An Analog Study of the Relative Importance of Various Factors Affecting Roll Coupling
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Weil, Joseph↗
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Flight and analytical study of roll requirements of a fighter airplane
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Adams, James J↗
Wind-tunnel investigation of damping in roll at supersonic speeds of triangular wings at angles of attack
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Mcdearmon, Russell W↗
Wind-tunnel Investigation of the Damping in Roll of the Douglas D-558-II Research Airplane and Its Components at Supersonic Speeds
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Mcdearmon, Russell W↗
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↗
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↗