Program developed to support research on National Aero-Space Plane, which takes off horizontally and flies into orbit. SCRAM performs nose-to-tail simulation of real gas flow with equilibrium thermodynamic characteristics encountered in hydrogen-fueled ramjet/scramjet engine. Written for supersonic flows, code modified to handle subsonic flows and dual-mode combustor operation. Written in FORTRAN 77.
An Engineer's Tool For Prediction Of Airframe Integrated Scramjet Performance (SCRAM)
NASA Tech Briefs ; 14 , 12
1990-12-01
Miscellaneous
No indication
English
Scram jet Engine/Airframe Integration Methodology
British Library Conference Proceedings | 1997
|Effects of Airframe Integrated Configuration on Scramjet Inlet Performance
British Library Conference Proceedings | 2000
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