Search U.S. government technical reports digitized or harvested by TRAIL.
Flight investigation of an aileron and a spoiler on a wing of the X-3 airplane plan form at Mach numbers from 0.5 to 1.6
Effect of a wing leading-edge flap and chord-extension on the high subsonic control characteristics of an aileron located at two spanwise positions
Investigation at transonic speeds of the hinge-moment characteristics of a 1/8-scale model of the X-1E aileron