• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.388-391
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• 2017

In this study, heat transfer analysis of variable thrust control system have been conducted by using commercial CFD code and FEM code. We Carried out computational fluid dynamics analysis to obtain the temperature and convective heat transfer coefficient of hot gas of variable thrust control system. Data are used as boundary condition for heat transfer analysis using mapping method. Temperature of O-ring for sealing was predicted

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.28 no.5
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• pp.347-358
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• 1999

암모니아는 독성, 가연성 및 동 재질의 부식성 등의 단점은 있지만 CFC계 냉매가 개발되기 전에는 우수한 열역학 및 열전달 특성 때문에 냉매로서 가장 많이 사용되어져 왔다. 미국에서는 약120년, 일본에서는 약 80년 전부터 암모니아가 냉동 사이클에 사용되었고, 따라서 축적된 관련 기술 수준도 놀고 경험도 많은 편이다. 지금도 미국에서는 상업용 냉동기의 80% 정도가 암모니아를 냉매로 사용하고 있다. 우리나라도 냉동창고 냉동용으로는 암모니아 시스템이 널리 사용되고 있다.

• Journal of Power System Engineering
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• v.10 no.1
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• pp.90-95
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• 2006

Pneumatic control systems have been mainly used as a high speed operating system. Therefore, state change of air in a control volume was assumed to be adiabatic change and, pneumatic control systems have been analyzed by using this assumption. Especially, when absolute value of pressure change in the control volume is small, there is a tendency to neglect effect of temperature change on pneumatic control system because temperature change owing to pressure change is small. In this study, an effect of temperature change of air on the decompression control process was analyzed by considering change of mass flow rate, and heat transfer characteristics between air in the chamber and the chamber wall. As a result, this study could confirm that a slight temperature change of the air in the pneumatic pressure control system can influence on the dynamic characteristics of pressure response, and pressure control performance.

• Journal of the Korean Society of Propulsion Engineers
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• v.17 no.2
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• pp.24-30
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• 2013

To guarantee the exact control of missile warhead, it is inevitable to ensure the stabilities in the view points of structural and fluid/thermo dynamics of the rocket motor. Specially, despite of shortness in operating time of the rocket motor which is initial turning type of missile, it occurs frequently some problems of ablation at the neighborhood of the nozzle throat, with the result that the system itself gets to failure. In these connections, in the present study, the effect of the operating time of a rocket motor on the coefficient of convective heat transfer at the nozzle wall is investigated by numerical analysis. As a result, it is turned out that the heat transfer coefficient is largest at the just ahead of nozzle throat and decreases with the increase of operating time of the rocket motor. Furthermore, we found that the radius of curvature of throat becomes smaller, the maximum coefficient of convective heat transfer becomes larger.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.11
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• pp.934-939
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• 2012

In this study, the performance validation of a PAO-AIR heat exchanger developed for the ECS(Environmental Control System) of a UAV(Unmanned Aerial Vehicle) has been carried out. The performance goals of a PAO-AIR heat exchanger were established by the system schematic analysis. And a heat exchanger to be met the ECS performance was developed by a detailed design and a precision manufacture. Using the developed heat exchanger, the experiment about pressure loss and effectiveness, overall heat transfer coefficient to prove the developed PAO-AIR heat exchanger performance in various conditions as well as a design point of heat exchanger was performed and the experimental results were analyzed. As the experimental results, the performance and characteristic of a PAO-AIR heat exchanger developed for the ECS of a UAV were analyzed and the development suitability was proved.

