• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1995년도 추계학술대회 논문집
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• pp.470-473
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• 1995

There exist two critical in application of the magnetic bearing system. One is the control axis interference caused by gyroscopic effect and the other is the vibration caused by the unbalance on the rotor. To solve both problems at the same time, first, a centralized full-state feedback controller based on the LQR control theory was designed to compensate for the gyroscopic effect. Second, disturbance rejection control input based on the observer was designed to avoid the vibration causer by the unbalanced rotor. Balancing input computer accroding to LQR and output of the observer were derived in term of rotational speed. Effectiveness of the on-line balancing was verified through numerical simulation. The developed observer-based controller was also applied to the linear and nonlinear magnetic bearing systems.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1987년도 전기.전자공학 학술대회 논문집(II)
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• pp.954-957
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• 1987

This paper proposes a kind of function-concentrated signaling service equipment structure, in which various kind of signaling service are efficiently made for call processing control. Based upon the typical switching system models, a philosophical study on the capacity, features of structure in world systems, and interfaces with peripheral equipments has been performed in order to provide the rationale on the merits or efficiency of the proposed digital signaling service equipment.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2000년도 추계학술대회논문집B
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• pp.410-415
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• 2000

Slip factor is defined as an empirical factor being multiplied to theoretical energy transfer for the estimation of real work input of a centrifugal compressor. Researchers have tried to develop a simple empirical model, for a century, to predict a slip factor. However most these models were developed on the condition of design point assuming inviscid flow. So these models often fail to predict a correct slip factor at off-design condition. In this study, we summarized various slip factor models and compared these models with experimental and numerical data at off-design condition. As a result of this study, Wiesner's and Paeng and Chung's models are applicable for radial impeller, but all the models are not suitable for backswept impeller. Finally, the essential avenues for future study is discussed.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집B
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• pp.658-663
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• 2001

In this study, the axial-compressor design and performance/flow analysis program is developed. A mean-line analysis was used to determine optimum arrangement of overall geometry and its off-design performance is predicted by stage-stacking method. Three dimensional blade shape is generated using radial equilibrium equation and vortex methods. Various blade shape is generated and their performance is compared. Finally the quasi-three dimensional flow analysis is applied to investigate the detailed flow phenomena.

• 기계저널
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• 제18권3호
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• pp.25-32
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• 1978

1973년 석규파동 이후 세계 각국은 에너지 문제를 심각하게 다루어 왔다. 화석 연료의 유한성은 미래의 세계 에너지에 대한 연구에 박차를 가해왔다. 현재 사용되는 연료로는 화석연료인 석탄, 석유, 그리고 원자력등이 있다. 그러나 이들은 모두 그의 매장이 어느지역에 제한된 지역편재성이 있는 것이며 그의 사용에 따른 대기오염, 환경오염등의 점차적으로 큰 문제로 대두되고 있다. 본 연구에서는 과거 71년부터 77년까지의 기상조건을 중심으로 하여 기온, 수평면 일사량, 운량, 일조시간에 대한 전반적인 조사를 근거로 이에대한 통계를 제시하고, 이들의 상호관계에 대한 일 반적인 식을 유도하였다. 그리고 1977년 8월부터 78년 3월까지의 수령면 일사량과 서울 지방에서 최적치라고 알려진 53도 경사면에서의 전 일사량을 측정하여 이에 대한 자료를 제시함으로써 국 내에서의 태양열 이용에 대한 기초자료를 마련하였다. 이어서 주어진 집열기에 의한 태양열 주택 의 설계와 이에따른 경제성 타당 검토를 하고자 하였다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.496-501
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• 2003

Reynolds averaged Wavier-Stokes simulations based on the Reynolds stress model was performed to investigated the effect of inlet flow angle on the distributions of the Reynolds stress tensor inside tip leakage vortex of a linear compressor cascade. Two different inlet flow angles ${\beta}=29.3^{\circ}$(design condition) and $36.5^{\circ}$(off-design condition) were considered. Stress tensor analysis, which transforms the Reynolds stress into the principal direction, was applied to show an anisotropy of the normal stresses. Whereas the anisotropy was highest in the region where the tip leakage vortex collides the suction side of the blade and tip leakage flow enters between blade tip of the pressure side and the endwall, it had the lowest value at the center of tip leakage vortex. It was also found that the magnitude of maximum shear stress at design condition was greater than that of off-design condition.

