A method for predicting the stability in roll of automatically controlled aircraft based on the experimental determination of the characteristics of an automatic pilot
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CONTROLS, MISSILE↗
SEARCH · Engineering Papers
Results for “Rolling”
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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A semiempirical method for estimating the rolling moment due to yawing of airplanes
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AIRFOILS - NACA 65A008 LOW DRAG↗
Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tipssupersonic leading edges
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THEORIES - WINGS - SUPERSONIC↗
Effect of an Unswept Wing on the Contribution of Unswept-tail Configuration to the Low-speed Static and Rolling-stability Derivatives of a Midwing Airplane Model
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SIDEWASH↗
Theoretical calculations of the lateral force and yawing moment due to rolling at supersonic speeds for sweptback tapered wings with streamwise tips : subsonic leading edges
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WINGS, SWEPTBACK - TAPERED↗
Analysis of the effects of wing interference on the tail contributions to the rolling derivatives
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Michael, William H , Jr↗
Some Effects of Varying the Damping in Pitch and Roll on the Flying Qualities of a Small Single-rotor Helicopter
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FLYING QUALITIES↗
Experimental Investigations of Rolling Performance of Straight and Sweptback Flexible Wings with Various Ailerons
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Cole, Henry A↗
Preliminary investigation of wear and friction properties under sliding conditions of materials suitable for cages of rolling-contact bearings
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Johnson, Robert L↗
Behavior of Vortex System Behind Cruciform Wings - Motions of Fully Rolled-up Vortices
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Sacks, Alvin H↗
Influence of Wing and Fuselage on the Vertical-tail Contribution to the Low-speed Rolling Derivatives of Midwing Airplane Models with 45 Degree Sweptback Surfaces
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Wolhart, Walter D↗
Estimation of the maximum angle of sideslip for determination of vertical-tail loads in rolling maneuvers
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Stone, Ralph W , Jr↗
Span load distributions resulting from constant angle of attack, steady rolling velocity, steady pitching velocity, and constant vertical acceleration for tapered sweptback wings with streamwise tips subsonic leading edges and supersonic trailing edg
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Hannah, Margery E↗
Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings I : Alloys Retaining Mechanical Properties to 600 F
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CONTACT SURFACES, SLIDING↗
Wear and Sliding Friction Properties of Nickel Alloys Suited for Cages of High-temperature Rolling-contact Bearings II : Alloys Retaining Mechanical Properties Above 600 F
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FRICTION AND LUBRICATION - SURFACE CONDITIONS↗
Span load distributions resulting from angle of attack, rolling, and pitching for tapered sweptback wings with streamwise tips
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Martin, John C↗
Effect of linear spanwise variations of twist and circular-arc camber on low-speed static stability, rolling, and yawing characteristics of a 45 degree sweptback wing of aspect ratio 4 and taper ratio 0.6
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Jaquet, Byron M↗
A preliminary study of the problem of designing high-speed airplanes with satisfactory inherent damping of the dutch roll oscillation
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FLYING QUALITIES↗