Investigation of impulse-type supersonic compressor with hub-tip ratio of 0.6 and turning to axial direction I : performance of rotor alone

Author:	Wilcox, Ward W
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E54B25
Link:	https://digital.library.unt.edu/ark:/67531/metadc60285/