Effect of rotor-and stator-blade modifications on surge performance of an 11-stage axial-flow compressor 1: original production compressor of XJ40-WE-6 engine

Author:	Finger, Harold B.
Additional Authors:	Essig, Robert H.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52G03
Link:	https://digital.library.unt.edu/ark:/67531/metadc59340/