• Journal of Advanced Marine Engineering and Technology
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• 제24권1호
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• pp.127-133
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• 2000

A numerical study of the flow of incompressible fluid in a polar cavity is presented. Irregular grids is proposed by applying the interior division principle to the variables on polar coordinate grid formation. Stability analysis and the pressure correction method of SOLA algorithms were discussed in detail on cylindrical coordinates. The results present that unsteady flow behavior appears over $Re=3{\times}10^4$ on polar cavities but nearly steady state at $Re=10^4$. Furthermore, with increasing Reynolds numbers, vortices behaviors indicate more complicated flow phenomena and more severe temporal fluctuation of total kinetic energy and time variation of velocity components at arbitrary pick-up points are detected in case of $Re=5{\times}10^4$.

• Journal of Ship and Ocean Technology
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• 제4권2호
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• pp.13-23
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• 2000

A low-order potential based boundary element method is applied to the prediction of the flow around the cavitating propeller in steady or in unsteady inflow. For given cavitation number, the cavity shape is determined in an iterative manner until the kinematic and the dynamic boundary conditions are both satisfied on the approximate cavity boundary. In order to improve the solution behavior near the tip region, a hyperboloidal panel geometry and a modified split panel method are applied. The method is then extended to include the analysis of time-varying cavitating flows around the propeller blades via a time-step algorithm in time domain. In the method, the steady state oscillatory solution is obtained by incremental stepping in the itme domain. Finally, the present method is validated through comparison with other numerical results and experimental data.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.813-824
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• 2004

The paper studies the effect of neighboring blade rows on flutter characteristics of cascading blades. For this purpose the computation program to calculate the unsteady blade loading based on the un-steady lifting surface theory for contra-rotating annular cascades was formulated and coded. Then a computation program to solve the coupled bending-torsion flutter equation for the contra-rotating annular cascades was also developed. Some results of the flutter analysis are presented. The presence of the neighboring blade row gives rise to significant change in the critical flutter condition when the main acoustic duct mode is of cut-on state.

• 대한기계학회논문집B
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• 제21권5호
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• pp.670-678
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• 1997

A method to mitigate the thermal stratification phenomenon of pressurizer surge line is proposed by heating bottom outside of horizontal pipe. Unsteady two dimensional model has been used to numerically investigate an effect of heating the bottom of pipe. The dimensionless governing equations are solved by using the control volume formulation and SIMPLE algorithm. Temperature and streamline profiles of fluids and pipe walls with time are compared with the previous study result. The numerical result of this study shows that the outside heating can relaxate the thermal stratification flow of the pressurizer surge line. Maximum dimensionless temperature difference between hot and cold sections of the pipe inner wall which causes thermal stratification was reduced from 0.514 to 0.424 at dimensionless time 1, 632 and 1, 500 respectively.

• 소성∙가공
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• 제24권3호
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• pp.161-166
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• 2015

The finite element method has been widely used in the analysis of ring rolling. For ring rolling it requires a high computational expense due to the non-steady state material flow characteristics of the process. The high computational expense causes the finite element analysis to be impractical for industrial applications. In the current study, we aim to develop a practical implicit finite element modeling method for ring rolling. This method uses a step-wise steady state assumption and is called the “Stepped method”. The stepped method divides the whole process time of unsteady-state flow model into a finite number of steady-state models. It then solves the process at several specific time steps until convergence is reached. In order to confirm the performance and validity of the newly proposed stepped method, the result from the stepped method were compared to the results from a Lagrangian finite element method and to results from experiments reported in the literature.

• 한국추진공학회지
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• 제22권2호
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• pp.152-159
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• 2018

고온밸브의 비정상상태 복합열전달 해석 기법을 확립하기 위한 연구를 수행하였다. 장시간 작동하는 고온밸브의 특성과 해석의 경제성을 고려하여 두 가지 해석 기법을 제시하였다. 발달순서에 따라 구간을 나누고 구간별로 시간간격을 증가시켜 해석을 수행하는 다 구간 해석 기법과 정상상태 유동장 해석결과를 비정상상태 해석의 초기 값으로 사용하는 one-way 해석 기법을 제시 하였다. 다 구간 해석 기법의 경우 신뢰도가 높은 해석이 수행 가능하지만 경제적인 측면에서 설계 단계의 해석 기법으로는 부적합하였다. one-way 해석 기법의 경우 초기 신뢰도는 떨어지나 기민한 설계 변수 연구가 가능한 경제적인 해석 수행이 가능하였다.

