Comparison of results of experimental and theoretical studies of blade-outlet boundary-layer characteristics of stator blade for a high subsonic Mach number turbine

Author:	Hauser, Cavour H.
Additional Authors:	Nusbaum, William J.
Year:	1957
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N21/5:15/E56K29a
Series:	NACA research memorandum ;
Report Number:	E56K29a
Subjects:	Boundary layer
	Aircraft gas-turbines--Blades
	Turbines--Blades--Aerodynamics
Link:	https://hdl.handle.net/2027/mdp.39015086464040