• Transactions of the Korean Society of Mechanical Engineers B
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• v.25 no.5
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• pp.722-730
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• 2001

The local heat transfer of an axisymmetric submerged air jet impinging on a heated flat plate is investigated experimentally with the variation of mesh-screen solidity. The screen installed in front of the nozzle exit modifies the flow structure and local heat transfer characteristics. The mean velocity and turbulence intensity profiles of streamwise velocity component are measured using a hot-wire anemometry. The temperature distribution on the heated flat surface is measured with thermocouples. The smoke-wire flow visualization technique was employed to understand the near-field flow structure qualitatively for different mesh screens. Large-scale toroidal vortices and high turbulence intensity enhance the heat transfer rate in the stagnation region. For a higher solidity, turbulence intensity become higher which increases the local heat transfer at small nozzle-to-plate spacings such as L/D<6. The local and average Nusselt numbers of impinging jet from the $\sigma$(sub)s=0.83 screen at L/D=2 are about 5.6∼7.5% and 7.1% larger than those for the case of no screen, respectively. For the nozzle-to-plate spacings larger than 6, however, the turbulence intensities for all tested screens approach to an asymptotic curve and the mean velocity along the jet centerline decreases monotonically. As the nozzle-to-plat spacing increases for high solidity screens, the heat transfer rate decreases due to the reduction in turbulence intensity and jet momentum.

• Computational Structural Engineering
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• v.7 no.3
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• pp.123-131
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• 1994

This paper is concerned with a new concept of vibration control in which thermal stresses are utilized. Thermal actuators are used to generate thermal stresses in a vibrating beam. The thermal actuators are found to work successfully as the control means. Especially the proposed control method in this paper can be effectively applied to the large space structures with low natural frequencies rather than to the structures with high natural frequencies. In the process of control design, various control methods including optimal-robust control method are investigated. Through numerical simulations, it is found that the robust-optimal control method can be efficiently with the vibration control of a cantilever beam using thermal stresses.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.20 no.4
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• pp.639-647
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• 2019

Recently, as the semiconductor integration technology due to miniaturization and high density of electronic equipment have developed, it is importantly recognized the application of thermal control system in order to release inner heat generated from chips, modules, In this study, we considered the heat transfer and pressure drop characteristics in a horizontal channel with four blocks using k-${\omega}$ SST turbulence model During CFD (Computational Fluid Dynamics) analysis, the parameters applied block width, block height, heat source and turbulence generator placement etc. As the boundary conditions of analysis, the channel inlet temperature and flow velocity were respectively 300 K and 3.84 m/s, the heat flux was $358W/m^2$. As a result, the heat transfer performance was decreased as the block width ratio (w/h) was increased, while it was increased as the block height ratio (h/w) was increased. In addition, as the arrangement of heat source size was increased to high heat flux from low heat flux, it was influenced by heat source size and the heat transfer coefficient showed a tendency to increase, When the turbulence generator was installed in the upper part of block No. 1 position the closely to the channel entrance, the heat transfer characteristics was greatly influenced on the whole of four heating blocks. and in oder to consider the pressure drop characteristics, we are able to select the most appropriate turbulence generator's position.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1998.05a
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• pp.95-103
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• 1998

오늘날 전기 철도 차량의 속도제어방식에는 A.C모터의 속도를 제어하는 방식을 많이 사용하고 있고 이 경우 여러 개의 GTO thyristor와 다이오드가 필요하다. 그런데 이러한 반도체 소자들은 전기 부하의 일부를 저항열로 소모하며 반도체의 용량에 따라 차이가 있으나 전기 철도 차량의 경우 약 1~2㎾의 열이 발생한다. 따라서 이들 소자들이 적정온도범위(100~12$0^{\circ}C$미만)를 유지하기 위해서는 소자의 내부저항열을 외부로 방출시켜야 한다. 지난 30여 년 동안 이러한 반도체 소자 냉각에는 강제대류, 침적 비등, 히트파이프식 냉각방법이 적용되어 왔다. 최근에는 히트파이프식 냉각방법이 유지보수, 크기 및 중량 등 여러 측면에서 상대적으로 유리하기 때문에 히트파이프식 냉각방법을 주로 사용하고 있다. (중략)

• Journal of Power System Engineering
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• v.7 no.3
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• pp.35-39
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• 2003

In this paper, the heat transfer phenomena in the sensor tube of a mass flow controller(MFC) were studied by experiments. In the sensor tube of MFC, the difference of temperature between inlet and outlet was necessary for calculating the mass flow rate. Therefore, the relations of flow rate, generated heat by heating wire, sensor location and tube thickness were investigated to find the optimized condition. Based on this study, static and dynamic characteristics of sensor can be used for mass flow controller.

