Effect of Design Over-All Compressor Pressure Ratio Division on Acceleration Characteristics of Three Hypothetical Two-Spool Turbojet Engines

Author:	Filippi, Richard E.
Year:	1956
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E56D13
Link:	https://digital.library.unt.edu/ark:/67531/metadc62651/