Influence of wall boundary layer upon the performance of an axial-flow fan rotor

Author:	Boxer, Emanuel.
Year:	1947
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/L6J18b
Series:	NACA research memorandum ;
Report Number:	L6J18b
Subjects:	Boundary layer
	Axial flow compressors--Blades--Aerodynamics
Link:	https://hdl.handle.net/2027/mdp.39015086464248