Application of supersonic vortex-flow theory to the design of supersonic impulse compressor- or turbine-blade sections

Author:	Boxer, Emanuel
Additional Authors:	Sterrett, James R.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L52B06
Link:	https://digital.library.unt.edu/ark:/67531/metadc59156/