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Design of supersonic inlets by a computer program incorporating the method of characteristicsFORTRAN computer program for designing supersonic inlets by characteristic theory
Document ID
19690005234
Document Type
Other - NASA Technical Note (TN)
Authors
Anderson, B. H. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-4960
Accession Number
69N14566
Funding Number(s)
CONTRACT_GRANT: 126-15-02-11-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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