• Journal of the KSME
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• v.32 no.8
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• pp.685-690
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• 1992

가전제품의 제조와 관련된 열공학문제를 몇가지 예를 들어 검토하여 보았다. 제품은 강도가 커야 하고 설계공차 내에 들어야 하는 등의 조건을 만족함과 아울러, 그의 생산공정은 가급적으로 쉬워야 하고 재료를 절감할 수 있어야 한다. 제조공정 중의 열공학적인 과정이 제품 구조내의 열응력분포를 결정지우므로 열전달과정의 세심한 제어가 필요하다. 근래에 들어 컴퓨터의 발달로 열전달과정의 수치해석이 제조장비의 설계와 제조과정의 최적제어의 보조수단으로 등장하고 있다. 실제의 문제에서는 대부분 삼차원형상을 가지고 있고, 시스템을 고려하여야 하므로 여러 가지 현상이 연계되어 있다. 그러므로 수치계산에는 여전히 종래의 실험기법에 의한 실험식들과 여러 가지 축적된 경험의 도움을 필요로 한다. 이러한 측면에서 볼 때, 종래의 실험식, 경험식, 물성치, 기존의 수치해석의 결과 등을 컴퓨터에 데이터베이스(data base)화하여 소위 전문가 시 스템(expert system)을 구축하는 편이 단순히 공정의 극히 일부분 현상들을 수치해석하는 작업 보다 선행되어야 함이 바람직할 수 있다. 또한, 가전제품의 제조에는 열공학 또는 열전달현상에만 따로 주의를 기울이지 말고, 재질의 선택, 그의 유변학(rheology), 구조내의 균열문제 등을 연계 하여 고려하여야 한다.

• The Journal of the Korea institute of electronic communication sciences
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• v.9 no.11
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• pp.1291-1296
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• 2014

The thermoelectric cooler is receiving great interest because of advantages such as the precise temperature control capability, the compact and lightweight cooler, and the mechanical vibrationless structure which enhances the reliability compared with the existing vapor compression cooler. However, it is not easy to design the optimal thermoelectric cooler which appropriate to the application because the thermal analysis should be necessary required. Accordingly, this paper studies the methodology of the modelling, sizing and thermal analysis of the thermoelectric cooler using SINDA/FLUINT analysis tool.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.36 no.12
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• pp.1177-1183
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• 2012

This study aims to develop a system that maximizes the radiative heat transfer from the heliostat to the receiver by using the configuration factor and a solar tracking device. As the heat transfer from the heliostat to the receiver is delivered by solar radiation, the configuration factor commonly utilized for radiation is applied to control the heliostat. Tracking the sun and calculating its position are possible by using an illuminance sensor (CdS) and Simulink. By applying optimized algorithms programmed using Simulink that maximize the configuration factors among the heliostat, receiver, and sun in real time, the solar absorption efficiency of the receiver can be maximized. Simulations were performed on how to change the angle required to control the elevation and azimuthal angle of the heliostat during the daytime with respect to various distances.

• Journal of the Korean Society of Propulsion Engineers
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• v.9 no.1
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• pp.9-16
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• 2005

Jet vane is an useful component which is installed at the end of a nozzle for the purpose of the posture control and the secure controlling stability during the initial launching of a rocket. During several seconds from its initial launching moment, the JV driving part is heated due to the direct contact of the vane with the combusted gas and the vane is ablated mechanically or chemically. In this study, as the fundamental study for the thermal analysis of jet vane, the heat transfer into a jet vane which is located in the uniform supersonic flow field is calculated. For this, boundary layer integral method and finite difference method are used simultaneously. Based on the thermal boundary conditions derived from the analysis, the transient heat conduction in the vane is also calculated.

• Journal of the Korean Institute of Gas
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• v.21 no.1
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• pp.72-79
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• 2017

The operating temperature range of the natural gas pipeline in Arctic environment would be controlled primarily to optimize gas throughput and to minimize the environmental impact resulting from operation of such pipelines. The temperature of the gas as it flows through the pipeline is a function of both the Joule-Thomson effect and the pipe to soil heat transfer. Therefore, the heat transfer and Joule-Thomson effect of the buried natural gas pipeline in this study were carefully considered. Soil temperatures and overall heat transfer coefficients were assumed to be $0{\sim}-20^{\circ}C$ and $0{\sim}5.5W/m^2K$, respectively. The gas temperature and pressure calculations along a pipeline were performed simultaneously at different soil temperatures and overall heat transfer coefficients. Also, this study predicted the phase change and hydrate formation for different soil temperatures and overall heat transfer coefficients using HYSYS simulation package.