Lateral Control Characteristics and Dihedral Effect of a Wing-body Combination with a Variable Incidence Triangular Wing and Wing-tip Ailerons at a Mach Number of 1.52
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Scherrer, Richard↗
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Results for “wings”
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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Aerodynamic Study of a Wing-fuselage Combination Employing a Wing Swept Back 63 Degrees : Effect of Reynolds Number at Supersonic Mach Numbers on the Longitudinal Characteristics of a Wing Twisted and Cambered for Uniform Load
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Heitmeyer, John C↗
A Transonic-wing Investigation in the Langley 8-foot High-speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2 : Wing-fuselage Configuration Having a Wing of 60 Degree Sweepback, Aspect-ratio 4, Taper Ratio 0.6, and NACA 65A006 Airf
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Wood, Raymond B↗
Wing-on and Wing-off Longitudinal Characteristics of an Airplane Configuration Having an Thin Unswept Tapered Wing of Aspect Ratio 3, as Obtained from Rocket-propelled Models at Mach Numbers from 0.8 to 1.4
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Gillis, Clarence L↗
A Transonic-wing Investigation in the Langley 8-foot High-speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2. : Wing-fuselage Configuration Having a Wing of 0 Degrees Sweepback, Aspect Ratio 4.0,taper Ratio 0.6, and NACA 65A006 Ai
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Cahn, Maurice S↗
A Transonic Wing Investigation in the Langley 8-foot High-speed Tunnel at High Subsonic Mach Numbers and at a Mach Number of 1.2 : Wing-fuselage Configuration Having a Wing of 35 Degrees Sweepback, Aspect Ratio 4, Taper Ratio 0.6, and NACA 65A006
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Henry, Beverly Z , Jr↗
The effects on the aerodynamic characteristics of reversing the wing of a triangular wing-body combination at transonic speeds as determined by the NACA wing-flow method
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Mckay, James M↗
An Investigation of Longitudinal Control Characteristics of a Wing-tip Control Surface on a Sweptback Wing at Transonic Speeds by the NACA Wing-flow Method
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Trant, James P , Jr↗
The Effects on the Aerodynamic Characteristics of Varying the Wing Thickness Ratio of a Triangular Wing-body Configuration at Transonic Speeds from Tests by the NACA Wing-flow Method
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Hall, Albert W↗
Effects of Simulated Skin Wrinkles on the Wing Surface on the Aerodynamic Characteristics of Two Wing-body Combinations Employing Wings of Low Aspect Ratio at Subsonic and Supersonic Speeds
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Heitmeyer, John C↗
Some Effects of Spoiler Height, Wing Flexibility, and Wing Thickness on Rolling Effectiveness and Drag of Unswept Wings at Mach Numbers Between 0.4 and 1.7
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Fields, E M↗
Investigation of three tapered 45 degree sweptback cambered and twisted wings covering a simultaneous variation in aspect ratio and thickness ratio and of one related symmetrical wing at transonic speeds by the wing-flow method
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Johnson, Harold I↗
Aerodynamic characteristics extended to high angles of attack at transonic speeds of a small-scale 0 degree sweep wing, 45 degree sweptback wing, and 60 degree delta wing
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Wiley, Harleth G↗
Transonic characteristics of a 45 degree sweptback wing-fuselage combination : effect of longitudinal wing position and division of wing and fuselage forces and moments
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Hallissy, Joseph M↗
Distribution of lift and pitching moment between wing and fuselage and effects of wing flexibility and dive brake on a 1/30-scale semispan model of the Bell X-5 airplane at transonic speeds as determined by the NACA wing-flow method
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Morris, Garland J↗
Lateral Control Characteristics of Two Structurally Similar Flexible Wings with 45 Degrees Sweep: a Sweptback Wing and a Wing with M Plan Form
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Naeseth, Rodger L↗
Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form : Effects of Various Tail Arrangements on Wing-on and Wing-off Static Longitudinal and Lateral Stability Characteristics
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Dunning, Robert W↗
The Effect of Wing Height on the Longitudinal Characteristics at High Subsonic Speeds of a Wing-fuselage-tail Combination Having a Wing with 40 Degrees of Sweepback and NACA Four-digit Thickness Distribution
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Dickson, Jerald K↗