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A low-pressure-loss short afterburner for sea-level thrust augmentationLow-pressure-loss short afterburner design for sea level thrust augmentation of axial flow turbojet engine
Document ID
19660010445
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Burley, R. R. (NASA Lewis Research Center Cleveland, OH, United States)
Ciepluch, C. C. (NASA Lewis Research Center Cleveland, OH, United States)
Velie, W. W. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
June 7, 1955
Subject Category
Propulsion Systems
Report/Patent Number
NACA-RM-E55D26
Report Number: NACA-RM-E55D26
Accession Number
66N19734
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THRUST AUGMENTATION
AFTERBURNER
TURBOJET ENGINE

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