NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Simulating The Performance Of A ScramjetSCRAM 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.
Document ID
19910000096
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Walton, James T.
(NASA Ames Research Center, Moffett Field, CA.)
Date Acquired
August 14, 2013
Publication Date
March 1, 1991
Publication Information
Publication: NASA Tech Briefs
Volume: 15
Issue: 3
ISSN: 0145-319X
Subject Category
Machinery
Report/Patent Number
ISSN: 0145-319X
Report Number: ARC-12338
ARC-12338
Accession Number
91B10096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Available Downloads

There are no available downloads for this record.
No Preview Available