Effect of Design Compressor Pressure Ratio on Performance of Hypothetical Two-Spool Nuclear-Powered Turbojet Engines

Author:	Dugan, James F., Jr.
Year:	1955
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E55K04
Link:	https://digital.library.unt.edu/ark:/67531/metadc61676/