With the resurgence of interest in high supersonic and hypersonic flight there is a need to simulate airbreathing engines which may be used in this flight regime. To meet this requirement the RAMSCRAM code was developed. The code calculates 1-D flow properties at each component interface and the overall performance of the engine. It uses equilibrium thermodynamics which accounts for dissociation and allows for any fuel or combination of fuels. The program can simulate ramjet, scramjet, rocket, and ducted rocket engines.
RAMSCRAM: A Flexible Ramjet/Scramjet Engine Simulation Program
1990
6 pages
Report
No indication
English
Jet & Gas Turbine Engines , Engine Studies, Energy Related , Fluid Mechanics , Supersonic combustion ramjet engines , Computer programs , Computerized simulation , Supersonic flight , Thermodynamic equilibrium , Ducted rocket engines , Engine tests , Flow characteristics , Fuels , Hypersonic flight , Propulsive efficiency , Computational fluid dynamics
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