Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section

Author:	Dugan, Duane W
Year:	1952
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A52E01
Link:	https://digital.library.unt.edu/ark:/67531/metadc59152/