Acceleration of high-pressure-ratio single-spool turbojet engine as determined from component performance characteristics 1: effect of air bleed at compressor outlet

Author:	Rebeske, John J., Jr.
Year:	1953
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E53A09
Link:	https://digital.library.unt.edu/ark:/67531/metadc59518/