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Investigation of Sea-Level Performance of I-16 Turbojet Engine at Zero Ram with XFR-1 Intake Duct Shroud, and Tail PipeThe sea-level performance of I-16 turbojet engine at zero ram was investigated to determine the effects of an intake duct, shroud, and tail pipe intended for installation in an XFR-1 airplane. Engine speeds ranged from 8000 to 16,500 rpm for several variations of the intake duct and tail pipes.
Document ID
20030065181
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Dowman, Harry W. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Anderson, William G. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 1947
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-E7G24
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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