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Characteristic design study of mixed- compression two-dimensional inlets with low-angle cowls for the Mach number range 2.70 to 1.80Design effects on performance of two dimensional mixed-compression supersonic inlets with low angle cowls
Document ID
19690020682
Acquisition Source
Legacy CDMS
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
July 1, 1969
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-5330
Report Number: NASA-TN-D-5330
Accession Number
69N30060
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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