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
International Gas Turbine Aeroengine Congress and Exposition ; 1990 ; Brussels, Belgium
1990-01-01
Conference paper
No indication
English
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