Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
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Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
Vol. 27, Issue 3, (2012)
作者机构:
北京航空航天大学 能源与动力工程学院 航空发动机气动热力国家级重点实验室,北京,100191
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DOI:
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Published:2012
稿件说明:
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ZHANG Bin, ZHANG Chun-ben, DENG Hong-wu, et al. Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes[J]. 2012, 27(3).
DOI:
ZHANG Bin, ZHANG Chun-ben, DENG Hong-wu, et al. Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes[J]. 2012, 27(3).DOI:
Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
Experimental results of convection heat transfer to supercritical hydrocarbon fuel (RP-3) in heated vertical tubes were reported in this paper.The effects of heat flux
inlet temperature and flow direction (upward and downward) on heat transfer were studied.In the experiments
the pressure and mass flow rate were maintained at 5MPa and 3g/s the respectively;the heat flux changed from 300kW/m2 to 600kW/m2 and the inlet temperature ranged from 293K to 673K.Test results indicate that heat transfer deterioration appears firstly at the inlet of the heated test section and then increases after thermal boundary layer is developed totally.In addition
heat transfer is enhanced near the critical point of the fuel due to the significant changes of thermalphysics properties;when the inlet temperature of RP-3 exceeds its pseudo-critical temperature
heat transfer deterioration occurs again due to the heat capacity of RP-3 decreases rapidly
Furthermore
the heat transfer coefficient of RP-3 in downward flow is greater than that in upward flow due to the buoyancy effect even if the value of determining factor is lower than 10-5.Based on the experimental data
correlations are developed for the local Nusselt number of convection heat transfer to supercritical hydrocarbon fuel in vertical miniature heated tubes.
Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure
Large eddy simulation of cryogenic jet under supercritical pressure based on OpenFOAM
Flow and thermal analysis of oil air two-phase medium in bearing chamber
Effect of channel cross sectional shape on flow distribution of hydrocarbon fuel
Theoretical and experimental studies of vacuum cooling of liquid nitrogen
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Yi WANG
Lixin ZHOU
Related Institution
Institute of Mechanics, Chinese Academy of Sciences
Institute of Engineering Thermophysics, Chinese Academy of Sciences
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National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation