Analysis of turbine stator adjustment required for compressor design-point operation in high Mach number supersonic turbojet engines

Author:	English, Robert E
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E53G06
Link:	https://digital.library.unt.edu/ark:/67531/metadc59780/