• Solar Energy
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• v.15 no.2
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• pp.25-37
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• 1995

This paper presents an approximate analytical solution to one-dimensional model of the charging process for stratified thermal storage tanks, in which variation of the inlet temperature as well as the momemtum-induced mixing is taken into accout. The mixing is incorporated into the model as a constant-depth perfectly mixed layer above the plug flow region. Based on the superposition principle, the variable inlet temperature is approximated by a number of step functions. Temperature distributions for the thermocline corresponding to three types of interfacial condition arr successfully derived in terms of well-defined functions, so that a linear combination of them constitutes the final solution. Validity and utility of this work is examined through the comparison of the approximate solution with an exact solution available for the case of linearly increasing inlet temperature. With increasing the number of steps, the present solution asymptotically approaches to the exact one. Even with a limited number of steps, the present results favorably agree with those by the exact solution for a wide range of the mixing depth. Also, it is revealed that fewer steps are needed for meaningful predictions as the mixing. depth becomes larger.

• Journal of the Korean Institute of Gas
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• v.15 no.3
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• pp.53-57
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• 2011

The present study has been carried out to analyze the flow characteristics of a heat recovery steam generator with the change of inlet flow conditions by using numerical flow analysis. The inlet of HRSG corresponds the outlet of gas turbine exit and the flow after gas turbine has strong swirl flow and turbulence. The inlet flow condition of HRSG should be included the exit flow characteristics of gas turbine. The present numerical analysis adopted the flow analysis result of gas turbine exit flow as a inlet flow condition of HRSG analysis. The computational flow analysis result of gas turbine exit shows that the maximum axial velocity appears near circular duct wall and the maximum turbulent kinetic energy and dissipation rate exist relatively higher gradient region of axial velocity. The comparison of flow analysis will be executed with change of inlet turbulent flow condition. The first case is using the inlet turbulent properties from the result of computational analysis of gas turbine exit flow, and the second case is using the assumed turbulent intensity with the magnitude proportional to the velocity magnitude and length scale. The computational results of flow characteristics for two cases show great difference especially in the velocity field and turbulent properties. The main conclusion of the present study is that the flow inlet condition of HRSG should be included the turbulent properties for the accurate computational result of flow analysis.

• Proceedings of the Korean Nuclear Society Conference
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• 1998.05a
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• pp.425-430
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• 1998

SMART 관류형증기발생기의 유동 불안정성을 분석할 수 있는 시간영역-비선형 해석모델을 개발하였다. 해석모델은 일차계통 모델을 포함하고 있으며 이차측 튜브 양단에 일정압력 경계조건을 이용하고 내부에서는 평형 균질 이상유동 모델을 도입하였다. 기존의 정상 상태 및 임계조건에 대한 실험 결과와 개발된 해석모델 모델을 이용한 계산 결과를 비교한 뒤 임계점 이후 나타나는 진동의 특성을 분석하였다. 개발된 해석모델은 SMART 관류형증기발생기에서 발생할 수 있는 유동 진동의 특성과 영향을 파악하고 유동 불안정성을 막기 위한 입구 오리피스 설계의 목적에 활용할 수 있을 것이다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.47-52
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• 2004

In the design of scramjet intake for hypersonic flight, a variety of aerothermodynamics phenomena are encountered. These phenomena include blunt leading - edge effects, boundary layer development issues, transition, inviscid / viscous coupling, shock - shock interactions, shock / boundary - layer interactions, and flow profile effects. For intakes that are designed to operate within a narrow Mach number / altitude envelope, an understanding of a few of these phenomena might be required. In this work several predominant flowfield phenomena (viscous phenomena, boundary - layer separation, and combustor entrance profile) are discussed to investigate the performance of the intake at the altitude and angle of attack extremes of the HyShot flight experiment.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.10
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• pp.618-627
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• 2016

This study numerically analyzes the characteristics of the velocity distribution for each location of a square-sectional $180^{\circ}$ bent duct using a Reynolds Stress Turbulent model. The flow parameters were varied, including the working fluids, inlet velocity, surface roughness, radius of curvature, and hydraulic diameter. The boundary conditions for computational fluid dynamics analysis were inlet temperatures of air and water of 288 K and 293 K, inlet air velocity of 3-15 m/s, inner surface roughness of 0-0.001 mm, radius of curvature of 2.5-4.5 D, and hydraulic diameter of 70-100 mm. The working fluid characteristics were highly affected by changes in the viscous force. The maximum velocity profiles in the bent duct were indicated when the $90^{\circ}$ section was in the region of X/D=0.8 and the $180^{\circ}$ section was in the region of Y/D=0.8. Lower surface roughness and higher radius of curvature resulted in a higher rate of velocity change. Also, an efficient measuring location downstream of the bent duct is suggested since the flow deviations were the most stable when the straight duct length was in the region of L/D=30. The minimum deviations at the same velocity conditions according to the hydraulic diameter were mostly indicated in the range of L/D=15-30 based on the standard deviation characteristics.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.881-888
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• 2017

In general, the choking phenomenon occurs by flow acceleration for a turbine at high pressure ratio condition. In choking condition, total pressure ratio increases without mass flow rate variation. It is hard to predict choking characteristics by using conventional meanline analysis which used mass flow inlet boundary condition. In the present study, the algorithm for predicting choking point is developed to solve the problem. Moreover, performance estimation algorithm after choking is presented by reflecting the flow behaviour of flow expansion at choked nozzle or rotor. The analysis results are compared with 3D CFD analysis and experimental data to validate present method.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.2
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• pp.20-28
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• 2018

In general, the choking phenomenon occurs due to the flow acceleration of a turbine under high pressure-ratio. During choking, the total pressure ratio increases without any variation in the mass flow rate. It is difficult to predict choking characteristics by using conventional meanline analysis, which utilizes mass flow inlet boundary condition. In this study, an algorithm for predicting the choking point is developed to solve this problem. In addition, a performance estimation algorithm is presented to estimate the performance after choking, based on the flow behavior of flow expansion at the choked nozzle or rotor. The analysis results are compared with 3D CFD analysis and experimental data to validate this method.

