Canard model had twisted wing with 67° of sweepback and aspect ratio of 2.91 and 3-trapezoidal canard surfaces having ratios of exposed area to wing area of 0.032, 0.076, and 0.121; details of outboard tail model; longitudinal characteristics of models were obtained for various control deflections, and lateral stability derivatives over maximum test angle of attack of -2 to 22° for lower test Mach numbers.
Aerodynamic characteristics of canard and outboard-tail airplane model at high subsonic speeds
NASA -- Tech Note
1961
67 pages
Report
English
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