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Compressor Design RequirementsThe important requirements of axial-flow compressors for aircraft gas-turbine engines and the reasons for these requirements are reviewed. Attention is first directed to the over-all requirements of the engines themselves; then the desired properties of compressors are examined.
Document ID
19650013746
Acquisition Source
Glenn Research Center
Document Type
Other - Technical Report
Authors
Robert O Bullock (Lewis Research Center Cleveland, OH, United States)
Ernst I Prasse (Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Publication Information
Publication: Aerodynamic Design of Axial Flow Compressors
Publisher: National Aeronautics and Space Administration
Subject Category
Aerodynamics
Report/Patent Number
NASA-SP-36
Accession Number
65N23347
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
GAS TURBINE
TURBOJET ENGINE
TURBOPROP ENGINE
AXIAL FLOW COMPRESSOR
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