Investigation at low speeds of the effect of aspect ratio and sweep on rolling stability derivatives of untapered wings
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AIRFOILS - NACA 0012↗
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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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Theoretical lift and damping in roll of thin sweptback wings of arbitrary taper and sweep at supersonic speeds subsonic leading edges and supersonic trailing edges
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DAMPING IN ROLL↗
The effect of torsional flexibility on the rolling characteristics at supersonic speeds of tapered unswept wings
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WINGS - TORSION↗
Damping-in-roll calculations for slender swept-back wings and slender wing-body combinations
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WINGS, SWEPTBACK↗
Summary of the theoretical lift, damping-in-roll, and center-of-pressure characteristics of various wing plan forms at supersonic speed
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WINGS - LEADING EDGES↗
Determination of the Rate of Roll of Pilotless Aircraft Research Models by Means of Polarized Radio Waves
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RADIOSONDES↗
Theoretical lift and damping in roll of thin sweptback tapered wings with raked-in and cross-stream wing tips at supersonic speeds.subsonic leading edges
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LIFT - WINGS, SWEPTBACK↗
Theory of Helicopter Damping in Pitch or Roll and a Comparison with Flight Measurements
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DAMPING IN PITCH↗
On the effect of subsonic trailing edges on damping in roll and pitch of thin sweptback wings in a supersonic stream
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DAMPING IN ROLL↗
Estimation of the damping in roll of supersonic-leading-edge wing-body combinations
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INTERFERENCE - WINGS & BODIES↗
Damping in roll of cruciform and some related delta wings at supersonic speeds
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DAMPING IN ROLL↗
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↗
Tests of a 0.30-scale Semispan Model of the Douglas XTB2D-1 Airplane Wing and Fuselage Combination in the NACA 19-Foot Pressure Tunnel II : Roll-Flap Positioning and Lateral-Control Investigation
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WIND TUNNEL TESTS - NACA & PRESSURE (19')↗
Charts for the determination of wing torsional stiffness required for specified rolling characteristics or aileron reversal speed
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ROLLING↗
Lifting-Surface-Theory Values of the Damping in Roll and of the Parameter Used in Estimating Aileron Stick Forces
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CONTROL STICKS - FORCES↗
Analysis of vertical-tail loads in rolling pull-out maneuvers
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LOADS - TAIL SURFACES↗
Tunnel-wall corrections to rolling and yawing moments due to aileron deflection in closed rectangular wind tunnels
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WIND TUNNEL TESTS - CORRECTIONS↗
On-Orbit Flight Testing of the Roll-Out Solar Array
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Roll Out Solar Array↗