Flight Investigation of the Effect of Thickening the Aileron Trailing Edge on Control Effectiveness for Sweptback Tapered Wings Having Sharp-and Round-nose Sections
Explore the source record for details and available documents.
Strass, H Kurt↗
Engineering topics
Strass, H Kurt
Publications and source records attributed to Strass, H Kurt.
Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a Partial-span Aileron on an Inversely Tapered Sweptback Wing
Explore the source record for details and available documents.
Strass, H Kurt↗
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
Explore the source record for details and available documents.
Strass, H Kurt↗
Comparative tests of the rolling effectiveness of constant-chord, full-delta, and half-delta ailerons on delta wings at transonic and supersonic speeds
Explore the source record for details and available documents.
Sandahl, Carl A↗
Effects of Some Airfoil-section Variations on Wing-aileron Rolling Effectiveness and Drag as Determined in Free Flight at Transonic and Supersonic Speeds
Explore the source record for details and available documents.
Sandahl, Carl A↗
Additional Free-flight Tests of the Rolling Effectiveness of Several Wing-spoiler Arrangements at High Subsonic, Transonic, and Supersonic Speeds
Explore the source record for details and available documents.
Strass, H Kurt↗
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
Explore the source record for details and available documents.
Strass, H Kurt↗
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
Explore the source record for details and available documents.
Sandahl, Carl A↗
Tests of a Full-scale Horizontal Tail Surface in the Langley 16-foot High-speed Tunnel
Explore the source record for details and available documents.
Schueller, Carl F↗
Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface
Explore the source record for details and available documents.
WIND TUNNEL TESTS - NACA - HIGH-SPEED (16')↗