Investigation of Reynolds number effect on performance of an eight-stage axial-flow research compressor with long- and medium-chord lengths in the two transonic inlet stages

Author:	Sievers, Gilbert K.
Additional Authors:	Geye, Richard P.
Year:	1958
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E57J30
Link:	https://digital.library.unt.edu/ark:/67531/metadc63977/