The static longitudinal characteristics at Mach numbers up to 0.95 of a triangular-wing canard model having a triangular control

Jack D. Stephenson, Ralph Selan
naca-rm-a51i07
Dec 1951


The longitudinal stability and control of a canard model employing a triangular wing of aspect ratio 2 and a control surface of identical plan form have been investigated at Mach numbers up to 0.95. The sections of the wing in streamwise planes were the NACA 0008-63 and the sections of the canard surface were the NACA 0005-63.

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-a51i07.pdf