Investigation of the Effect of Sweep on the Flutter of Cantilever Wings
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Barmby, J G↗
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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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Effect of Wing Sweep, Taper, and Thickness Ratio on the Transonic Drag Characteristics of Wing-body Combinations
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Thompson, Jim Rogers↗
High-Speed Wind-Tunnel Investigation of the Lateral Control Characteristics of Plain Ailerons on a Wing with Various Amounts of Sweep
A three-dimensional investigation of straight-sided-profile plain ailerons on a wing with 30 degrees and 45 degrees of sweepback and sweepforward was made in a high-speed wind tunnel for aileron deflections from -10 degrees to 10 degrees and at Mach numbers from 0.60 to 0.96. Wing configurations of 30 degrees generally reduced the severity of the large changes in rolling-moment and aileron hinge-moment coefficients experienced by the upswept wing configurations as the result of compression shock and extended to higher Mach numbers the speeds at which such changes occurred.
Luoma, Arvo A.↗
Pressure-distribution Measurements over an Extensible Leading-edge Flap on Two Wings Having Leading-edge Sweep of 42 Degrees and 52 Degrees
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Salmi, Reino J↗
Low-speed Wind-tunnel Investigation of the Longitudinal Stability Characteristics of a Model Equipped with a Variable-sweep Wing
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Donlan, Charles J↗
Effects of Mach Number and Sweep on the Damping-in-roll Characteristics of Wings of Aspect Ratio 4
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Kuhn, Richard E↗
Full-scale Investigation of Boundary-layer Control by Suction Through Leading-edge Slots on a Wing-fuselage Configuration Having 47.5 Degree Leading-edge Sweep with and Without Flaps
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Pasamanick, Jerome↗
Longitudinal Characteristics at Mach Number of 1.24 of 1/30-scale Semispan Model of Bell X-5 Variable-sweep Airplane with Wing Swept Back 60 Degrees : from Tests by NACA Wing-flow Method
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Silsby, Norman S↗
The Effect of Spanwise Aileron Location on the Rolling Effectiveness of Wings with 0 Degree and 45 Degree Sweep at Subsonic, Transonic, and Supersonic Speeds
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Strass, H Kurt↗
Aerodynamic Characteristics at a Mach Number of 1.38 of Four Wings of Aspect Ratio 4 Having Quarter-chord Sweep Angles of 0 Degrees, 35 Degrees, 45 Degrees, and 60 Degrees
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Kemp, William B , Jr↗
Effects of sweep on the maximum-lift characteristics of four aspect-ratio-4 wings at transonic speeds
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Turner, Thomas R↗
Effects of a fuselage flap dive brake on the aerodynamic characteristics of 1/30 scale semispan model of the Bell X-5 variable-sweep airplane at a Mach number 1.24 as determined by the NACA wing flow method
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Kennedy, Robert M↗
Effects of sweep on the damping-in-roll characteristics of three sweptback wings having an aspect ratio of 4 at transonic speeds
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Lockwood, Vernard E↗
Aerodynamic Characteristics at Transonic Speeds of a Wing Having a 45 Degree Sweep, Aspect Ratio 8, Taper Ratio 0.45, and Airfoil Sections Varying from the NACA 63A010 Section at the Root to the NACA 63A006 Section at the Tip.
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Morrison, William D , Jr↗
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↗
Wind-tunnel Investigation of the Aerodynamic Characteristics in Pitch of Wing-fuselage Combinations at High- Subsonic Speeds : Sweep Series
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Wiggins, James W↗
Pressure Distribution at Low Speed on a Model Incorporating a W Wing with Aspect Ratio 6, 45 Degrees Sweep, Taper Ratio 0.6, and an NACA 65A009 Airfoil Section
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Polhamus, Edward C↗
Wind-tunnel Investigation of the Static Lateral Stability Characteristics of Wing-fuselage Combinations at High Subsonic Speeds : Sweep Series
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Kuhn, Richard E↗