Experimental investigation of a 0.4 hub-tip diameter ratio axial-flow compressor inlet stage at transonic inlet relative Mach numbers I : rotor design and over-all performance at tip speeds from 60 to 100 percent of design

Author:	Serovy, George K
Additional Authors:	Robbins, William H
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E53I11
Link:	https://digital.library.unt.edu/ark:/67531/metadc59984/