스효과가 더 강하게 나타난다는 것을 보여주었다. 본 연구의 제한점과 추후 연구에 대한 시사점이 논의에서 다루어졌다.

• 한국지하수토양환경학회:학술대회논문집
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• 한국지하수토양환경학회 2004년도 총회 및 춘계학술발표회
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• pp.503-508
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• 2004

Optimal remediation design using the pump and treat(P&T) method and natural attenuation was accomplished in consideration for degradation processes, such as sorption and first-order decay rate. Variation of both sorption and first-order decay rate has influence on design of optimal remediation application. When sorption effect increases, the more pumping rate and pumping wells are required. The location of operated wells is on the centerline of contaminant plume and wells near hot spot are mainly operated when sorption effect increases. The higher of first-order decay rate, the less pumping rate is required. These results show that the degradation processes have to be considered as one of the essential factors for optimal remediation design.