Effects of compressor interstage bleed and adjustable inlet guide vanes on compressor stall characteristics of a high-pressure-ratio turbojet engine at altitude

Author:	Mallett, William E
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55G27
Link:	https://digital.library.unt.edu/ark:/67531/metadc61663/