Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages IV : modification of aerodynamic design and prediction of performance

Author:	Geye, Richard P
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55B28
Link:	https://digital.library.unt.edu/ark:/67531/metadc61343/