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Design and experimental performance of a 0.35 hub-tip radius ratio transonic axial-flow-compressor rotor designed for 40 pounds per second per unit frontal area
Document ID
19930086063
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Montgomery, John C
Yasaki, Paul T
Date Acquired
August 16, 2013
Publication Date
September 4, 1958
Report/Patent Number
NACA-RM-E58D17
Report Number: NACA-RM-E58D17
Accession Number
93R15353
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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