Effect of nose shape and trailing-edge bluntness on the aerodynamic characteristics of an unswept wing of aspect ratio 3.1, taper ratio 0.4, and 3-percent thickness

Author:	Heitmeyer, John C.
Year:	1954
Document Type:	N/A
Series:	NACA Research Memorandums
Report Number:	NACA-RM-A54A04
Link:	https://digital.library.unt.edu/ark:/67531/metadc60094/