The recent worldwide interest in developing ramjet engines has motivated this preliminary study of the ramjet thermodynamic cycle. Results show that for fixed flight conditions (altitude, flight Mach number and thrust) there is an optimum combustor temperature which furnishes a minimum fuel consumption.
Estudo Termodinamico de Estato-Reatores (Thermodynamic Study of Ramjet Engines)
1986
18 pages
Report
No indication
English
Springer Verlag | 2021
|Fundamentals of Ramjet Engines
Springer Verlag | 2021
|Thermodynamic cycle analysis of ramjet engines using magnesium-based fuel
Online Contents | 2012
|NTRS | 1967
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