NACA 65-series compressor rotor performance with varying annulus-area ratio, solidity, blade angle, and Reynolds number and comparison with cascade results

Author:	Schulze, Wallace M.
Additional Authors:	Erwin, John R., Ashby, George C.
Year:	1953
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L52L17
Series:	National Advisory Committee for Aeronautics research memorandum ;
Report Number:	L52L17
Subjects:	Cascades (Fluid dynamics)
	Reynolds number
	Compressors--Performance
	Axial flow compressors--Blades
Link:	https://hdl.handle.net/2027/mdp.39015086465187