• Journal of Aerospace System Engineering
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• v.13 no.6
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• pp.1-8
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• 2019

The synthetic turbulence generation model for inlet boundary conditions of subsonic Backward Facing Step (BFS) was investigated. The average u-velocity and Reynolds stress at inlet boundary follows experimental data. Synthetic Eddy Method (SEM), random noise, and uniform flow conditions were implemented relative to the synthetic turbulence generation method. A three dimensional Large Eddy Simulation (LES) was applied for turbulent flow simulation. Turbulent and mean flow characteristics such as flow reattachment length, velocity profiles, and Reynolds stress profiles of BFS were compared with respect to the turbulent effects.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.705-708
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• 2011

Ejector system can induce the secondary flow or affect the secondary chamber pressure by both shear stress and pressure drop which are generated in the primary jet boundary. Ejectors are widely used in a range of applications such as a turbine-based combined-cycle propulsion system and a high altitude test facility for rocket engine, pressure recovery system, desalination plant and ejector ramjet etc. The primary interest of this study is to set up an design procedure on the configuration and operating condition of multi-ejector for the various high altitude simulation.

• Journal of Energy Engineering
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• v.2 no.1
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• pp.75-82
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• 1993

A 50 ㎾ phosphoric acid fuel cell(PAFC) system using natural gas was simulated for steady state with the commercial software, ASPEN PLUS. The USER block and the FORTRAN block were prepared to simulate the cell. The changes of hydrogen yield according to the variation of several operating conditions were examined and the operating conditions to maximize hydrogen yield were obtained. The simulation results agree with the real data, which can be used to prepare the basic process data and the optimal conditions for the domestic commercial fuel cell system. H$_2$utilization rate over 50% should be maintained to achieve the efficiency of the conventional electricity generation. Energy consumption can be reduced by utilizing the heat released from the reformer and the cell which are operated at high temperatures.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.5
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• pp.100-109
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• 2003

A performacne simulation model of the PT6A-62 turboprop engine using the $SIMULINK^R$ was proposed to predict transient and steady state behaviors. The $SIMULINK^R$ has several advantages such as user-friendliness due to the GUI(Graphic User Interfaces) and ease in the modification of the computer program. The $SIMULINK^R$ model consists of subsystems to represent engine gas path components such as flight initial subsystem, compressor subsystem, burner subsystem, compressor turbine subsystem, power turbine, exhaust nozzle subsystem and integrator subsystem. In addition to subsystems, there are search subsystems to find an appropriate operating point by scaling from the 2-D components look-up table, Gasprop Subsystem to calculate the gas property precisely. In case of steady state validation, performance results analyzed by the proposed $SIMULINK^R$ model were agreed well with the analysis results by the commercial GASTURB program. Moreover in validation of the transient model, it was found that performance simulation results by the proposed model were reasonable agreement with analysis results by the well-proved computer program using FORTRAN.

• ICROS
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• v.11 no.3
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• pp.38-43
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• 2005

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.11
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• pp.927-933
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• 2020

This paper presents a fuel quantity measurement system (FQMS) for an aircraft supplementary fuel tank considering the change of aircraft attitude. The developed FQMS consists of fuel sensors, a signal process unit, an indicator and a software to estimate the fuel quantity from the sensor data. To replicate the change of the roll and pitch attitude on the ground, the test simulator is developed in this work. Using the test simulator, the sensor data at various fuel quantities, roll and pitch angles are automatically measured to build a training data set. The data-driven software to estimate the fuel quantity is then developed using a trilinear interpolation method with the training data set. The developed FQMS is verified by investigating the fuel estimation error of the test data set that we know the true values. Through the test, it is confirmed that the error of the developed FQMS system satisfies the criteria of TSO-C55 document.

• Smart Media Journal
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• v.1 no.1
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• pp.48-52
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• 2012

A reliable test of offshore plant hold a key post in offshore engineering technology. The offshore self-supporting of process module design and basic design technology needs engineering verification based on the reliable test. And also reliable verification test data is very important. Therefore, verification test system for offshore installation simulation is necessary. This paper explains design of data acquisition system and control system based on the parameter of measured and controlled variable which is for establishing offshore installation simulation system.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2001.10a
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• pp.765-768
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• 2001

A universal shipborne automatic identification system(AIS) uses self-organised time division multiple access(SOTDMA). The performance evaluation system of the SOTDMA algorithm for AIS is needed to implement it efficiently. This paper shows the method of designing it. Real ships access the VHF maritime mobile band but in this performance system, several ship objects access the shared memory. Real ships are designed as the object and the wireless communication channel is designed as the shared memory. This system shows several stations are assigned the transmission slot by the SOTDMA algorithm

• The Journal of the Korea institute of electronic communication sciences
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• v.14 no.3
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• pp.553-558
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• 2019

Global auto parts companies are making efforts to develop EWP(: Electric Water Pump) which is one of the core parts of environment friendly car. In eco-friendly automobiles, an independent cooling system is used rather than a cooling system that is linked to an internal combustion engine. Therefore, the research and development of the water pump operating separately from the engine and the related production system are being actively carried out. In order to overcome the shortcoming of EWP of PPS material suitable for injection system, G company which is a global parts company that researches and develops EWP around SUS and is in the process of developing robot-based production equipment for mass production. In this paper, a heat shock simulation system is designed and implemented that works with the robot-based production system to test the performance of the produced EWP. By using this system, it is possible to test the EWP in an virtual environment similar to the actual environment, thereby reducing the defect rate of the product. At the same time, all the data produced during the entire process for testing can be stored, which can be utilized in the future development of CPS(: Cyber Physical System) of EWP system based on big data.

• Proceedings of the Korea Society for Simulation Conference
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• 1999.10a
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• pp.144-149
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• 1999

발전소의 안정적 운영을 위한 발전소 운전원의 훈련에는 기준 발전소 주제어실의 각종 패널라 계기들을 기계적으로 동일하게 만들고 정확한 수학적 모델로 발전소 시스템을 모사한 전 범위 시뮬레이터가 주로 이용된다. 전범위 시뮬레이터는 실제 현장을 모사하는 시뮬레이션 컴퓨터와 주제어실의 패널 계기들을 연결시켜 주는 I/O 인터페이스 시스템을 필요로 한다. 기 설치 운용되고 있는 선행 호기 시뮬레이터를 보면 주 공급업체는 모델링 기술을 가지고 있는 업체가 맡고, I/O 인터페이스 시스템은 I/O 모듈과 네트웍 프로토콜까지 협력업체나 자사의 독자 모델을 취하고 있다. 그러나 I/O 모듈의 제작사가 대부분 외국의 특정 업체여서 예비품의 입수가 용이하지 않아 유지보수가 어렵고, 많은 비용을 지불해야 하는 단점을 가지고 있다. 따라서, 유지보수 용이성과 경제적 측면에서 특정 벤더 규격에 종속되지 않고 일반적인 표준을 따르는 off-the-shelf 제품을 이용하는 발전소 시뮬레이터 I/O 인터페이스 시스템의 구축이 요구된다. 본 논문에서는 화력 발전소와 원자력 발전소를 대상으로 시뮬레이터 I/O 인터페이스 시스템의 요구사양을 소개하고, 네트웍에서 시스템 아키텍처까지 개방형 인터페이스 방식의 상용 제품을 채용하는 PC기반 시뮬레이터 I/O 인터페이스 시스템 구축방안을 제시하고, 성능 예측을 통해 제안한 시스템 구축 방안의 효용성을 보인다.