• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 추계 학술대회논문집
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• pp.61-64
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• 2004

To analyze the performance of Wind turbine of the drag force type, 3-D RANS equations were solved by the iterative time marching method on sliding multiblock grid system. The numerical flow simulations by changing blade number and pitch angle were carried out : blade number = 15, 20 circumferentially; pitch angle = $30^{\circ},\; 50^{\circ}$ radially. The torque coefficient was also calculated.

• 한국유체기계학회 논문집
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• 제9권2호
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• pp.7-12
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• 2006

This study is to develop a system of electric power generation utilizing the wind resources available in the domestic wind environment. We tested drag-type vortical wind turbine models, which have two different types of blades: a flat plate and circular arc shape. Through a performance test, conditions of maximum rotational speed were found by measuring the rpm of wind turbine. The rotational speed was measured by a tachometer in a wind tunnel and the tunnel wind speed was by using a pilot-static tube and a micro manometer. The performance test for a prototype was accomplished by calculating power, power coefficient, torque coefficient from the measurement of torque and rpm by a dynamometer controller From the measurements for miniature turbine models with two different blades, the circular arc shape was found to Produce a maximum rotational speed for the same wind velocity condition. Based on this result, the prototype with the circular arc blade was made and tested. We found that it produces 500W at the wind velocity of 10.8 m/s and the power coefficient was 20%.

• 한국항공우주학회지
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• 제40권8호
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• pp.655-661
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• 2012

본 연구에서는 비정렬 중첩 혼합 격자계를 사용하는 전산유체기법으로 무베어링 로터허브의 공기역학적 항력을 계산하였다. 동체와 로터 허브 모두 점성 항력보다는 압력 항력이 주요 요소로 작용하고 있으며, 토크 튜브의 항력이 허브 항력에서 가장 큰 비중을 차지하고 있음을 확인할 수 있었다. 허브 항력은 동체 항력 대비 39~41%를 차지하는 것으로 나타났다. 최종적으로 개발된 헬리콥터의 항력 추세와의 비교를 통해, 설계된 무베어링 로터 허브의 항력은 요구도를 충족시키는 것으로 확인되었다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제6권2호
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• pp.269-281
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• 2014

This paper examines the suitability of using the Computational Fluid Dynamics (CFD) tools, ANSYS-CFX, as an initial analysis tool for predicting the drag and propulsion performance (thrust and torque) of a concept underwater vehicle design. In order to select an appropriate thruster that will achieve the required speed of the Underwater Disk Robot (UDR), the ANSYS-CFX tools were used to predict the drag force of the UDR. Vertical Planar Motion Mechanism (VPMM) test simulations (i.e. pure heaving and pure pitching motion) by CFD motion analysis were carried out with the CFD software. The CFD results reveal the distribution of hydrodynamic values (velocity, pressure, etc.) of the UDR for these motion studies. Finally, CFD bollard pull test simulations were performed and compared with the experimental bollard pull test results conducted in a model basin. The experimental results confirm the suitability of using the ANSYS-CFX tools for predicting the behavior of concept vehicles early on in their design process.

• 항공우주기술
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• 제11권1호
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• pp.19-26
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• 2012

무베어링 로터 허브시스템 개발에서 할당된 공기역학적 허브 항력 요구도를 분석하여, 요구도에서 제시된 방법으로 입증 가능하도록 요구도를 구체화 시켰다. 초기 허브 형상에 대해 공력계수에 기반하여 항력 예측을 수행하였으며, 요구도 충족을 위한 설계 변경안을 제시하였다. 최종 형상에 대해 전산유체기법을 사용하여 항력 예측을 수행하였으며, 그 결과 구체화된 요구도를 만족시킴을 확인할 수 있었다. 또한 기 개발된 헬리콥터의 추세선으로부터 유추할 수 있는 허브 항력의 범위 내에 있음을 확인할 수 있다.

• 드라이브 ㆍ 컨트롤
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• 제17권1호
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• pp.76-80
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• 2020

• Tribology and Lubricants
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• 제35권2호
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• pp.123-131
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• 2019

This study characterizes the coastdown performances of two small electric motors supported on high-speed ball bearings (BBs) and gas foil bearings (GFBs), and it predicts their acceleration performances. The two motors have identical permanent magnetic rotors and mating stators. However, the shaft of the GFBs has a larger mass and polar/transverse moments of inertia than that of the BBs. Motor coastdown tests demonstrate that the rotor speed decreases linearly with the BBs and nonlinearly with the GFBs. A simple model for the BBs predicts a constant drag torque and linear decay of speed with time. The test data validate the model predictions. For the GFBs, the hydrodynamic lubrication model predictions reveal that the drag torque increases linearly with speed, and the speed decreases exponentially with time. The predictions agree very well with the test data in the speed range of 100-30 krpm. The boundary lubrication model predicts a constant drag torque and linear decay of speed with time. The predictions agree well with the test data below 15 krpm. Mixed lubrication occurs in the speed range of 30-15 krpm. Rotor acceleration performances are predicted based on the characteristics of deceleration performances. The GFBs require more time to reach 100,000 krpm than the BBs because of their larger shaft polar moment of inertia. However, predictions for the assumed identical polar moment of inertia reveal that the GFBs have a nearly identical acceleration performance to that of the BBs with a motor torque greater than $0.03N{\cdot}m$.

• 항공우주시스템공학회지
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• 제17권1호
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• pp.10-15
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• 2023

덕티드팬의 동력절환장치인 클러치의 마찰판 사양을 최적설계하고 그 결과를 분석하였다. 클러치는 기계적 잠금장치의 적용 여부에 따라 2가지 방식으로 구분하고 각자의 설계 조건 하에 최적화 되었다. 클러치를 최적 설계하기 위한 인자로 전달토크 용량, 마찰재 면압, 마찰면의 온도 및 드래그 토크 등을 계산하였고, 클러치 분리판의 부피와 드래그 토크의 최소화를 최적설계의 목적함수로 활용하였다. 기계적 잠금장치가 포함되지 않은 Type 1의 경우 덕티드팬의 피치각에 상관없이 클러치의 작동이 가능하지만, 기계적 잠금장치가 포함된 Type 2에 비해 마찰면의 외경이 약 2배정도 증가하였고, 부피는 약 5~7배, 드래그 토크는 약 7~12배 정도 증가하였다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제6권4호
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• pp.965-980
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• 2014

This paper presents a new estimation method of full scale propulsive performance for the pulling type podded propeller. In order to estimate the drag of pod housing, a drag velocity ratio, which includes the effects of podded propeller loading and Reynolds number, is presented and evaluated through the comparison of model test and numerical analysis. By separating the thrust of propeller blade and the drag of pod housing, extrapolation method of pod housing drag to full scale is deduced, and correction method of propeller blade thrust and torque to full scale is presented. This study utilized the drag coefficient ratio of the pod housing as a measure for expanding it to full scale, but in order to increase the accuracy of performance evaluation, additional study is necessary on the method for the full scale expansion via separating the drag of pod body, strut and fin which consist the pod housing.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1992년도 하계학술대회 논문집 B
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• pp.659-661
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• 1992

This paper deals with aerodynamic problems of the rotating blade of Darrieus wind turbine and its instantaneous torque. The instantaneous torque varying with the rotating angle of blade was obtained through resultant wind velocity, angle of attack, lift and drag coefficient. These are obtained from a given wing section, size and wind velocity.