The Aerodynamic Characteristics at Transonic Speeds of an All-movable, Tapered, 45 Degree Sweptback, Aspect-ratio-4 Tail Deflected about a Skewed Hinge Axis and Equipped with an Inset Unbalancing Tab

The Aerodynamic Characteristics at Transonic Speeds of an All-movable, Tapered, 45 Degree Sweptback, Aspect-ratio-4 Tail Deflected about a Skewed Hinge Axis and Equipped with an Inset Unbalancing Tab PDF Author: James M. Watson
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Category :
Languages : en
Pages : 40

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Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 508

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Research Abstracts

Research Abstracts PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 442

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Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degrees Sweptback Wing of Aspect Ratio 3 Having a Full-span Flap-type Control

Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degrees Sweptback Wing of Aspect Ratio 3 Having a Full-span Flap-type Control PDF Author: Vernard E. Lockwood
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 35

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The aerodynamic characteristics in pitch and the control characteristics of a wing-flap combination have been determined for a wing having a quarter-chord line sweep of 45.58 degrees, an aspect ratio of 3, a taper ratio of 0.5, and an NACA 64A010 airfoil section measured in a plane at an angle of 45 degrees to the plane of symmetry. The wing employed a 25.4-percent-chord full-span plain flap-type control with a removable seal so that the effects of a relatively small gap could be determined. The investigation covered a Mach number range from 0.6 to 1.17 at angles of attack of 0, 4, and 8 degrees through a control-surface deflection range from -27 degrees to approximately 5 degrees. These data were obtained from the Langley high-speed 7- by 10-foot-tunnel transonic bump.

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections

Investigation at Transonic Speeds of the Loading Over a 45 Degree Sweptback Wing Having an Aspect Ratio of 3, a Taper Ratio of 0.2, and NACA 65A004 Airfoil Sections PDF Author: Jack F. Runckel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 104

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An investigation at transonic speeds of the loading over a 45 degree sweptback wing having an aspect ratio of 3, a taper ratio of 0.2, and NACA 65A004 airfoil sections has been conducted in the Langley16-foot transonic tunnel. Pressure measurements on the wing-body combination were obtained at angles of attack from 0 to 26 degrees at Mach numbers from 0.80 to 0.98 and from 0 to about 12 degrees at Mach numbers from 1.00 to 1.05. Reynolds number, based on the wing mean aerodynamic chord, varied from 7,000,000 to 8,500,000 over the test Mach number range.

Hinge-moment and Other Aerodynamic Characteristics at Transonic Speeds of a Quarter-span Spoiler on a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3

Hinge-moment and Other Aerodynamic Characteristics at Transonic Speeds of a Quarter-span Spoiler on a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 PDF Author: Joseph E. Fikes
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ISBN:
Category :
Languages : en
Pages : 22

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Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2

Transonic Aerodynamic Characteristics of a Wing-body Combination Having a 52.20 Sweptback Wing of Aspect Ratio 3 with Conical Camber and Designed for a Mach Number of 2 PDF Author: William B. Igoe
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ISBN:
Category : Aerodynamics
Languages : en
Pages : 56

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Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-span Flap Type of Control with Overhang Balance

Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degree Sweptback Wing of Aspect Ratio 3 Having a Full-span Flap Type of Control with Overhang Balance PDF Author: Vernard E. Lockwood
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degrees Sweptback Wing of Aspect of Aspect Ratio 3 Having a Full-span Flap-tyre Control

Aerodynamic Characteristics at Transonic Speeds of a Tapered 45 Degrees Sweptback Wing of Aspect of Aspect Ratio 3 Having a Full-span Flap-tyre Control PDF Author: Vernard E. Lockward
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

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The Aerodynamic Characteristics at Transonic Speeds of a Model with a 45 Degree Sweptback Wing, Including Effect of Leading-edge Slats and a Low Horizontal Tail

The Aerodynamic Characteristics at Transonic Speeds of a Model with a 45 Degree Sweptback Wing, Including Effect of Leading-edge Slats and a Low Horizontal Tail PDF Author: Jack F. Runckel
Publisher:
ISBN:
Category :
Languages : en
Pages : 60

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