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Compressor Stall and Blade VibrationMultistage axial flow compressor stalling characteristics and blade vibration
Document ID
19650013755
Acquisition Source
Glenn Research Center
Document Type
Contribution to a larger work
Authors
Robert W Graham (Lewis Research Center Cleveland, OH, United States)
Eleanor Costilow Guentert (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
Volume: NASA-SP-36
Subject Category
Aerodynamics
Accession Number
65N23356
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
MULTISTAGE COMPRESSOR
STALLING
COMPRESSOR BLADE
VIBRATION
AXIAL FLOW COMPRESSOR
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IDRelationTitle19650013744Collected WorksAerodynamic Design of Axial Flow Compressors
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