• 한국가시화정보학회:학술대회논문집
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• 2002.11a
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• pp.55-58
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• 2002

To control the frost formation, a temperature variation of the cooling plate and characteristics on hydrophilic and hydrophobic surfaces was attempted. As a temperature variation of the cooling plate, being closely related to the frost layer density of frost layer is found to be affected by the melting process inside the frost layer during the heating period. At characteristics on surface, completely different structures of frost are appeared in the initial stage of frost formation due to the difference in surface conditions, while those effects are vanished with time. It is found that the frost thickness, density and heat flux characteristics are closely associated with the frost structure.

• ICROS
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• v.8 no.6
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• pp.23-25
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• 2002

이 논문은 탄소나노튜브의 전자소자 응용이라는 관점에서 최근의 연구동향과 실제적으로 응용이 되기 위해서 해결해야 할 이슈들을 정리하고자 하였다. 탄소나노튜브가 고해상도 투과전자현미경 1991년도에 발견된 이래로, 그 특유의 뛰어난 특성과 잠재되어있는 차세대 소자로서의 응용가능성으로 인하여 큰 주목을 받고 있는 실정이다 [1]. 93년에 수집 편에 불과하던 논문발표 건수가 2001년에는 1500 여편에 달하고 있으며 특허건수만 해도 2100여건에 달하고 있다 [2]. 탄소나노튜브는 수 nm~수백nm의 직경과 함께 내부의 빈 공간을 지니는 1차원의 튜브형태로서, 성장되는 구조에 따라서 금속성, 반도체성을 지니게 된다 [3,4]. 우수한 열전도성, 전자수송능력, 기계적 특성으로 이를 이용한 차세대소자 nanoelectronics [5], fileld emission display [6], hydrogen storage, fuel cell [7], supercapacitors [8], gas sensors [9] 및 STM 탐침으로서 그 응용이 기대 되어진다. 특히 이 논문에서는 나노튜브의 응용과 소자를 실현화하기 위해서 해결해야 할 이슈들과 기능 소자로서의 응용 현황을 중점적으로 살펴보고 그 연구 방향을 제언하고자 한다.

• Proceedings of the Korea Concrete Institute Conference
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• 2008.11a
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• pp.249-252
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• 2008

In recent large-scale structures, as mass concrete type structure is frequently applied to the building, temperature crack due to hydration heat needs to be considered. Since a volume change is internally or externally restricted in a mold after placing concrete, temperature crack of mass concrete takes place. By this reason, the reduction method to control this crack is required. In this study, low heat mixture and hydration heat difference is used to execute the analysis of hydration heat, considering the changes of heat transfer coefficient according to curing conditions and block placement of mass concrete. For the analytical modelling, original portland cement and concrete of low heat mixture are placed in the upper and lower payer, respectively. A convection boundary condition is fixed because mass concrete of block placement is characterized by the difference of mold form and curing condition. Through the analysis results considering the changes of low heat mixture, block placement, and heat transfer coefficient, we check out the temperature and stress distribution and analyze the temperature crack reduction effect.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.365-369
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• 2007

The solid rocket interacts circumscriptively in terms of is many more than liquid rocket. It is uncontrollable than liquid rocket because all part of combustion is decided such as Mixture ratio of propellant, burning time and area. However, production cost is cheap and because authoritativeness security can be easy and enlarge the early speed that follow thrust-to-weight ratio, it is used comprehensively by small size rocket. Considered about nozzle cooling to control phenomenon that burn by thermal conduction in interior wall of nozzle that follow in thrust increase of solid rocket and erosion phenomenon by combustion gas of high speed.

• Journal of the Society of Naval Architects of Korea
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• v.39 no.2
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• pp.52-60
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• 2002

Line heating is a forming process which makes the curved surface with the residual strain created by applying heat source of high temperature to steel plate. in order to control the residual strain, it is necessary to understand not only conductive heat transfer between heat source and steel plate, but also temperature distribution of steel plate. In this paper we attempted to analyze is temperature distribution of steel plate by simplifying a line heating process to collision-effusive flux of high temperature and high velocity, and conductive heat transfer phenomenon. To analyze this, combustion in the torch is simplified to collision effusive phenomenon before analyzing turbulent heat flux. The distribution of temperature field between the torch and steel plate is computed through turbulent heat flux analysis, and the convective heat transfer coefficient between effusive flux and steel plate is calculated using approximate empirical Nusselt formula. The velocity of heat flux into steel plate is computed using the temperature distribution and convective heat transfer coefficient, and temperature field in the steel plate is obtained through conductive heat transfer analysis in which the traction is induced by velocity of heat flux. In this study, Finite Element Method is used to accomplish turbulent heat flux analysis and conductive heat transfer analysis. FEA results are compared with empirical data to verify results.