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Altitude-Wind-Tunnel Investigations of Thrust Augmentation of A Turbojet Engine Performance With Tail-Pipe Burning
Document ID
19930085675
Acquisition Source
Langley Research Center
Document Type
Other
Authors
W. A. Fleming (Aircraft Engine Research Laboratory Cleveland, United States)
R.O. Dietz (Aircraft Engine Research Laboratory Cleveland, United States)
Date Acquired
August 16, 2013
Publication Date
September 25, 1946
Report/Patent Number
NACA-RM-E6I20
Accession Number
93R14965
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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