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Altitude-Wind-Tunnel Investigation of a 4000-Pound-Thrust Axial-Flow Turbojet EngineOperating characteristics of the 11-stage 4000-pound-thrust axial-flow turbojet engine were determined. A standard compressor and a compressor with the blade angles of the rotor and stator blades increased 5 degrees to obtain greater air flow, were investigated.
Document ID
20030064033
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Dietz, Robert O., Jr. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Suozzi, Frank L. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 5, 1948
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-E8F09c
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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