Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure
|更新时间:2026-07-07
|
Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure
Vol. 25, Issue 8, (2010)
作者机构:
1. 中国科学院工程热物理研究所,北京,100190
2. 中国科学院力学研究所,北京,100190
作者简介:
基金信息:
DOI:
CLC:
Published:2010
稿件说明:
移动端阅览
LI Xun-feng, ZHONG Feng-quan, FAN Xue-jun, et al. Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure[J]. 2010, 25(8).
DOI:
LI Xun-feng, ZHONG Feng-quan, FAN Xue-jun, et al. Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure[J]. 2010, 25(8).DOI:
Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure
RNG(renormalization group) k-ε turbulent model combined with Wolfstein one-equation model in the vicinity of the wall was used to calculate the convective heat transfer properties of Daqing RP-3 aviation kerosene in a horizontal pipe at a supercritical pressure.A significant secondary flow was generated by the buoyancy effect due to the dramatic changes of the thermophysical properties of the kerosene near the pseudo-critical point.The secondary flow enhanced the turbulence intensity and convective heat transfer on the bottom of the pipe
and reduced the turbulence intensity and heat transfer on the top.Finally
the applicability of two criteria
used for the buoyancy effect on the convective heat transfer of horizontal pipes
was analyzed and compared at the supercritical conditions.
Experiment on flow instability of aviation kerosene under supercritical pressures
Experiment on convective heat transfer of aviation keroseneRP-3 in vertical micro-tube at supercritical pressure
Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
Large eddy simulation of cryogenic jet under supercritical pressure based on OpenFOAM
Effect of key parameters on knock of two⁃stroke kerosene engine
Related Author
王彦红
李素芬
赵星海
赵伟
闻洁
付衍琛
张楠
黄浩然
Related Institution
大连理工大学 能源与动力学院
东北电力大学 能源与动力工程学院
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
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics, School of Jet Propulsion, Beijing University of Aeronautics Astronautics
National Key Laboratory of Science and Technology on Liquid Rocket Engines,Xi'an Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation