Search U.S. government technical reports digitized or harvested by TRAIL.
Lateral-control investigation of flap-type controls on a wing with quarter-chord line sweptback 35©�, aspect ratio 4, taper ratio 0.6, and NACA 65A006 airfoil section.Transonic-bump method
Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at transonic and supersonic speeds
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered winds at transonic speeds
Aerodynamic characteristics of a spoiler-slot-deflector control on a 45©� sweptback wing at Mach numbers of 1.61 and 2.01
Recent control studies