• Proceedings of the Korea Contents Association Conference
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• 2010.05a
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• pp.469-471
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• 2010

본 연구는 한국전통건축 중 한옥을 중심으로 건축설계물 내부의 기류현상을 분석하여 전통건축의 설계에 있어서 에너지 효율을 높이기 위한 방안을 과학적으로 검증하고자 하는 것이다. 이를 위해서 전통 건축물의 주요부재에 관한 열역학적 물성치를 대표 값으로 설정하고 물성치의 변화를 실험 결과를 활용하여 보정하여 한옥 내부의 유동장과 온도분포 예측하여 그 결과를 제시한다. 이를 통해 건축 부재의 열역학적 특성이 현대의 다양한 기능재료에 비해 열악할지라도 이를 부재간의 배치와 조합을 통해 소정의 에너지 효율을 달성한 사례를 규명할 것이다.

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.5
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• pp.1337-1348
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• 1990

Estimations of the thermodynamic properties are made for the selected binary non-azeotropic refrigerant mixtures including R13B1/R114, R22/R114, R12/R114, R152a/R114, R13B1/R152a and R13B1/R12 using the Peng-Robinson equation of state and mixing rules. In this study, we find that the binary interaction coefficients for the above mixtures have an effect upon the vapor-liquid equilibria and the thermodynamic properties. As the binary interaction coefficient becomes larger, the deviation from the idealized model, say, Raoult`s rule, is obvious. A correlation is proposed to relate the binary interaction coefficient to the difference between the dipole moments op each pure refrigerant. Vapor-liquid equilibrium are also accurately estimated using the binary interaction coefficient. Pressure-enthalpy and temperature-entropy relations are plotted for a certain composition ratio of each refrigerant mixture. Results show that the estimating method in this study can be applied to the investigation of the thermodynamic properties for the binary non-azeotropic refrigerant mixtures.

• Transactions of the Korean Society of Mechanical Engineers
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• v.15 no.6
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• pp.2189-2205
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• 1991

Thermodynamic properties of binary nonazeotropic refrigerant mixtures are estimated by using a modified Carnhan-Starling equation of state. In this study, pure component refrigerants such as R14, R23, R13, R13 B1, R22, R12, R134a, R152a, R142b, RC318, R114, R11, R123 and R113 are chosen and the thermodynamic properties of enthalpy and entropy are calculated in terms of relevant variables. The modified Carnahan-Starling equation of state is compared with the carnahan-Staring-De Santis equation of sate. Results show that the relative errors become slightly smaller with the equation of state proposed in this study. Correlations are obtained for the mixtures of which the vapor liquid equilibruim data are available to us in the literature. Those mixtures are R14/R23, R23/R12, R13/R12, R13/R11, R13B1/R22, R13B1/RC318, R12/RC138, R12/R114 and R12/R11. The binary interaction coefficients are found under the condition of minimizing the pressure deviations at the vapor liquid equiblibrium state and the estimation of the vapor liquid equilibrium for the refrigerant mixtures is done. Pressure-enthalpy and temperature-entropy diagrams are plotted for the refrigerant mixtures of specific composition.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.10
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• pp.56-60
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• 2006

It is essential to predict thermodynamic properties of combustion gas with respect to a propellant mixture ratio for the development of a gas generator for a liquid rocket engine. The present study shows the temperature measurement of exit combustion gas as a function of a mixture ratio through the series of combustion tests of a fuel-rich gas generator with liquid oxygen and Jet A-1. The measurements of dynamic and static pressures, and combustion gas temperatures allowed the estimation of thermodynamic properties like a specific heat ratio, a gas constant, and a constant pressure specific heat of the combustion gas. The comparison of the experimental results with predictions made by interpolation parameters obtained from the modification of the chemical equilibrium code indicates that the interpolation method calibrated using the temperature measurements can be utilized as an effective tool for the initial design of a fuel-rich gas generator.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.118-122
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• 2006

For the development of a gas generator of a liquid rocket engine, the prediction of thermodynamic properties of combustion gas with respect to a propellant mixture ratio becomes critical. The present study focuses on the temperature measurement of exit combustion gas as a function of a mixture ratio through combustion tests of a fuel-rich gas generator propelled by Lox/Jet A-1. The measurement of combustion dynamic and static pressures allowed indirect estimation of thermodynamic properties like specific heat ratio, gas constant, and constant pressure specific heat. Comparing the results with empirical prediction through an interpolation reveals that the interpolation method calibrated using temperature results can be utilized as an effective tool for the design of a fuel-rich gas generator.

