Large eddy simulation of shock-combustion-film interaction at hydrogen injection in a model scramjet combustor
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference74 articles.
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4. Influences of accelerating states on supercritical n-decane heat transfer in a horizontal tube applied for scramjet engine cooling;Chen;Aerosp. Sci. Technol.,2021
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1. Large eddy simulation of turbulent transport and thermal enhancement in a steam-cooled ribbed channel;Case Studies in Thermal Engineering;2024-09
2. Effect of jet splitting using passive strut on the performance and thermoacoustic characteristics of a scramjet combustor;Physics of Fluids;2024-08-01
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