Investigation of a High-Performance Axial-Flow Compressor Transonic Inlet Rotor Designed for 37.5 Pounds Per Second Per Square Foot of Frontal Area: Aerodynamic Design and Overall Performance

Author:	Savage, Melvyn
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L55A05
Link:	https://digital.library.unt.edu/ark:/67531/metadc61117/