Component and over-all performance evaluation of an axial-flow turbojet engine over a range of engine-inlet Reynolds numbers

Author:	Walker, Curtis L.
Additional Authors:	Huntley, S. C.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52B08
Link:	https://digital.library.unt.edu/ark:/67531/metadc59177/