• 한국농촌건축학회논문집
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• 제17권3호
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• pp.81-88
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• 2015

The aim of this study is to provide readers with the development strategies in terms of the Ancient Capital Plan through its status analysis and field survey. In particular, This study is expected to contribute to establish reasonable policies and prepare with development strategies of ancient capital Buyeo. The followings are specific conclusions : Firstly, Ancient Capital Preservation Plan and boundaries of district designation should be reasonably adjusted. Secondly, The relevant Act Ancient Capital Preservation and Promotion should be revised corresponding to the present state. Thirdly, exclusive organization should be established and kept consistently to produce experts. Fourthly, strategies for revitalizing Historical and Cultural Environment are required for the future. Fifthly, it should be mentioned how Cultural heritage and people in region should co-exist. Therefore life benefit and welfare for the peoples should follow. Sixthly, the commercial environment and cultural tourism environment should be improved.

• 한국유체기계학회 논문집
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• 제17권5호
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• pp.27-36
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• 2014

This paper presents a numerical investigation of the effect of the rotation speed on the performance in a transonic axial compressor with the dihedral stator. Four stator geometries with different stacking line variables were tested in the flow simulations over the whole operating range. It was found that a large shroud loss at the rotor outlet and the subsequent shroud corner separation in the stator passage occurred at low mass flow rate with the 100 % design speed. The hub dihedral stator could suppress the shroud loss region and consequently improve the stall margin. In case of the 70 % design speed condition as the mass flow rate decreased, it was seen that the high loss region was placed at the midspan of the rotor passage. The dihedral stator slightly affected the local diffusion factor, but the performance of the compressor was not changed.

• 대한기계학회논문집B
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• 제32권2호
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• pp.83-91
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• 2008

A three-dimensional computation was conducted to understand effects of the low Reynolds number on the performance in a low-speed axial compressor at the design condition. The low Reynolds number can originates from the change of the air density because it decreases along the altitude in the troposphere. The performance of the axial compressor such as the static pressure rise was diminished by the separation on the suction surface with full span and the boundary layer on the hub, which were caused by the low Reynolds number. The total pressure loss at the low Reynolds number was found to be greater than that at the reference Reynolds number at the region from the hub to 85% span. Total pressure loss was scrutinized through three major loss categories in a subsonic axial compressor such as the profile loss, the tip leakage loss and the endwall loss using Denton#s loss model, and the effects of the low Reynolds number on the performance were analyzed in detail.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2002년도 유체기계 연구개발 발표회 논문집
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• pp.258-263
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• 2002

A numerical analysis using 2-D unsteady compressible program is conducted to explain characteristics of rotating stall such as rotating speed and number of stall cells in an one-stage axial compressor. Unlike an axial compressor which has only a rotor, in one-stage axial compressor a rotating stall is generated by rotor/stator interaction and tack pressure rising without any artificial disturbance and modeling. As a back pressure is raised, the separation of suction side at blades is increased uniformly, but because of the discrepancy of blockage effect by stator, the disturbances are generated to form a stall cell. Once the stall cell is formed, regularly the stall cell are rotating through rotor blades. When the speed of rotor is design speed the rotating speed of stall cell is $83.3\%$ of rotor rotating speed. When the speed of rotor is $80\%$ of design speed, the speed of rotating stall is $88.2\%$ of rotor speed. The number of generated stall cell are also varied for rotor speed and back pressure.