Investigation of a simple device for preventing separation due to shock and boundary-layer interaction

Author:	Donaldson, Coleman duP.
Year:	1950
Document Type:	NACA
Issuing Agency:	National Advisory Committee for Aeronautics,
SUDOC:	Y 3.N 21/5:15/L50B02A
Series:	NACA research memorandum ;
Report Number:	L50B02A
Subjects:	Turbulence
	Shock waves
	Charts, diagrams, etc
	Vortex generators
	Boundary layer
	Aerofoils
Link:	https://hdl.handle.net/2027/mdp.39015086464644