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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