Calculated effects of turbine rotor-blade cooling-air flow, altitude, and compressor bleed point on performance of a turbojet engine

Author:	Arne, Vernon L
Year:	1951
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-E51E24
Link:	https://digital.library.unt.edu/ark:/67531/metadc58909/