Effect of Horizontal Tail on Low-speed Static Lateral Stability Characteristics of a Model Having 45 Degree Sweptback Wing and Tail Surfaces
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WINGS, SWEPTBACK - CHARACTERISTICS↗
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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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Experiments with three horizontal empennages
The main objective of these experiments was to determine how the air forces on the whole empennage are affected by varying the size of the elevator without changing the size of the whole empennage. The secondary objective was to determine how the magnitude of the air forces acting on the elevator (or the elevator moments) are affected by varying the angle of attack of the whole empennage, or of the elevator alone.
CONTROL UNITS - WIND TUNNEL TESTS↗
Comparison between calculated and measured loads on wing and horizontal tail in pull-up maneuvers
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LOADING, WING↗
Investigation of Effect of Sideslip on Lateral Stability Characteristics II : Rectangular Midwing on Circular Fuselage with Variations in Vertical-tail Area and Fuselage Length with and Without Horizontal Tail Surface
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TAIL SURFACES, HORIZONTAL↗
Investigation of Effect of Sideslip on Lateral Stability Characteristics III : Rectangular Low Wing on Circular Fuselage with Variations in Vertical-tail Area and Fuselage Length With and Without Horizontal Tail Surface
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MONOPLANES, LOW-WING↗
Investigation of Effect of Sideslip on Lateral Stability Characteristics I : Circular Fuselage with Variations in Vertical-Tail Area and Tail Length with and Without Horizontal Tail Surface
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TAIL SURFACES - AREA↗
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics V : symmetrically tapered wing with a circular fuselage having a horizontal and a vertical tail
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WING FLAPS, SPLIT - PARTIAL-SPAN (20%-CHORD)↗
Power-On Longitudinal-Stability and Control Tests of the 1/8-scale Model of the Brewster F2A Airplane Equipped with Full-Span Slotted Flaps and a New Horizontal Tail
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WING FLAPS, SLOTTED - FULL-SPAN↗
Determination of the effect of horizontal-tail flexibility on longitudinal control characteristics
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CONTROL, LONGITUDINAL↗
Preliminary Flight Research on an All-Movable Horizontal Tail as a Longitudinal Control for Flight at High Mach Numbers
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ELEVATORS, BALANCED-CURTISS P-42↗
Effect of elevator-profile modifications and trailing-edge strips on elevator hinge-moment and other aerodynamic characteristics of a full-scale horizontal tail surface
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WIND TUNNEL TESTS - NACA - HIGH-SPEED (16')↗
Wind-Tunnel Investigation of a Section of the Horizontal Tail Surface for the Bell XP-63 Airplane
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AIRFOILS - NACA 66,2X-009 (MODIFIED) - CHAR , MOME↗
High-Speed Wind-tunnel Tests of Semispan Horizontal Tails with Fabric-Covered and Metal-Covered Elevators for a Bomber Airplane
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TABS, ELEVATOR - DOUGLAS B-42↗
Effect of Fabric Deflection at High Speeds on the Aerodynamic Characteristics of the Horizontal Tail Surface of an SB2D-1 Airplane
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ELEVATORS-HINGE MOMENTS↗
Wind-Tunnel Investigation of a Revised Horizontal Tail Surface for the Grumman TBF-1 Airplane
No abstract available
TABS, ELEVATOR - GRUMMAN TBF-1↗
Comparison of fixed-stabilizer, adjustable- stabilizer and all-movable horizontal tails
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CONTROL STICKS - FORCES↗
Flight studies of the horizontal-tail loads experienced by a fighter airplane in abrupt maneuvers
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STALLING↗
Computation of hinge-moment characteristics of horizontal tails from section data
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CONTROL SURFACES, BALANCED-AERODYNAMIC↗