• 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.

• 대한토목학회논문집
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• 제14권6호
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• pp.1465-1474
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• 1994

직립벽(直立壁) 전면(前面)에 중복파(重複波)가 작용할 때 직립벽에 설치된 수로(水路)에 발생하는 비정상류(非定常流) 흐름을 Fourier 전개기법의 비선형(非線形) 중복파 이론을 적용하여 해석하였으며 그 결과를 수리실험(水理實驗)을 통하여 검증하였다. 전반적으로 비선형이론은 선형이론(線形理論)과 비교하여 수로(水路)내의 유량변화를 더 잘 예측함을 확인하였다. 투수성(透水性)의 분석결과 수로내 유량변화의 폭은 파고(波高), 주기(週期)가 클수록, 수로연장(水路延長)이 짧을수록 커짐을 확인하였으며 이들간의 상관관계를 명확히 파악하기 위한 무차원(無次元) 관계식을 제시하였다. 수로의 해수교환기능(海水交換機能)과 직접 관련이 있는 일주기당(一週期當) 평균수량(平均水量)은 수로가 수면하(水面下) 바닥 근처에서는 음방향(陰方向)의 값이 나타날 수 있음을 이론과 실험을 통하여 확인하였고, 최대(最大) 수량(水量)은 입구(入口)가 정수면(靜水面)에 위치하는 수로에서 발생함을 보였다. 아울러, 중복파의 주기가 길수록 그리고 수로의 연장이 짧을수록 해수교환 효과면에서 유리함을 확인하였다.

• 한국생산제조학회지
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• 제8권4호
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• pp.38-44
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• 1999

This paper primarily directed toward analyzing the frequency response in hydraulic pipe lines with a small diameter. The exact solution to the frequency response is obtained by using the complicated transfer function. The discrepancy with the exact and the approximate is small so the approximation solution is adopted to compare the experimental results with the theoretical analysis. In this experiment the input frequency was generated by the frequency generator with the ball valve and speed controller. In order to compare the theoretical were forms with the experimental ones the trace obtained from the oscilloscope is photographed, The diameter the length of lines and input pressure amplitude are varied to investigate their effects,. the experiment results show that th values of dimensionless parameter are very affected to the phase delay and guide response time in the design of pressure manifold to measure the pressure of hydraulic pipelines.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집E
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• pp.416-421
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• 2001

This paper presents the numerical prediction of sound generated by viscous flow past a circular cylinder. The two dimensional flow field is predicted using FEM based Reynolds-averaged Navier-Stokes solver, and the calculated unsteady fluid field values are utilized by an acoustic code that implements Ffowcs Willianms-Hawkings(FW-H) equation. The integration surface used in acoustic analysis is extended from the cylinder surface to permeable surfaces. The 2D based CFD calculations overpredict the acoustic amplitude, however, if adequate correlation length is used, the predicted acoustic amplitude agrees well with experiment. The predictions using extended integral surface in FW-H equation show results that contain the characteristics of quadrupole - volume integration - noise term, and do not vary seriously with the integral surface location.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2001년도 추계학술대회 논문집
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• pp.227-231
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• 2001

Analysis of two-dimensional unsteady flows with a free surface in a rectangular container subject to a linear reciprocating force is performed by numerical and experimental methods. FVM is used for the numerical computation of the two-dimensional flows. We consider the surface tension as well as the viscous/elastic properties of the free surface. One-dimensional analysis as well as experiment is used in establishing the free surface properties. The steady recirculatory flow is visualized by a laser sheet. It is shown that the one-dimensional analysis provides useful informations associated with the free surface properties.

• The Journal of the Acoustical Society of Korea
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• 제20권4E호
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• pp.17-23
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• 2001

To develop the code of predicting flow-field and aeroacoustic noise by an electrical cable, a combined CFD-Acoustic analogy approach is selected. The two dimensional, unsteady and incompressible Reynolds-averaged Navier-Stokes solver with κ-ω and κ-ω SST turbulence modeling is used to calculate the near flow-field around an electric cable. Near-field results are then coupled with two-dimensional Curle's integral formulation based upon Lighthill's acoustic analogy with the assumption of acoustic compactness. To validate this code, numerical results are compared with experimental data for a circular cylinder. The simulation shows an overprediction on acoustic amplitudes, but overally speaking, the spectrum pattern of sound pressure agrees well with experiment within an acceptable amount of error. In addition, a few cross-sections of the cable were selected and tested with each other in terms of drag and radiated noise

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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• pp.113-119
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• 2001

Interaction of flow through an Impeller and a Vaned Diffuser in Centrifugal Compressor was investigated using the 3-dimensional Wavier-Stokes solution method. To consider the interaction effect of impeller and vaned diffuser, Inlet boundary conditions are imposed with the results of the steady calculation of the impeller and rotates with time. The results have been compared to steady computation results and experiment. From this, it is discussed about the compatability of the method and the advantage and disadvantage of the steady calculation.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2002년도 학술대회지
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• pp.557-560
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• 2002

In this study, simulation of weak shock waves are peformed by a two-dimensional thermal fluid or compressible fluid model of the lattice Boltzmann method. The shock wave represents an abrupt change in fluids properties, in which finite variations in pressure, internal energies, and density occur over the shock thickness. The characteristics of the proposed model with a simple distribution function is verified by calculation of the sound speeds, and the shock tube problem. The reflection of a weak shock wave by wedge propagating in a channel is performed. The results agree well with those by finite difference method or by experiment. In the simulation of unsteady shock wave diffraction around a sharp corner, we show a flow field of vortical structure near the comer.

• 대한기계학회논문집B
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• 제27권5호
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• pp.628-634
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• 2003

We present numerical and experimental results of periodic flows inside a rectangular container under a background rotation. The periodic flows are generated by changing the speed of rotation periodically so that a time-periodic body forces produce the unsteady flows. In numerical computation, a parallel-computation technique with MPI is implemented. Flow visualization and PIV measurement are also performed to obtain velocity fields at the free surface. Through a series of numerical and experimental works, we aim to clarify, if any, the fundamental reasons \ulcornerf discrepancy between the two-dimensional computation and the experimental measurement, which was detected in the previous study for the same flow model. Specifically, we check if the various assumptions prerequisite for the validity of the classical Ekman pumping law are satisfied for periodic flows under a background rotation.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2008년도 추계학술대회A
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• pp.1566-1569
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• 2008

The flow visualization is conducted in order to investigate an unsteady flight characteristic of a model dragonfly. The flapping wings are analyzed using smoke-wire and high speed camera. The results of this experiment show that three mechanisms and high incidence angle of the wings are responsible for the lift. The leading edge vortex, which is induced by the rapid acceleration of the wing at the beginning of a stroke, causes the lift enhancement. The delayed stall during the stroke and the fast supination and pronation of the wing near the end of each stroke are also responsible for the lift generation.