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Altitude-wind-tunnel Investigation of Tail-pipe Burner with Converging Conical Burner Section on J35-A-5 Turbojet EngineAn investigation of turbojet-engine thrust augmentation by means of tail-pipe burning has been conducted in the NACA Lewis altitude wind tunnel.
Document ID
19930086005
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Thorman, H Carl
Campbell, Carl E
Date Acquired
August 16, 2013
Publication Date
February 10, 1950
Report/Patent Number
NACA-RM-E9I16
Report Number: NACA-RM-E9I16
Accession Number
93R15295
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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