Effects of three types of blunt trailing edges on the aerodynamic characteristics of a plane tapered wing of aspect ratio 3.1, with a 3-percent- thick biconvex section
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Dugan, Duane W↗
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Results for “ASPECT RATIO”
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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Effects of finite span on the section characteristics of two 45 degree swept-back wings of aspect ratio 6
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Hunton, Lynn W↗
Effect of Vertical Location of a Horizontal Tail on the Static Longitudinal Stability Characteristics of a 45 Degree Sweptback-wing-fuselage Combination of Aspect Ratio 8 at a Reynolds Number of 4.0 x 10(exp 6)
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Salmi, Reino J↗
Preliminary Investigation of Control Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Horn-balanced Full-span Control
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Lowry, John G↗
Aerodynamic Characteristics of Two-plane, Unswept Tapered Wings of Aspect Ratio 3 and 3-percent Thickness from Tests on a Transonic Bump
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Emerson, Horace F↗
A Transonic Wind-tunnel Investigation of the Aerodynamic Characteristics of Three 4-percent-thick Wings of Sweepback Angles 10.8 Degrees, 35 Degrees, and 47 Degrees, Aspect Ratio 3.5, and Taper Ratio 0.2 in Combination with a Body
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Bielat, Ralph P↗
The Effect of an Operating Propeller on the Aerodynamic Characteristics at High Subsonic Speeds of a Model of a Vertical-rising Airplane Having an Unswept Wing of Aspect Ratio 3
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Sutton, Fred B↗
Low-speed Longitudinal Aerodynamic Characteristics of a Twisted and Cambered Wing of 45 Degree Sweepback and Aspect Ratio 8 with and Without High-lift and Stall-control Devices and a Fuselage at Reynolds Numbers from 1.5 x 10(exp 6) to 4.8 x 10(exp 6
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Salmi, Reino J↗
Free-flight-tunnel investigation of the dynamic lateral stability and control characteristics of a high-aspect-ratio bomber model with a sweptback-wing fighter model attached to each wing tip
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Bennett, Charles V↗
Aerodynamic characteristics at supersonic speeds of a series of wing-body combinations having cambered wings with an aspect ratio of 3.5 and a taper ratio of 0.2 : effects of sweep angle and thickness ratio on the aerodynamic characteristics in pitch
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Robinson, Ross B↗
Small-scale Transonic Investigation of the Effects of Full-span and Partial-leading-edge Flaps on the Aerodynamic Characteristics of a 50 Degree 38 Foot Sweptback Wing of Aspect Ratio 2.98
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Spreeman, Kenneth P↗
Effects of Horizontal-tail Position and Aspect Ratio on Low-speed Static Longitudinal Stability and Control Characteristics of a 60 Degree Triangular-wing Model Having Twin Triangular All-movable Tails
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Jaquet, Byron M↗
Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket Propelled Vehicles
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Bland, William M , Jr↗
Small scale transonic investigation of the effects of partial-span leading-edge camber on the aerodynamic characteristics of a 50 degree 38 foot sweptback wing of aspect ratio 2.98
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Alford, William J , Jr↗
Transonic aerodynamic characteristics of three W-plan-form wings having aspect ratio 8, taper ratio 0.45, and NACA-63A-series airfoil sections
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Morrison, William D , Jr↗
The Transonic Characteristics of 38 Cambered Rectangular Wings of Varying Aspect Ratio and Thickness as Determined by the Transonic Bump Technique
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Nelson, Warren H↗
Lateral-control investigation at transonic speeds of retractable spoiler and plug-type spoiler-slot ailerons on a tapered 60 degree sweptback wing of aspect ratio 2 : transonic-bump method
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Hammond, Alexander D↗
The Longitudinal Characteristics at Mach Numbers up to 0.92 of a Cambered and Twisted Wing Having 40 Degrees of Sweepback and an Aspect Ratio of 10
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Edwards, George G↗