• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 2001.11a
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• pp.51-56
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• 2001

정유공장으로부터 발생으로 중잔사유를 이용하는 가스화 복합발전 플랜트에 대한 공정모사를 수행하였고, 공기분리장치의 연계공정 최적화를 통해 IGCC 플랜트이 효율을 극대화하였다. 가스화 복합사이클의 발전계통을 모델링하기 위해, 본 연구는 MS7001FA 가스터빈이 공기분리장치와 연계되어 있고, 공기분리장치를 위한 공기 추출과 공기분리장치로 부터의 질소회석이 이루어진다고 가정하였다. 가스터빈의 폐열은 삼중압력의 폐열회수 증기발생장치로부터 회수하였다. 정유공장 중잔사유는 Shell 가스화 및 Sulfinol-SCOT-Claus 공정을 거쳐, 합성가스 연료를 발생시키는 것으로 가정하였다. 공기분리 장치의 연계 공정 최적 결과는 가스화 복합사이클의 효율이, 질소 회석이 없는 경우와 있는 경우에 대해, 공기추출비 20% 또는 40-60%에서 가장 우수함을 보여주었다.

• Journal of Energy Engineering
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• v.5 no.2
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• pp.160-169
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• 1996

Parametric studies are conducted for optimizing the integration design between gas turbine compressor and air separation unit (ASU) of integrated gasification combined cycle power plant. The present study adopts the ASU of double-distillation column process, from which integration conditions with compressor such as the heat exchanger condition between air and nitrogen, the amount and the pressure of extracted air are defined and mathematically formulated. The performance variations of the compressor integrated with ASU are analyzed by combining streamline curvature method and pressure loss models, and the predicted results are compared with the performance test results of actual compressors to verify the prediction accuracy. Using the present performance prediction method, the effects of pinch-point temperature difference (PTD) in the heat exchanger, the amount and the pressure of extracted air on compressor performances are quantitatively examined. As the extraction air amount or the PTD is increased, the pressure ratio and the power consumption of compressor are increased. The compressor efficiency deteriorates as the increase of the flow rate of air extracted at higher pressure level while improving at lower pressure air extraction. Furthermore, through the characteristic curve between generalized inlet condition and efficiency of compressor, optimal integration condition is presented to maximize the compressor efficiency.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.04a
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• pp.9-9
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• 1998

가스터빈 연소기의 난류유동장을 구성하는 기본적인 유동형태는 크게 밀폐관내의 돌연 확대를 가지는 동축제트, 선회유동, 그리고 연소공기공 및 회석공기공을 통해 연소실에 수직방향으로 유입되는 제트유동 등으로 분류할 수 있다. 실제 가스터빈 연소기내의 난류유동장을 수치해석하기 위해서는 임의의 형상을 갖는 3차원 유동장을 모사할 수 있는 수치해석법과 고차정확도를 유지하면서도 수렴안정성을 만족시키는 대류항 처리기법 등과 같은 수치모델의 개발이 선행되어야 하며, 이와 함께 복잡한 난류연소유동장을 정확히 묘사할 수 있는 난류모델 및 난류연소모델의 개발 및 검증이 가장 중요한 요인이 된다. 또한 가스터빈 연소기의 최적 설계는 넓은 작동구간에서 높은 효율, NOx 및 CO 배기량의 저감, 희박연소 가연한계의 확장, 연소계통에서의 낮은 압력강하, 낮은 연소벽면온도와 온도구배를 유지시키기 위한 공기에 의한 충분한 냉각 같은 서로 상충되는 설계조건을 만족해야 한다. 그리고, 이러한 상충된 연소설계조건들을 충족시키는 최적 연소기의 설계를 위해서는 실험적인 연구뿐만 아니라 연소기내의 물리적인 현상을 잘 반영할 수 있는 물리적 모델을 바탕으로 한 연소유동의 해석적인 연구를 필요로 한다. 본 연구에서는 원통형 가스터빈 연소기의 등온 및 연소유동장, 그리고 연소기와 연결되는 Scroll 내부의 난류유동장에 대한 수치해석을 수행하여 수치 및 물리모델의 예측능력을 검증하였고, 가스터빈 연소유동장 해석에 관련된 중요 논점들에 대하여 심도있게 분석하였다.

• Journal of the Korean Society of Radiology
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• v.13 no.2
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• pp.261-270
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• 2019

The separation permeation characteristics of $N_2-O_2$ gas in air at cell membrane model of skin which irradiated by high energy electron(linac 6 MeV) were investigated. The cell membrane model of skin used in this experiment was a sulfonated polydimethyl siloxane(PDMS) non-porous membrane. The pressure range of $N_2$ and $O_2$ gas were appeared from $1kg_f/cm^2$ to $6kg_f/cm^2$. In this experiment(temperature $36.5^{\circ}C$), the permeation change of $N_2$ and $O_2$ gas in non-porous membrane by non-irradiation were found to be $1.19{\times}10^{-4}-2.43{\times}10^{-4}$, $1.72{\times}10^{-4}-2.6{\times}10^{-4}cm^3(STP)/cm^2{\cdot}sec{\cdot}cmHg$, respectively. That of $N_2$ and $O_2$ gas in non-porous membrane by irradiation were found to be $0.19{\times}10^{-4}-0.56{\times}10^{-4}$, $0.41{\times}10^{-4}-0.76{\times}10^{-4}cm^3(STP)/cm^2{\cdot}sec{\cdot}cmHg$, respectively. The irradiated membrane was significantly decreased about 4-10 times than membrane which was not irradiated. And ideal separation factor of $N_2$ and $O_2$ gas by non-irradiation was found to be from 1.32 to 0.42 and that of $N_2$ and $O_2$ gas by irradiation was found to be from 0.237 to 0.125. The irradiated membrane was significantly decreased about 4-5 times than membrane which was not irradiated. When the operation change(cut) and pressure ratio(Pr) by non-irradiation were about 0, One was increased to the oxygen enrichment and the other was decreased to the oxygen enrichment. The irradiated membrane was significantly decreased about 4-19 times than membrane which was not irradiated. As the pressure of $N_2$ and $O_2$ gas was increased, the selectivity was decreased. As separation permeation characteristics of $N_2-O_2$ gas in cell membrane model of skin were abnormal, cell damages were appeared at cell.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2005.11a
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• pp.93-99
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• 2005

