Some Effects of Aileron Span, Aileron Chord, and Wing Twist on Rolling Effectiveness as Determined by Rocket-powered Model Tests and Theoretical Estimates
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Strass, H Kurt↗
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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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Some effects of external wing tip stores on the rolling effectiveness and drag of plain and half-delta tip ailerons on a 4-percent-thick, tapered, upswept wing
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English, Roland D↗
Effects of overhang balance on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing
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Guy, Lawrence D↗
Free-flight Investigation to Determine Some Effects of Tail Damping and Wing-tail Interference on the Rolling Effectiveness of Inboard and Outboard Ailerons on an Untapered Sweptback Wing
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English, Roland D↗
Free-flight Investigation, Including Some Effects of Wing Aeroelasticity, of the Rolling Effectiveness of an All-movable Horizontal Tail with Differential Incidence at Mach Numbers from 0.6 to 1.5
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English, Roland D↗
Effects of a Detached Tab on the Hinge-moment and Effectiveness Characteristics of an Unswept Trailing-edge Control on a 60 Degree Delta Wing at Mach Numbers from 0.75 to 1.96
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Morris, Odell A↗
Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60 degree delta wing at Mach numbers form 0.75 to 1.96
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Guy, Lawrence D↗
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of plain spoilers on thin untapered wings at transonic speeds
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Hammond, Alexander D↗
The effect of fluid injection on the compressible turbulent boundary layer : the effect of skin friction of air injected into the boundary layer of a cone at M = 2.7
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Tendeland, Thorval↗
Experimental and Theoretical Studies of Interference Effects on the Damping in Roll of the Bell X-1A Research Airplane at Supersonic Speeds (including Canopy Shape Effects)
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Mcdearmon, Russel W↗
Free-flight Investigation to Determine Some Effects of Tail Damping and Wing-tail Interference on the Rolling Effectiveness of Ailerons and a Spoiler on a Modified-delta Wing at Mach Numbers from 0.6 to 1.5
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English, Roland D↗
Wind-tunnel investigation of the effect of aspect ratio and chordwise location on effectiveness of spoiler-slot-deflector controls on thin untapered wings at transonic speeds
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Hammond, Alexander D↗
Wind-tunnel investigation of the effect of sweep and taper ratio on effectiveness of spoiler-slot-deflector controls on aspect-ratio-4 wings at transonic speeds
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Hammond, Alexander D↗
An experimental investigation of sting-support effects on drag and a comparison with jet effects at transonic speeds
Various dummy stings were tested on the rear of a related series of afterbody shapes for Mach numbers from 0.80 to 1.10 and Reynolds numbers based on body length from 15.0 x 16 to the 6th power to 17.4 x 10 to the 6th power. A method is presented whereby approximate sting interference corrections can be made to models having afterbody shapes and sting supports similar to those of these tests if the Reynolds numbers are of the same order of magnitude and a turbulent boundary layer exists at the model base. Also presented is an analysis of jet duplication by use of a sting.
Cahn, Maurice S↗
Determination of the Effect of Wing Flexibility on Lateral Maneuverability and a Comparison of Calculated Rolling Effectiveness with Flight Results
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WINGS, FLEXIBLE↗
A study of the effects of radii of gyration and altitude on aileron effectiveness at high speed
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AIRPLANES, PURSUIT↗
Force Balance and Substorm Effects in the Magnetotail and Nonguiding Center Motion and Substorm Effects in the Magnetotail
Most of the work carried out to date on this project is summarized in the enclosed reprints of two papers that were just published. The earlier paper that is also enclosed, Structure of the Magnetotail, by D. L. Larson and R. L. Kaufmann, was primarily intended to describe our Consistent Orbit Tracing (COT) technique and to show that the resulting magnetotail models were in good agreement with published experimental observations. The following are the most important results from the two new papers.
Kaufmann, Richard L.↗
Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor. II - Effect on Over-All Performance Characteristics of Increasing Twelfth through Fifteenth Stage Stator-Blade Angles 3 deg
The stator-blade angles in the twelfth through fifteenth stages of a 16-stage axial-flow compressor were increased 3O. The over-all performance of this modified compressor is compared to the performance of the compressor with original blade angles. The matching characteristics of the modified compressor and a two-stage turbine were obtained and compared to those of the compressor with original blade angles and the same turbine.
Hatch, James E.↗