Effect of inlet-air baffles on rotating-stall and stress characteristics of an axial-flow compressor in a turbojet engine

Author:	Huntley, S. C.
Additional Authors:	Huppert, Merle C.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E54G09
Link:	https://digital.library.unt.edu/ark:/67531/metadc60793/