The aerodynamic characteristics throughout the subsonic speed range of a thin, sharp-edged horizontal tail of aspect ratio 4 equipped with a constant-chord elevator

Angelo Bandettini, Verlin D. Reed
Jun 1949

Wind-tunnel tests have been made of a semispan model of a horizontal tail of aspect ratio 4 and taper ratio 0.5 equipped with a full-span constant-chord elevator having an area equal to 20 percent of the total semispan-tail area.

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