Experimental investigation of an axial-flow-compressor inlet stage operating at transonic relative inlet Mach numbers V : rotor blade-element performance at a reduced blade angle

Author: Schwenk, Francis C
Additional Authors: Lewis, George W , Jr
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56J17
Link: https://digital.library.unt.edu/ark:/67531/metadc62950/

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