NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Theoretical analysis of various thrust-augmentation cycles for turbojet engines
Document ID
19930082793
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lundin, Bruce T
Date Acquired
August 16, 2013
Publication Date
May 1, 1950
Report/Patent Number
NACA-TN-2083
Accession Number
93R12083
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
ENGINES, TURBOJET - THRUST AUGMENTORS
ENGINES - WATER INJECTION
BLEED-OFF
ENGINES, TURBOJET - THRUST
AFTERBURNING
No Preview Available