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

Duane W. Dugan
naca-rm-a52e01
Jul 1952


Effects of wing trailing-edge bluntness upon the aerodynamic characteristics of a wing-body combination have been experimentally investigated at Mach numbers ranging from 1.5 to 3.8 million.

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