Flow and Mass Transfer of Pyrolytic Aviation Kerosene in Curved Channel
Author:
Affiliation:
1. Harbin Institute of Technology, 518055 Shenzhen, Guangdong, People’s Republic of China
2. Harbin Institute of Technology, 150001 Harbin, Heilongjiang, People’s Republic of China
Funder
Development and Reform Commission of Shenzhen Municipality
Fundamental Research Funds for the Central Universities
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Condensed Matter Physics,Aerospace Engineering,Space and Planetary Science,Fluid Flow and Transfer Processes,Mechanical Engineering
Reference40 articles.
1. Conjugate heat transfer, endothermic fuel pyrolysis and surface coking of aviation kerosene in ribbed tube at supercritical pressure
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3. Validation and analyses of RANS CFD models for turbulent heat transfer of hydrocarbon fuels at supercritical pressures
4. Numerical simulation of supercritical catalytic steam reforming of aviation kerosene coupling with coking and heat transfer in mini-channel
5. Numerical analysis of convective heat transfer characteristics of supercritical hydrocarbon fuel in cooling panel with local flow blockage structure
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