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Computer program for calculating flow fields in supersonic inletsFortran IV computer program to calculate flow fields in supersonic inlets
Document ID
19650019694
Document Type
Other - NASA Technical Note (TN)
Authors
Sorensen, V. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1965
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-2897
Accession Number
65N29295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
COMPUTER PROGRAM
FLOW FIELD
SUPERSONIC INLET

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