A simplified method for approximating the transient motion in angles of attack and sideslip during a constant rolling maneuver
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Sternfield, Leonard↗
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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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Low-speed roll effectiveness of a differentially deflected horizontal-tail surface on a 42 degree swept-wing model
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Boisseau, Peter C↗
An analog computer study of several stability augmentation schemes designed to alleviate roll-induced instability
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Creer, Brent Y↗
Theoretical investigation of the effect of rudder and stabilizer deflections on the angles of attack and sideslip in rapid rolls
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Woodling, C H↗
Dornier "Superwal" commercial seaplane with : two Rolls-Royce "Condor" 600 HP. engines
In November 1926, an exhibition flight of the Dornier giant flying boat was made for 3/4 of an hour. It was a larger version of the Dornier Wal, with a stepped hull, and wing stubs for lateral stability. It has a range of 1200 miles and is outfitted for baggage and 8 passengers.
SEAPLANES - DORNIER SUPERWAL (GER )↗
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↗
A simplified method for assessing the effect of steady rolling on angle of attack and sideslip
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Schmidt, Stanley F↗
Free-flight Investigation at Mach Numbers Between 0.5 and 1.7 of the Zero-lift Rolling Effectiveness and Drag of Various Surface, Spoiler, and Jet Controls on an 80 Degree Delta-wing Missile
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Schult, Eugene D↗
Tolerable Limits of Oscillatory Accelerations Due to Rolling Motions Experienced by One Pilot During Automatic-interceptor Flight Tests
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Brissenden, Roy F↗
Permeability Variation of a Taper-rolled Wire Cloth
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Diaguila, Anthony J↗
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↗
Free-flight Performance of a Rotating-vane-spoiler Roll Control System with Low Actuating Forces
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Schult, Eugene D↗
Free-flight Investigation of Comparative Zero-lift Rolling Effectiveness of a Leading-edge and a Trailing-edge Air-jet Spoiler on an Unswept Wing
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Kehlet, Alan B↗
Influence of automatic control of roll coupling and pitch-up on tail loads
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Stone, Ralph W , Jr↗
A Brief Analog Investigation of Inertia Coupling in Rolling Maneuvers of an Airplane Configuration Using a Variable-incidence Wing as the Longitudinal Control
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Gillis, Clarence L↗
The Effects of a Modified Roll-command System on the Flight-path Stability and Tracking Accuracy of an Automatic Interceptor
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Triplett, William C↗
Experimental determination of the effects of frequency and amplitude of oscillation on the roll-stability derivatives for a 60 degree delta-wing airplane model
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Fisher, Lewis R↗
Free-flight Roll Performance of a Steady-flow Jet-spoiler Control on an 80 Degree Delta-wing Missile Between Mach Numbers of 0.6 and 1.8
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Schult, Eugene D↗