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:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-SE52G03
Link:	https://digital.library.unt.edu/ark:/67531/metadc65357/