• Wind and Structures
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• 제24권3호
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• pp.205-221
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• 2017

The unsteady flow field disturbance between the blades and tower is one of the primary factors affecting the aerodynamic performance of wind turbine. Based on the research object of a 3MW horizontal axis wind turbine which was developed independently by Nanjing University of Aeronautics and Astronautics, numerical simulation on the aerodynamic performance of wind turbine system in halt state with blades in different position was conducted using large eddy simulation (LES) method. Based on the 3D unsteady numerical simulation results in a total of eight conditions (determined by the relative position with the tower during the complete rotation process of the blade), the characteristics of wind pressure distributions of the wind turbine system and action mechanism of surrounding flow field were analysed. The effect of different position of blades on the aerodynamic performance of wind turbine in halt state as well as the disturbance effect was evaluated. Results of the study showed that the halt position of blades had significant effect on the wind pressure distribution of the wind turbine system as well as the characteristics of flow around. Relevant conclusions from this study provided reference for the wind-resistant design of large scale wind turbine system in different halt states.

• 폴리머
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• 제38권5호
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• pp.640-644
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• 2014

평판 디스플레이 제조공정 중의 하나인 유리기판 위에 감광액을 도포하는 과정에 슬롯코팅 방법이 많이 쓰이고 있다. 도포공정에서는 균일한 코팅 두께를 얻는 것이 중요하며, 코팅의 균일성은 노즐방향과 운전방향의 균일성으로 나뉜다. 운전방향의 코팅 균일성은 코터의 운전조건에 영향을 받고, 노즐방향의 균일성은 다이 내부의 흐름의 균일성에 영향을 받게 된다. 이러한 영향 인자들로 인해 코팅두께가 불균일한 현상이 발생하는데, 코터 진행의 초기 구간에는 비정상상태 구간으로 운전방향과 노즐방향으로 코팅두께가 균일하지 않다. 본 연구에서는 이러한 현상이 나타나는 원인을 파악하기 위해 비정상상태와 정상상태를 구별하여 해석하고 이를 실험과 비교하였다. 그 결과 감광액이 다이 내부에서 균일한 압력분포에 도달하기까지 시간이 필요하고 이로 인해 코팅 초기구간에서 다이의 양가장자리 영역의 속도가 중앙 영역에 비해 속도가 낮게 나타났으며 코팅 두께도 얇게 나타났다. 그러나 정상상태에 도달한 후에는 가장자리 영역의 속도가 중앙 영역보다 높게 나타났고 코팅 두께 역시 두껍게 나타났다.

• 소성∙가공
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• 제8권4호
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• pp.364-373
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• 1999

For material characterization of semi-solid materials, backward extrusion process, which has been used in forming of hollow-sectioned products, was analyzed by the upper bound analysis in the current study. The existing kinematically admissible velocity field was applied to steady state at which there was no change in the assumed regions of velocity field. For unsteady state, new velocity field, as a function of dead zone angle, was proposed. Through the whole analysis, fiction between die and workpiece was also considered. It has been studied how the process variables, such as friction factor and punch velocity, and material parameters, such as strength coefficient, strain rate sensitivity could affect on analysis results. Finally, by the comparison with the finite element analysis, the reliability and efficiency of the proposed velocity field were discussed.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2002년도 춘계학술대회 논문집
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• pp.278-283
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• 2002

Cooling characteristics for the three type spindles with high frequency motor are studied. For the analysis, three dimensional models are built considering heat transfer characteristics such as natural and forced convection coefficients. Unsteady-state temperature distributions and thermal deformations according to the cooling conditions are analyzed by using the finite element method.