Experimental investigation of an axial-flow supersonic compressor having rounded leading-edge blades with an 8-percent mean thickness-chord ratio

Author:	Goldberg, Theodore J.
Additional Authors:	Boxer, Emanuel
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L53G16
Link:	https://digital.library.unt.edu/ark:/67531/metadc59682/