Investigation of Low-speed, Power-off Stability and Control Characteristics of a Model with a 35 Degree Sweptback Wing in the Langley Free-flight Tunnel
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Schade, Robert O↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Free-flight-tunnel Tests of a Target-seeking Glide-bomb Model with Flicker Lateral Control
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Mckinney, Marion O , Jr↗
Preliminary free-flight investigation of the effect of airfoil section on aileron rolling effectiveness at transonic and supersonic speeds
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Sandahl, Carl A↗
Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a 42.7 Degree Sweptback Wing Having Partial-span Ailerons
An investigation of the rolling effectiveness at transonic and supersonic speeds of partial-span ailerons on a 42.7 degree sweptback wing having symmetrical circular-arc airfoil sections of 10-percent thickness ratio normal to the wing quarter-chord line has been made by means of rocket-propelled test vehicles. The results are compared with results of a supersonic wind-tunnel test at Mach number 1.9.
CONTROLS, LATERAL↗
Free-flight Investigation of 16-inch Diameter Supersonic Ram-jet Unit
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Kinghorn, George F↗
Free-flight Investigation at Transonic and Supersonic Speeds of a Wing-aileron Configuration Simulating the D-558-2 Airplane
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Sandahl, Carl A↗
Free-flight Investigation of the Rolling Effectiveness of Several Delta Wing : Aileron Configurations at Transonic and Supersonic Speeds
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Sandahl, Carl A↗
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
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Strass, H Kurt↗
Langley Free-flight-tunnel Investigation of the Automatic Lateral Stability Characteristics of a Model Equipped with a Gyro Stabilizing Unit that Provided Either Flicker-type or Hunting Control
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Schade, Robert O↗
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 Section Thickness and Wing Sweepback
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Sandahl, Carl A↗
Additional Free-flight Tests of the Rolling Effectiveness of Several Wing-spoiler Arrangements at High Subsonic, Transonic, and Supersonic Speeds
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Strass, H Kurt↗
Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of Several Aileron Configurations on a Tapered Wing Having 42.7 Degrees Sweepback
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Sandahl, Carl A↗
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
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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
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Sandahl, Carl A↗
A Free-flight Technique for Measuring Damping in Roll by Use of Rocket-powered Models and Some Initial Results for Rectangular Wings
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Edmondson, James L↗
Preliminary results from a free-flight investigation at transonic and supersonic speeds of the longitudinal stability and control characteristics of an airplane configuration with a thin straight wing of aspect ratio 3
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Gillis, Clarence L↗
The Path and Motion of Scale Models of Jettisonable Nose Sections at Supersonic Speeds as Determined from an Investigation in the Langley Free-flight Apparatus
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Gale, Lawrence J↗
Free-flight Investigation at Transonic and Supersonic Speeds of the Rolling Effectiveness of a Partial-span Aileron on an Inversely Tapered Sweptback Wing
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Strass, H Kurt↗