Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Author:	Lewis, George W.,
Additional Authors:	Serovy, G. K., Schwenk, Francis C.
Year:	1954
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/E53L21a
Series:	NACA research memorandum ;
Report Number:	E53L21a
Subjects:	Axial flow compressors--Design and construction
	Axial flow compressors--Blades--Testing
Link:	https://hdl.handle.net/2027/mdp.39015086490052