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Inlet sensitivity study for a supersonic transportMethod of comparing inlet performance and weight compromises for supersonic transport
Document ID
19670010560
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Koenig, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1967
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-3881
Report Number: NASA-TN-D-3881
Accession Number
67N19889
Funding Number(s)
CONTRACT_GRANT: 126-15-02-02-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
TURBOJET ENGINE
AIR INLET
SUPERSONIC TRANSPORT

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