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Experimental Investigation of an Axial Flow Compressor Inlet Stage Operating at Transonic Relative Inlet Mach Numbers I : Over-all Performance of Stage with Transonic Rotor and Subsonic Stators up to Rotor Relative Inlet Mach Number of 1.1
Document ID
19930086942
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Lieblein, Seymour
Lewis, George W , Jr
Sandercock, Donald M
Date Acquired
August 16, 2013
Publication Date
March 10, 1952
Report/Patent Number
NACA-RM-E52A24
Report Number: NACA-RM-E52A24
Accession Number
93R16232
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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