Performed were 2-phase numerical studies on two types of fuel atomizers, plain orifice and pressure swirl atomizer. In case of plain orifice, cavitation model was applied so that discharge coefficient, cavitation size, and magnitude of cavitation region characterized and compared with experimental results for several different pressure enforced to the orifice. In case of swirl atomizer, VOF model was applied to analyze air core size, spray angle, and wall pressure distributions with comparison of experimental results.

• Journal of Biomedical Engineering Research
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• v.19 no.4
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• pp.423-429
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• 1998

Human pharynx is unique, acting as a complex interchange between the oral cavity and esophagus, and between the nasal cavity and lungs. It is actively involved in the transport of food and liquid, producing the forces that guide that bolus into the upper esophagus and away from the adjacent larynx and lungs. This study intended to develop a biomechanical model of the human pharynx, utilizing Finite Element Method(FEM). Within each model changes in cross sectional intralumenal area were calculated and compared with the area from the computer-generated FE model. Area matching allowed estimation of intraluminal pressure gradients during swallow. The estimated pharyngeal pressure gradient varies from one region to another. The estimated pharyngeal pressure gradients showed different patterns for upper four levels and lower four levels. The contraction velocity for upper four levels is much higher than lower four levels. The higher contraction velocities and pressure gradients in the upper levels are consistent with the bolus velocities required for efficient swallow.

• Proceedings of the KIEE Conference
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• 2015.07a
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• pp.1241-1242
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• 2015

이 연구는 정전용량형 압력센서 내의 공기가 센서 성능에 미치는 영향을 줄이고자 이론적 접근과 실험적 확인을 통해 제안된 바 있는 센서 모델을, 유한요소해석 프로그램인 ANSYS로 각각의 조건에 따라 해석하여 기존에 제시 된 결과들과 비교하는 과정을 다루었다. FEA(Finite Element Analysis)결과, air chamber를 추가한 센서는 기존의 센서보다 sensitivity가 향상되었음을 확인할 수 있었다. 또한, FEA로 얻은 sensitivity 값은 이론값과 1.8%~10.1%의 차이를 보였으며, sensitivity ratio는 이론값과 실험값의 중간 정도로 나타났다.

• Journal of Korean Tunnelling and Underground Space Association
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• v.17 no.3
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• pp.319-332
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• 2015

The pressure wave formed by the piston effects of the train proceeds within the tunnel when a train enters the tunnel with a high speed. Depending on the condition of tunnel exit, the compression waves reflect at a open end, change to the expansion waves, transfer to tunnel entrance back. Due to interference in the pressure waves and running train, passengers experience severe pressure fluctuations. And these pressure waves result in energy loss, noise, vibration, as well as in the passengers' ears. In this study, we performed comparison between numerical analysis and field experiments about the characteristics of the pressure waves transport in tunnel that appears when the train enter a tunnel and the variation of pressure penetrating into the train staterooms according to blockage ratio of train. In addition, a comparative study was carried out with the ThermoTun program to examine the applicability of the compressible 1-D model(based on the Method of Characteristics). Furthermore examination for the adequacy of the governing equations analysis based on compressible 1-D numerical model by Baron was examined.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.16 no.10
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• pp.6445-6452
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• 2015

The surface of the cooling coil becomes dry, wet or partially wet depending on the operating condition. Thus, a proper design of the cooling coil should include a heat transfer analysis on dry, wet or partially wet surfaces. In this study, an elementary model, which analyzes the cooling on an elementaty basis, is proposed. Comparison of the predictions of the model with experimental data of the cooling coil revealed that heat transfer rates were predicted within 10.1%, airside pressure drop within 11.1% and sensible heat ratio within 5.7%. The model was used to investigate the effect of water circuitory on cooling coil performance.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.04a
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• pp.8-8
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• 1999

2-유체 인젝터의 분무연소에 대한 통찰 및 구조에 대한 이해와 연료-공기 혼합과 연소반응의 물리적 이해에 필요한 수치적 모델의 개발 및 검증을 위해서는 2유체 시스템에서 액체 및 기체 각각의 기본적 특성인 액적크기, 액적속도, 액적의 질량플럭스(flux), 가스상의 속도측정 등이 필요하다. 특히, 액체분무에서는 액적의 크기를 예측하는 것이 매우 중요한 과제이며, 액적의 크기에 영향을 주는 인자들로는 노즐의 형태, 분사액체의 물성치(점도, 표면장력, 밀도), 주위기체의 조건(온도, 압력, 응축과 증발현상), 분사압력 등이 있다. 그러나, 실제 분무액적의 크기는 분포를 가지므로 같은 SMD를 가지더라도 그 분포의 정도는 크게 다를 수 있어 결과적으로 분무액적의 크기를 평균값만으로 표현하는 것은 불충분할 뿐만 아니라 그 적용에도 한계를 가지게 된다. 따라서 분무액적의 평균크기와 함께 그 분포의 정도 등을 함께 나타내려는 시도가 많은 과학자들에 의하여 연구되었다.