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Turbojet and turbofan cycle considerations and engine configurations for application in lightweight aircraftCycle characteristics and structural configuration of turbojet and turbofan engines for lightweight aircraft
Document ID
19680022004
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Roelke, R. J. (NASA Lewis Research Center Cleveland, OH, United States)
Stewart, W. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-1624
Report Number: NASA-TM-X-1624
Accession Number
68N31476
Funding Number(s)
CONTRACT_GRANT: 126-15-01-23-22
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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