Numerical investigation of combustion field of hypervelocity scramjet engine
Author:
Funder
National Natural Science Foundation of China
Publisher
Elsevier BV
Subject
Aerospace Engineering
Reference28 articles.
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3. Nonlinear characteristics and detection of combustion modes for a hydrocarbon fueled scramjet;Zhang;Acta Astronaut,2015
4. Large eddy simulation of combustion characteristics in a kerosene fueled ro cket-based combined-cycle engine combustor;Huang;Acta Astronaut,2016
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