Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds

John W. Boyd
Jul 1952

The results of an experimental investigation of flap-type controls on a low-aspect-ratio triangular wing using NACA 0005-63 sections are presented for a constant-chord and a constant-percent-chord control surface. Two flap profiles were investigated, one having a true contour and the other a blunt trailing edge.

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