• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.6
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• pp.110-117
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• 2003

The operational characteristics of the landing gear retraction/extension depend on the complexity of design variables operational/environmental conditions. In order to meet the requirements of minimum stow area and performance, the integration of the landing gear system requires operational kinematic and dynamic analysis considering an effect of its related system. This study investigates operational dynamic behaviors of the T-50 landing gear system using ADAMS. Taking into account for various operational/environmental conditions, an analysis of dynamic behavior on the landing gear operational characteristics is performed with experience derived from a wide range of proprietary designs. Analytical results are presented for discussing the effects of temperature, aerodynamic and maneuver load on normal/emergency operation of the landing gears and doors. This analysis leads us to the conclusion that the proposed program is shown to be a better quantitative one that apply to a new development and troubleshooting of the landing gear system.

• Journal of the Korean Electrochemical Society
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• v.7 no.2
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• pp.69-79
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• 2004

To correctly simulate performance characteristics of fuel cells with a modeling method, various physical and chemical phenomena must be considered in fuel cells. In this study, performance characteristics of planar solid oxide fuel cells were simulated by a commercial CFD code, CFD-ACE+. Through simultaneous considerations for mass transfer, heat transfer and charge movement according to electrochemical reactions in the 3-dimensional planar SOFC unit stack, we could successfully predict performance characteristics of solid oxide fuel cells under operation for structural and progress variables. In other words, we solved mass fraction distribution of reactants and products for diffusion and movement, and investigated qualitative and quantitative analysis for performance characteristics in the SOFC unit stack through internal temperature distribution and polarization curve for electrical characteristics. Through this study, we could effectively predict performance characteristics with variables in the unit stack of planar SOFCs and present systematic approach for SOFCs under operation by computer simulation.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.731-736
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• 2011

A pneumatic driving solenoid valve operates pneumatic control devices by opening/closing operating flow passage when the command is given by control system for the liquid-propellant feeding system of space launch vehicle. The simulation model of pneumatic driving solenoid valve is designed with AMESim to verify the designs and evaluate the dynamic characteristics and pneumatic behaviors of valve. To validate a valve simulation model, the simulation results of their operating durations of valve by AMESim analysis are compared with the results of experiments. In addition, the results of internal flow simulation with FLUENT are utilized to improve the accuracy of valve-modeling. Using the model, we analyze performance of valve; opening/closing pressure, operating time on various design factors; shape of control valve seat, drainage seat, rate of sealing diameter, volume of control cavity. This study will serve as one of reference guides to enhance the developmental efficiency of ventilation-relief valves with the various operating conditions, which shall be used in Korea Space Launch Vehicle-II.

• Journal of the Institute of Electronics and Information Engineers
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• v.52 no.5
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• pp.214-221
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• 2015

In this paper, we present robust estimation and detection algorithms for discrete-time switched linear systems whose output measurements are corrupted by noises. First, a mode estimation algorithm is proposed based on the minimum distance criterion. Then, state variables are also observed under the active mode estimate. Second, a detection algorithm is constructed to detect the mode switching of the switched system. With the boundedness of measurement noise, the proposed estimation algorithm returns the exact active mode and approximate state information of the switched system. In addition, the detection algorithm can detect the switching time within a pre-determined time interval after the actual switching occurred.

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.4
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• pp.971-980
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• 1990

본 연구에서는 실험적으로 2상 밀폐 직사각형 열사이폰 루프에 대하여 안정성 에 주된 영향을 줄수 있는 변수들, 즉 루프 경사각도, 작동유체의 유동현상을 관찰하 고 작동유체의 온도변동과 류프의 전열성능을 측정하여 열사이폰이 안정하게 작동하는 범위를 종합적으로 조사해 보았다.

• Aerospace Engineering and Technology
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• v.11 no.2
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• pp.109-116
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• 2012

A vent-relief valve performs as a safety-valve assembly for liquid propellant feeding system of space launch vehicle, which relives pressurant propellant tanks during the filling and the flight. At vent mode, valve is opened and closed by driving pneumatic pressure, and at relief mode, valve is automatically operated to set relief pressure. In this study, we have analyzed a basic layout of vent-relief valve which is designed using foreign LVs(Saturn) to satisfy requirements of Korean Space Launch Vehicle. The simulation model of vent-relief valve is designed by using the AMESim code to verify design parameters and evaluate pneumatic behaviors of valve. In this study, we performed dynamic characteristic simulations on design parameters. And we could predict opening/closing time and pressures, operating performances on design parameters. Using this results, we could suggest detail design and boundary conditions of design.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.37 no.9
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• pp.1133-1140
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• 2013

