Experimental investigation of axial-flow compressor inlet stage operating at transonic relative inlet Mach numbers : blade-coordinate data

Author:	Lewis, George W , Jr
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52C27
Link:	https://digital.library.unt.edu/ark:/67531/metadc59324/