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Compressor operation with one or more blade rows stalledHigh pressure-ratio multistage axial flow compressor operation efficiency with one or more blade rows stalled - performance prediction
Document ID
19650013757
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Benser, W. A. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 2, 2013
Publication Date
January 1, 1965
Subject Category
Aerodynamics
Accession Number
65N23358
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AXIAL FLOW COMPRESSOR
STALLING
PERFORMANCE PREDICTION
MULTISTAGE COMPRESSOR
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