• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1995.05a
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• pp.123-128
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• 1995

고등기술연구원에서 수행하고 있는 IGCC 연구프로그램의 일부로 이루어지고 있는 석탄가스연소가스터빈 시스템의 공정개발을 위한 해석체계를 소개하였고, 지금까지 이루어진 해석결과들을 제시하였다. 본 해석체계는 가스터빈 시스템해석을 위한 사이클해석. 구성요소인 압축기, 연소기, 터빈에 대한 해석모듈들로 구성하였으며, 각 해석모듈은 구성요소에 대한 전문적인 열유동장 해석방법을 채택한다. 각 해석모듈간의 상호작용 및 해석결과들의 종합을 통하여 IGCC용 가스터빈 공정개발을 위한 기초적인 자료제공이 가능하다.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.14 no.4
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• pp.703-710
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• 1994

A nonlinear FEM analysis of steel members under very-low-cycle loading has been performed in conjunction with experimental works. This analysis is an FEM tracing toward cracking of steel members under cyclic loads such as a strong earthquake. After verifying the procedure by comparing global hysteretic behaviors from the analytical and experimental results, the local stress-strain hysteresis at critical sections for large cyclic deformations was traced by the numerical analysis. Local strain history was discussed in relation to cracking. Based on the experimental and analytical results, a new approach to seismic safety assessment for steel members was proposed in this paper.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.6
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• pp.104-110
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• 2018

Operating mode analysis of a liquid propellant rocket engine(LRE) is a crucial tool through the development of an engine. The operating mode analysis of an engine based on a collection of the acceptance tests of components shows discrepancies when compared to the test results. We propose a correction method for performance parameters to develop an engine analysis model for the gas generator cycle of an LRE. In order to simulate engine behavior, the performance parameters for the analysis model are tuned based on the test results of the 75tf engine of KSLV-II.

• Journal of Energy Engineering
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• v.10 no.2
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• pp.105-113
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• 2001

지구환경문제와 에너지문제를 해소하는 한 방법으로서 Vuilleumier 사이클 기관(VM)을 이용한 공조기형 열구동형 히트펌프시스템(VMHP)이 각광을 받고 있다. VMHP의 제작에 있어서는 VM의 각 부분의 이론적 검토 및 최적설계를 위한 해석프로그램의 개발이 필수적이고 최적설계를 위한 설계 기본서의 도출 및 설계자료의 확보가 필요하다. VMHP의 상세한 성능해석이나 설계에 활용 가능한 성능해석프로그램을 개발하였다. 해석은 VM의 시스템의 각 부분을 11개 부분으로 나누어 단열모델해석으로 수행하였다. 열교환기에서의 열전달 성능과 재생기손실, 열전도손실, 셔틀손실, 유동에 의한 압력손실과 열압축측과 열펌프측 사이의 마찰손실, 피스턴실 및 로드실의 마찰손실을 고려한 해석을 수행하였다. 해석에 의한 계산치의 정확성을 본 해석결과를 이용하여 제작한 시험기에 의해 비교하였다. 계산치와 시험기에 의한 전체성능을 비교하였고 또한 각각의 손실에서 고유한 파라미터를 추출하여 그 파라미터의 변화에 따른 열손실 전체의 변화 정도를 파악하여 실험치와 계산치의 정상적인 비교로부터 성능해석의 정도를 비교하였다. 비교결과에 의해 난방능력은 8%, 냉방능력은 19%의 최대오차로서 본 해석결과가 VMHP의 설계를 위해 유용한 수단으로 사용될 수 있음을 확인하였다.

• Journal of Advanced Marine Engineering and Technology
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• v.33 no.8
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• pp.1100-1106
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• 2009

Recently, there are quite a lot of attention is drown on the researches related to of Miller method applied high expansion cycle. For this study, high expansion cycles are formed and analyzed with the base view point of thermodynamics, and the features of each factors are also investigated. As a result of analysis, the expansion-compression ratio is expected with a decrease of effective compression ratio as intake valve closing time retarded, however, the decrease of mean effective pressure and its output is accompanied with the counterflow of intake air. Accordingly, as the consequence of such failure, it is expected that an alternative is needed for the realization of high expansion cycles, and the improvement over thermal efficiency. To materialize such cycle, the control system to delay the closing time of intake valve was designed and VVT, the 3 S/B low speed diesel engine, is applied to evaluate the efficiency. The result of the trial shows that there was no significant errors.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2012.05a
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• pp.52-57
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• 2012

A liquid rocket system consists of a combustion chamber, a gas generator, a turbo pump, and a turbine, etc. Each component is connected by supply components such as valves, pipes, and orifices. Since each component has a combined effect on engine performance, preliminary analysis for overall system must be required before the conceptual design stage. Comprehensive analysis program considered the supply system has not been developed yet. In this paper, a supply component model of the liquid rocket engine has been designed after verification of each component. The gas generator cycle with supply components has been composed. The results of the cycle has been compared to those of the F-1 engine with the representative gas generator cycle.

• Journal of Korea Society of Industrial Information Systems
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• v.4 no.1
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• pp.68-76
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• 1999

The intuitive understanding of the dynamic pattern generation in asymmetric networks may be useful for developing models of dynamic information processing. In this paper, dynamic behavior of the ring connection neural network in which each neuron is only to its nearest neurons with binary synaptic weights of ±1, has been inconnected vestigated Simulation results show that dynamic behavior of the network can be classified into only three categories: fixed points, limit cycles with basin and limit cycles with no basin. Furthermore, the number and the type of limit cycles generated by the networks have been derived through analytical method. The sufficient conditions for a state vector of n-neuron network to produce a limit cycle of n- or 2n-period are also given The results show that the estimated number of limit cycle is an exponential function of n. On the basis of this study, cyclic connection neural network may be capable of storing a large number of dynamic information.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.3
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• pp.58-66
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• 2019

In this study, the start-up characteristics of a staged combustion engine were analyzed numerically based on relational equation modeling of the entire engine components. The start-up characteristics were extensively analyzed considering the transient period of the total engine system from the start-up sequence till the steady-state of the engine. The performance characteristics of the engine components such as RPM of engine power-pack, chamber pressure and O/F ratio of pre-burner, and mass flow of propellants in the start-up period were investigated. Furthermore, the calculated engine data were compared satisfactorily with the experimental data. Through the comparison of data, successful validation of present engine start-up analysis has been obtained.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.5
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• pp.18-25
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• 2008

A performance analysis program has been developed for the gas generator cycle liquid rocket engine. This program predicts the system performance with the performances of subsystems which are evaluated by the models based on another analyses or experiments. The analysis method has been validated by comparing the engine performance against the published conceptual design. The performance models of the subsystems have been verified to give reasonable results by comparing with the MC-1 engine design and the system analysis of 10 ton thrust engine. The system performance of the 30 ton thrust rocket engine using LOx/Jet-A1 has been presented as an application example.

• Transactions of the Korean Society of Mechanical Engineers
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• v.10 no.1
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• pp.150-156
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• 1986

A Rankine cycle including heat exchange processes in the steam generator has been analyzed by the concept of available energy. The operation condition of the cycle can be expressed with the evaporation temperature, and there exists an optimum power condition at which the thermal efficiency of the cycle is almost the same as that of the Carnot cycle at the maximum power condition. The mass flow rate of the working fluid increases sharply as the evaporation temperature approaches to the critical point, and the regenerative system is needed to operate the cycle at the maximum power condition.