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A supersonic inlet-engine control using engine speed as a primary variable for controlling normal shock positionSupersonic inlet engine control using engine speed as primary variable for controlling normal shock position
Document ID
19710011199
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Hagedorn, R. E. (NASA Lewis Research Center Cleveland, OH, United States)
Neiner, G. H. (NASA Lewis Research Center Cleveland, OH, United States)
Paulovich, F. J. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1971
Subject Category
Propulsion Systems
Report/Patent Number
E-5492
NASA-TN-D-6021
Report Number: E-5492
Report Number: NASA-TN-D-6021
Accession Number
71N20674
Funding Number(s)
CONTRACT_GRANT: 720-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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