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
naca-rm-a52d01c
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.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1952/naca-rm-a52d01c.pdf