thermal conductivity and specific heat of five kinds of surrogate models for endothermic hydrocarbon fuel RP-3 by extended corresponding state law were conducted. In the computation
the temperature and pressure ranged from 300K to 800K and from 3MPa to 6MPa
respectively. Results indicated that all surrogate models could qualitatively reproduce sharp variation of physical property of RP-3 in the vicinity of pseudo-critical temperature; a three-species surrogate model consisting of mole of 53% n-undecane
18% n-butylcyclohexane
29% 1
3
5-trimethyl-benzene performed best among five physical surrogate models in predicting physical property of RP-3. The relative errors of this surrogate model for density were less than 0.08 at the temperature from 300K to 700K. Pseudo-critical temperature increased with growing relative molecular mass of surrogate models
showing that there was no obvious relationship between thermal properties under pseudo-critical temperature and relative molecular mass of surrogate models.
Pressure effect on the heat transfer characteristics of hydrocarbon fuel in the horizontal circular tube at supercritical pressures
Numerical investigation on effects of ambient and injection parameters on supercritical injection
Effects of RP-3 coke deposition on heat transfer under supercritical pressure
Heat transfer characteristics of hydrocarbon fuel at supercritical pressure in vertical circular tubes
An integrated optimization of hypersonic forebody/inlet based on surrogate models
Related Author
ZHANG Qi-jun
JIA Zhou-xia
XU Guo-qiang
ZHU Kun
ZHOU Zhou
FAN Zhen-cen
FAN Wei
JIN Le
Related Institution
Academy of Aeronautic Propulsion Technology, Aviation Industry Corporation of China
National Key Laboratory of Science and Technology on Aero-Engine Aero-Thermodynamics,School of Energy and Power Engineering,Beijing University of Aeronautics and Astronautics
School of Power and Energy,Northwestern Polytechnical University
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermcolynamics, School of Jet Propulsion, Beijing University of Aeronautics Astronautics
Institute of Aerospace and Material Engineering, National University of Defense Technology