NASA NTRS · 19910000096
Simulating The Performance Of A Scramjet
Abstract
SCRAM computer program determines, according to one-dimensional mathematical model, cycle performance for airframe-integrated subsonic or supersonic combustion Ramjets. Reliable, efficient, and speedy ramjet designer's software tool usable on all standard computers down to those compatible with IBM PC-AT's. Scramjet cycle analysis code simulates, from nose to tail, hydrogen-fueled, airframe-integrated scramjet in real gas flow with equilibrium thermodynamic properties. Enables rapid scramjet performance estimates. Written in FORTRAN 77.
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Walton, James T.. 1991-03-01. Simulating The Performance Of A Scramjet. https://ntrs.nasa.gov/citations/19910000096
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