Evaluation of a compressor bleed system for rim cooling the turbine wheel of a turbojet engine

Author:	Morse, C. R.
Additional Authors:	Kemp, R. H.
Year:	1954
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/E53L22b
Series:	NACA research memorandum ;
Report Number:	E53L22b
Subjects:	Gas-turbine disks--Cooling--Testing
	Airplanes--Turbojet engines--Compressors--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086429837