• Journal of Energy Engineering
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• v.23 no.1
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• pp.75-80
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• 2014

The past several years have seen a substantial growth in mathematical modeling activities whose interests are to describe the performance, efficiency and emissions characteristics of various types of internal combustion engines. The key element in these simulations of various aspects of engine operation is the model of the engine combustion process. Combustion models are then classified into three categories: zero-dimensional, quasi-dimensional and multidimensional models. zero-dimensional models are built around the first law of thermodynamics, and time is the only independent variable. This paper presents a introduction to the combustion characteristics of a spark ignition combustion modeling by zero-dimensional model.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.31 no.7
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• pp.4-9
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• 2002

환경문제에 대한 관심이 높아짐에 따라, 냉동공조 산업에서 다양하게 이용되는 냉매에 대하여도 많운 시각이 집중되고 있다. 특히, 몬트리얼 의정서와 교토의정서에 의한 지구온난화 물질에 대한 규제로 CFCs와 HCFCs 냉매를 사용하지 못하게 펌에 따라 냉동공조업계에서는 열역학적 물성치가 우수하고 환경친화적인 대체냉매의 개발에 관한 연구를 활발히 진행하고 있다. 이러한 문제의 근본적인 해결책은 자연상태로 존재하는 자연냉매를 이용하는 것이디. 이산화탄소, 암모니아, 탄화수소계열, 물, 공기 등이 대표적으로 거론되고 있는 자연냉매이다. 이 중에서 도 이산화탄소는 인체에 무해하며, 독성이 없고, 화 학적으로 안정하며,기존의 냉동기 재료를 그대로 사용할 수 있는 장점이 있다. 또한 열역학적 성질 및 전달물성이 우수하고, 냉통기에 적용할 때 성능이 개선될 가능성이 많다는 점도 매우 고무적이다. 본 고에서는 최근 가장 주목을 받고 있는 이산화탄소를 이용한 냉동사이클의 특성과 성능향상 방안에 대하여 기존 연구결과를 정리하여 설명하고자 한다.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.3 no.4
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• pp.286-296
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• 1991

The thermodynamic properties of R134a, the prospective R12 alternative, have been computerized using Martin-Hou equation of state and the coefficients given by Willson-Basu. Several experimental results in literatures for PVT data, saturated vapor pressure, saturated liquid density are compared with the calculated results to investigate the accuracy. The average deviation (max. deviation) is 0.13% (0.25%) for saturated liquid density, 0.25% (0.8%) for PVT data. Thermodynamic properties, enthalpy, entropy are compared with the NIST's. The maximum percent difference is 3% for saturated liquid enthalpy, 1.5% for saturated vapor enthalpy, 4% saturated liquid entropy, and 0.7% for saturated vapor entropy. Correction of W-B's coefficients and inclusion of the sixth term of M-H EOS for improvement of accuracy are recommended. R134a and R12 are compared with respect to refrigeration performance. COP's are different from each other within 3%. Refrigeration effect of R134a is superior to that of R12 but refrigeration capacity of R134a is inferior to that of R12 because the volumetric efficiency of the system using R134a is lower than that of the system using R12.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.04a
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• pp.89-92
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• 2011

The modeling of thermodynamic non-idealities and transport anomalies is a crucial prerequisite to realistically simulate the mixing and combustion processes of liquid propellants injected above critical pressures. This study has developed a specific set of subroutines to calculate the thermodynamic and transport properties based on the generalized cubic equation of state (EoS) in a coupled manner with the standard chemical kinetics packages (Chemkin). The existing flamelet analysis code is extended with the real-fluid package and applied to numerical investigation of local flame structures of kerosene and liquid oxygen at high pressure conditions relevant to the actual rocket engines.

• Proceedings of the Korean Institute of Industrial Safety Conference
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• 1999.06a
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• pp.69-72
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• 1999

공정상에서 화재 및 폭발위험을 최소화하기 위해서는 공정의 안전과 최적화조작이 이루워 져야 하는데, 우선 작업 조건하에서 취급물질의 연소특성치 파악이 필요하다. 화학공정에 있어서 설계의 요지는 공정모사 프로그램이다. 최근에는 공정모사 프로그램에 응용하기 위해 열역학적 물성치 데이터베이스 연구에 화재ㆍ폭발 특성치 연구가 활발히 진행되고 있다. 이는 공장을 건설하기 전에 안전성 평가가 이루어져야 하기 때문이다. (중략)