Considering the total mass change of liquid nitrogen and heat capacity of tank
the mathematical model of vacuum cooling of liquid nitrogen based on the physico-chemical depression
heat transfer coefficient and mass transfer coefficient approach was built. The theoretical results were in satisfactory agreement with the experimental data of making subcooled liquid nitrogen
which indicated the mathematical model could well predict the phase change of liquid nitrogen. The physico-chemical depression of 1.21 K
heat transfer coefficient of 2 942.37 W/(m2·K) and mass transfer coefficient of 0.004 4 m/s respectively were also obtained.
Flow and thermal analysis of oil air two-phase medium in bearing chamber
Experiment on flow boiling heat transfer of R134a in mini-channel of flat tube
Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
Investigation on heat transfer characteristics of spiculate lamilloy internal surfaces
Influence of dimple space on heat transfer enhancement and pressure loss in a dimpled rectangular channel
Related Author
LIU Zhenxia
YANG Fu
LI Yanjun
张大林
文涛
詹宏波
ZHANG Bin
ZHU Kun
Related Institution
南京航空航天大学 航空宇航学院
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics, School of Jet Propulsion, Beijing University of Aeronautics Astronautics
School of Power and Energy,Northwestern Polytechnical University
The Fourth Department, Institute of Ship Engineering, China State Shipbuilding Corporation