Effect of Various Blade Modifications on Performance of a 16-Stage High-Pressure-Ratio Axial-Flow Compressor 1 - Effect on Over-All Performance Characteristics of Decreasing Twelfth Through Fifteenth State Stator-Blade Angles 3 Degrees

Author:	Medeiros, Arthur A.
Additional Authors:	Hatch, James E.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E51L03
Link:	https://digital.library.unt.edu/ark:/67531/metadc65407/