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Investigation of a mixed-compression axisymmetric inlet system at Mach numbers 0.6 to 3.5Wind tunnel tests of mixed compression axisymmetric inlet system at Mach numbers 0.6 to 3.5
Document ID
19710003549
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Smeltzer, D. B. (NASA Ames Research Center Moffett Field, CA, United States)
Sorenson, N. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
A-3516
NASA-TN-D-6078
Report Number: A-3516
Report Number: NASA-TN-D-6078
Accession Number
71N13024
Funding Number(s)
CONTRACT_GRANT: 720-03-01-10-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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