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Manual for improved source flow characteristics programA FORTRAN IV program for analyzing the nozzle flow for a hypersonic scramjet by a two dimensional second order characteristic procedure is presented.
Document ID
19750021287
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Delguidice, P. D. (Advanced Technology Labs., Inc. Westbury, NY, United States)
Date Acquired
September 3, 2013
Publication Date
May 1, 1975
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
ATL-TM-183
NASA-CR-132696
Report Number: ATL-TM-183
Report Number: NASA-CR-132696
Accession Number
75N29360
Funding Number(s)
CONTRACT_GRANT: NAS1-13303
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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