Thermodynamic analysis of a high Mach number scramjet engine with secondary combustion for thrust enhancement
Author:
Publisher
Elsevier BV
Subject
Fluid Flow and Transfer Processes
Reference33 articles.
1. Experimental study on atomization characteristics of high-energy-density fuels using a fuel slinger;Sun;Energy,2021
2. Utilization of high-density strained hydrocarbon fuels for propulsion;Roy;J. Propul. Power,2000
3. T. Kokan, J.R. Olds, Characterizing High-Energy-Density Propellants for Space Propulsion Applications. 57th International Astronautical Congress, Valencia, Spain: American Institute of Aeronautics and Astronautics; 2006. https://doi.org/10.2514/6.IAC-06-C4.P.1.10.
4. Analysis of the maximum flight Mach number of hydrocarbon-fueled scramjet engines under the flight cruising constraint and the combustor cooling requirement;Wang;Aerosp. Sci. Technol.,2020
5. First step to an operational application of high-speed airbreathing propulsion;Falempin,2003
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