A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed

Author:	Felix, A. Richard.
Additional Authors:	Emery, James C.
Year:	1953
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L53B26a
Series:	National Advisory Committee for Aeronautics research memorandum ;
Report Number:	L53B26a
Subjects:	Cascades (Fluid dynamics)
	Gas-turbines--Blades
	Axial flow compressors--Blades
Link:	https://hdl.handle.net/2027/mdp.39015086465211