• Journal of Industrial Technology
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• v.26 no.A
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• pp.29-38
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• 2006

Efficiency and universality which was the spirit of the modern age, had also an enfluence on our living environment. Various types of individual housing unit were developed and mass-produced. However, the exterior space in our city is a place for our social life and intermediate place to connect the private life of each individual to our society. For the people to adapt themselves well to their environment, it should be well organized which means it is clearly divided and integrated in a hierarchical order. To realize these conditions, adequate boundaries to divide each territory and entrances to connect each territory are two essential elements. One of the possible methods to realize these conditions can be found in korean traditional architecture where the exterior space has the same figural quality like buildings and is the center of the whole composition. Buildings, walls and colonnades are the elements to define space. Gates, pavilions, gabs between buildings and posts are the elements to symbolize the entrance connecting each space. Each exterior space is integrated to a whole composition. One is the gradual differentiation along the axis which is unique in korean traditional architecture. The other is the rectangular connection which is also found in the other area in the world. The results of this thesis are as follows. The exterior space in the housing area should have the figural quality. The elements to make boundaries defining exterior space are classified into horizontal elements such as low buildings and walls, and vertical elements such as tower-shape buildings which define space in a different way. The position of openings in a housing block affects the characteristic and openness of a exterior space. Various types of gates are used to decide the relationship between spaces.

• Proceedings of the Korea Water Resources Association Conference
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• 2021.06a
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• pp.102-102
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• 2021

광양만의 해수교환은 주로 여수해만을 통해 이루어지고, 만의 동측에는 노량수로를 통해 진주만으로의 해수교환이 일어나고 있으며, 만의 북측에는 섬진강을 끼고 있다. 광양항 건설 전 만내의 수심은 약 10 m 이내로 얕았으며, 만의 입구인 여수해만과 노량수로에서의 수심은 약 20 m 이상이었다. 광양만은 1982년 광양제철소의 건설을 시점으로 하여 광양항의 확장 개발, 폐기물처리장 건설 등으로 인한 매립이 진행되었다. 특히, 섬진강 하구는 광양만 개발 전에는 넓은 조간대 퇴적층의 발달로 다양한 생태계환경을 유지하고 있었으나, 광양항 건설 및 하구에서 모래 준설 등으로 인해 근래에 와서는 해수의 역류가 심각한 상태이다. 1982년 광양제철소 건설이후 계속적으로 광양만을 개발함으로써 해양환경에 큰 변화가 발생하였다. 따라서, 본 연구에서는 광양만 개발 전·후의 조석 및 해수유동의 변화특성을 해석하기 위해 조석 및 조류에 대한 현장관측과 3차원 해수유동 수치모형실험을 수행한 후 남해도를 둘러싸고 있는 광양만, 진주만 등의 조석 및 조류의 변동특성을 해석하였다. 광양만 개발 전·후의 해수유동의 변동특성을 해석하기 위해 김 등(1999)에 의해 개발된 3차원 layer·level 혼성 해수유동 모델을 광양만, 진주만을 포함하는 남해도 주변해역에 적용하여 30일간의 수치계산결과를 이용하여 해수유동의 변동특성을 해석하였다. 모델에서 격자간격은 동서-남북방향 동일하게 200 m, 시간간격은 20 sec, 계산영역은 동서방향으로 52 km, 남북방향으로 65 km인 260×325 격자체계로 구성 운영하였다. 외해 개방경계에서 조위는 수로국에서 관측한 조위와 본 연구에서 관측한 조위를 보간하여 사용하였다. 광양만 개발전·후의 조류의 변동특성을 수치해석한 결과 여수해만에서는 광만만 개발전이 개발 후보다 유속이 강하게 나타났으나, 노량수로에서는 개발 후가 개발전보다 유속이 훨씬 강하게 나타났다. 이와 같은 현상은 광양만 개발로 광양만으로 유입되는 조량이 감소함으로 인해 여수해만에서는 유속이 감소한 것으로 생각된다. 노량수로에서 개발 후가 개발전보다 유속이 증가한 것은 여수해만을 통해 유입한 해수가 개발 후에는 광양만의 해수면적 감소로 광양만의 서측으로 유입하는 조량이 감소한 반면에 광양만의 북측(섬진강 하구) 또는 동측(노량수로)으로 유입하는 조량이 많기 때문인 것으로 사료된다.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.3
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• pp.46-52
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• 2018

A simple Crocco's $n-{\tau}$ time delay model and linear analysis of fluid flow coupled with acoustics are combined to investigate the high frequency combustion instability in the combustion chamber of LOX/hydrocarbon engines. The partial differential equation of the velocity potential is separated into ordinary differential equations, and eigenvalues that correspond to tangential resonance modes in the cylindrical chamber are determined. A general solution is obtained by solving the differential equation in the axial direction, and boundary conditions at the injector face and nozzle entrance are applied in order to calculate the chamber admittance. Frequency analysis of the transfer function is used to evaluate the stability of system. Stability margin is determined from the system gain and phase angle for the desired frequency range of 1T mode. The chamber model with variable baffle length and configurations are also considered in order to enhance the 1T mode stability of the combustion chamber.