An approximate method of determining the subsonic flow in an arbitrary stream filament of revolution cut by arbitrary turbomachine blades

Author:	Wu, Chung-Hua
Additional Authors:	Brown, Curtis A.
Year:	1952
Document Type:	N/A
Series:	NACA Technical Notes
Report Number:	NACA-TN-2702
Link:	https://digital.library.unt.edu/ark:/67531/metadc55871/