A computer model is a useful tool that provides solution via physical modeling instead of expensive testing. In reality, however, it often does not agree with the experimental data owing to simplifying assumption and unknown or uncertain input parameters. In this study, a Bayesian approach is proposed to calibrate the computer model in a probabilistic manner using the measured data. The elasto-plastic analysis of a pyrotechnically actuated device (PAD) is employed to demonstrate this approach, which is a component that delivers high power in remote environments by the combustion of a self-contained energy source. A simple mathematical model that quickly evaluates the performance is developed. Unknown input parameters are calibrated conditional on the experimental data using the Markov Chain Monte Carlo algorithm, which is a modern computational statistics method. Finally, the results are applied to determine the reliability of the PAD.

• The Journal of the Korea Contents Association
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• v.15 no.12
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• pp.185-192
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• 2015

This study analyzed the spatial interrelation between living wages and economic variables and how they operate based on systems thinking theory to understand what value living wages have as policy instruments and why they are necessary. Results from this study can be summed as follows. First, the relationship between living wages and economic variables shows close interaction at a considerable level. In particular, mutual feedback which connects to laborers' standards of living, consumption, business, and economy was operating closely. Second, largely three positive (+) feedback loops were operating in the feedback structure of living wages and economic variables. This can be interpreted to mean that positive economic variables which are associated with living wages have the possibility of growth. Also, it can mean that the minimum wage system did not fully fulfill its role. Through these study results, it can be learned that living wages have sufficient value as a policy means and that it is advisable to allow living wages to exceed simple application levels in the public sector to expand into the private sector, to bring positive change to the economic system.

• Journal of Energy Engineering
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• v.4 no.3
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• pp.354-363
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• 1995

차세대 연료전지인 용융탄산염 연료전지의 운전조건을 확립하기 위하여 운전변수와 단위전지 성능과의 관계를 살표보았다. 용융탄산염 연료전지에 산화제로 공기를 사용하는 경우 양극가스에 질소가 포함된다. 그리고 연료전지의 작동압력을 높이면 출력을 크게 할 수 있다. 그리하여 본 연구에서는 에너지 및 물질수지를 이용하여 양극가스내 질소 조성과 작동압력 변화에 따른 전지내의 온도분포 및 성능변화를 구하였다. 본 연구팀이 이미 발표한 용융탄산염 단위 연료전지의 전류밀도의 온도분포를 구하기 위한 수치모사가 이용되었다. 가스흐름의 형태는 십자류를 선택하였다. 양극가스내 질소의 영향은 냉각효과로 나타났다. 작동압력이 증가할수록 전지의 성능은 증가하였고, 기전력[mV]변화 대 압력[atm]의 상용대수값의 변화(즉, ΔV 대 Δ(log))의 1차함수 그래프 기울기는 79.9로 문헌상의 실험치와 유사하게 나타났다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.10a
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• pp.15-15
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• 1999

램 가속기에 대한 연구는 램 가속기의 작동 조건이 고온, 고압, 초고속이라는 점과 가속기 내부에서 급격한 화학반응이 수반된다는 특성으로 인하여 실험과 해석상의 상당한 어려움이 존재한다. 램 가속기는 작동 모드에 따라 탄체 후방의 열적 질식 조건을 이용한 열적 질식 모드(Thermally Choked Mode)와 탄체 표면에 형성되는 데토네이션파를 이용한 초폭굉모드(Superdetonative Mode)로 나뉘어진다. 본 연구는 초폭굉 모드로 작동하는 램 가속기의 작동 성능 향상을 위한 방법으로 수치 최적화 기법을 이용한 램 가속기 내부 예 혼합기의 조성비 최적화를 수행하였다. 설계 변수로는 수소와 질소의 조성비를 선정하였으며, 최적 설계 목표는 일정한 질량과 형상을 갖는 탄체를 초기속도 2500m/s에서 3000m/s로 가속시키기 위하여 필요한 최소 램 가속관의 길이로 정하였다. 본 연구에서는 구베법에 기반한 Simplex 방법 및 SLP(Sequential Linear Programming)등의 수치 최적화 기법을 적용하였고, 가속기 내부의 유동장은 해석의 효율성을 고려하여 이차원 비점성 유동으로 가정하였고, 비평형 화학반응 해석을 수행하였다.