56 research outputs found
Additional Free-flight Tests of the Rolling Effectiveness of Several Wing-spoiler Arrangements at High Subsonic, Transonic, and Supersonic Speeds
Summary of Some Rocket-model Investigations of Effects of Wing Aspect Ratio and Thickness on Aileron Rolling Effectiveness Including Some Effects of Spanwise Aileron Location for Sweptback Wings with Aspect Ratio of 8.0
The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings with 0 Degree and 45 Degree Sweep at Subsonic, Transonic, and Supersonic Speeds
Summary of Some Effective Aerodynamic Twisting-moment Coefficients of Various Wing-control Configurations at Mach Numbers from 0.6 to 1.7 as Determined from Rocket-powered Models
Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface
Free-flight Investigation of the Rolling Effectiveness at High Subsonic, Transonic, and Supersonic Speeds of Leading-edge and Trailing-edge Ailerons in Conjunction with Tapered and Untapered Plan Forms
Rolling Effectiveness of All-movable Wings at Small Angles of Incidence at Mach Numbers from 0.6 to 1.6
Recent Experiences with Flutter Failure of Sweptback, Tapered Wings Having Outboard, Partial-span Spoiler Controls
Additional Results in a Free-flight Investigation of Control Effectiveness of Full-span, 0.2-chord Plain Ailerons at High Subsonic, Transonic, and Supersonic Speeds to Determine Some Effects of Wing Sweepback, Aspect Ratio, Taper, and Section Thickne
Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds
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