Investigation of Turbines for Driving Supersonic Compressors 2: Performance of First Configuration With 2.2 Percent Reduction in Nozzle Flow Area

Author:	Stewart, Warner L.
Additional Authors:	Schum, Harold J.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E52E26
Link:	https://digital.library.unt.edu/ark:/67531/metadc59457/