Numerical investigations of supersonic combustion characteristics of thermally cracked fuels at typical pyrolysis temperatures
Author:
Funder
National Natural Science Foundation of China
National Major Science and Technology Projects of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference51 articles.
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2. Effects of fuel cracking on combustion characteristics of a supersonic model combustor;Zhong;Acta Astronaut.,2015
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5. Investigation of an optimal pulsed jet mixing and combustion in supersonic crossflow;Zhao;Combust. Flame,2021
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