Convective heat transfer of supercritical China aviation fuel RP-3 in vertical micro-tube (inner diameter of 1.09mm) was experimentally investigated. Influences of system pressure
heat flux
flow direction and buoyancy on heat transfer were analyzed. Wall heat fluxes (180-460kW/m2)
system import pressure (3-5MPa) and inlet Reynolds number (3200-10200) were maintained in experiments. The result showed that the buoyancy force deteriorated the heat transfer of downward flow in the entrance of test section; system pressure affected the convective heat transfer mainly by the impact of fluid thermal properties; effects of different flow directions on convection heat transfer were very significant. Overall heat transfer was strengthened for downward flow and decreased for upward flow.
Flow resistance characteristics of supercritical aviation kerosene in helix tube
Numerical study of convective heat transfer characteristics of kerosene flowing in a horizontal pipe at supercritical pressure
Effect of key parameters on knock of two⁃stroke kerosene engine
Effect of lean blowout performance of trapped vortex combustor of the afterburner
Research on mixture formation of two⁃stroke heavy fuel direct injection engine
Related Author
FU Yan-chen
DENG Hong-wu
LV Pin
XU Guo-qiang
RAN Zhen-hua
LI Xun-feng
ZHONG Feng-quan
FAN Xue-jun
Related Institution
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
Institute of Mechanics, Chinese Academy of Sciences
Institute of Engineering Thermophysics, Chinese Academy of Sciences
College of Energy and Power Engineering,Nanjing University of Aeronautics and Astronautics
Sichuan Gas Turbine Establishment,Aero Engine Corporation of China