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Compressor stall and blade vibrationMultistage axial flow compressor stalling characteristics and blade vibration
Document ID
19650013755
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Graham, R. W. (NASA Lewis Research Center Cleveland, OH, United States)
Guentert, E. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
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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