Static stability and control of canard configurations at Mach numbers from 0.70 to 2.22 :longitudinal characteristics of a triangular wing and canard

Boyd, John W., Peterson, Victor L.
naca-rm-a57j15
1958


The canard configuration investigated at Mach numbers from 0.70 to 2.22 consisted of a triangular wing and triangular movable canard, both of aspect ratio 2.0, a low-aspect-ratio vertical tail, and a fineness ratio 12.5 Sears-Haack body.

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