The effects of suction through porous leading-edge surfaces on the aerodynamic characteristics of a 47.5 degree sweptback wing-fuselage combination at a Reynolds number of 4.4 x 10(exp 6)

Author:	Scallion, William I.
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-L51K15
Link:	https://digital.library.unt.edu/ark:/67531/metadc59855/