• Title/Summary/Keyword: 유동방향 전도열전달

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Numerical Analysis on Longitudinal Heat Conduction in Printed Circuit Heat Exchanger (인쇄기판형 열교환기의 유동방향 전도열전달에 관한 수치해석 연구)

  • Oh, Dong-Wook;Kim, Young;Choi, Jun Seok;Yoon, Seok Ho
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.26 no.12
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    • pp.600-604
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    • 2014
  • Longitudinal heat conduction is known to be an important factor in the design of a printed circuit heat exchanger(PCHE) for cryogenic applications. Parasitic heat conduction through the heat exchanger frame needs to be considered because it is known to decrease the effectiveness of the heat exchanger. In this paper, a conjugate heat transfer problem in a simple counter-flow PCHE is analyzed by a computational fluid dynamics simulation. The effect of longitudinal conduction in a straight channel is compared with the theoretical effectiveness-NTU relationship that assumes a "thin" heat exchanger frame. The calculation results suggest that the theoretical model is valid in the present calculation conditions where NTU is < 13.

A Numerical Simulation of Regenerative Cooling Heat Transfer Processes for the Liquid Propellant Rocket Engine (액체추진제 로켓엔진의 재생냉각 열전달과정 전산모사)

  • 서호원
    • Journal of the Korean Society of Propulsion Engineers
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    • v.2 no.3
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    • pp.54-61
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    • 1998
  • A numerical simulation is attempted for the regenerative cooling heat transfer processes of the liquid propellant rocket engine. The heat transfer from the combustion gases to the thrust chamber wall is called gas side heat transfer. This heat is conducted radially to the coolant through the carbon deposit and metallic wall of thrust chamber Finally, this heat is convected away by the coolant flowing along the passages in the thrust chamber. The equivalence of these three heat fluxes of the above processes is utilized to determine the coolant side wall temperature, gas side wall temperature and the heat flux. When the number and shape(width, height) of coolant passages, the shape(size) of thrust chamber, oxidant and fuel properties, coolant properties, oxidant/fuel mixture ratio, coolant inlet temperature, the thickness of carbon deposit formed along the thrust chamber wall during combustion are given, reasonable radial direction temperature distributions and heat fluxes along the thrust chamber axis are obtained.

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A Study of Heat Transfer during Freezing Process of Water in a Vertical Cylinder - Comparison of thermal storage performance on the working fluid direction - (수직원통형 축열조내 물의 응고과정시 열전달에 관한 실험적연구 - 작동유체의 유동방향에 따른 열저장성능 비교 -)

  • Heo, K.;Kim, Y.K.;Kim, Y.J.;Kim, J.K.;Yim, C.S.
    • Solar Energy
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    • v.15 no.2
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    • pp.77-90
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    • 1995
  • An effective heat transfer during freezing process was proposed in the vertical cylinder to improve the effectiveness of the heat storage. Vertical cylinder was filled with pure water in order to investigate ice-shape, temperature distribution of the liquid, temperature distribution of the cylinder tube wall, total heat storage per unit mass in the test section under the two experimental conditions; inlet temperature of working fluid is constant($-10^{\circ}C$) and inlet direction of working fluid is either upward flow or downward. Both the mean temperature of the liquid and temperature difference of cylinder tube wall in the upward were lower than those in the downward. In case that the initial temperature of water was $7^{\circ}C$ and $4^{\circ}C$, the shape of ice layer in the upward was more uniform than that in the downward. In case of $1^{\circ}C$, the shape of ice layer is formed by inlet direction of working fluid. Finally, time-varying total heat energy stored in the water in the upward was higher than that in the downward.

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