C4+ Surrogate Models for Thermophysical Properties of Aviation Kerosene RP-3 at Supercritical Pressures
Author:
Affiliation:
1. Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Department of Engineering Mechanics, Tsinghua University, Beijing 100084, China
Funder
Ministry of Science and Technology of the People's Republic of China
Publisher
American Chemical Society (ACS)
Subject
Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering
Link
https://pubs.acs.org/doi/pdf/10.1021/acs.energyfuels.1c00326
Reference43 articles.
1. Numerical study of heat transfer deterioration of turbulent supercritical kerosene flow in heated circular tube
2. Numerical investigation of heat transfer characteristics and flow resistance of kerosene RP-3 under supercritical pressure
3. Modeling and analysis of heat and mass transfers of supercritical hydrocarbon fuel with pyrolysis in mini-channel
4. Experimental investigation on heat transfer of a specific fuel (RP-3) flows through downward tubes at supercritical pressure
5. Heat transfer degradation of buoyancy involved convective RP-3 hydrocarbon fuel in vertical tubes with various diameters under supercritical pressure
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