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Analysis of a bypass air control system for a supersonic mixed-compression inletBypass air control system analysis for supersonic mixed compression inlet
Document ID
19670019707
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Brown, S. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-4032
Report Number: NASA-TN-D-4032
Accession Number
67N29036
Funding Number(s)
CONTRACT_GRANT: 720-03-01-01-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC FLOW
COMPRESSION
CONTROL SYSTEM
ANALOG COMPUTER

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