Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages V : preliminary analysis of over-all performance of modified compressor

Author:	Standahar, Raymond M
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55A03
Link:	https://digital.library.unt.edu/ark:/67531/metadc61074/