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Graphic Analysis of American and British Axial-Flow Turbojet Engine Performance Trends (Current and Future)This report presents a compilation of static sea-level data on existing or designed American and British axial-flow turbojet engines in terms of basic engine parameters such as thrust and air flow. In the data presented, changes in the over-U engine performance with time sre examined as well as the relation of the various engine parameters to each other.
Document ID
20050019237
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Cesaro, Richard S. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Lazar, James (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
August 22, 2013
Publication Date
December 10, 1951
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-51K29
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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