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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
Author:
Lieblein, Seymour
Additional Authors:
Lewis, George W , Jr
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E52A24
Link:
https://digital.library.unt.edu/ark:/67531/metadc59093/
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