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
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.

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