An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Download

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An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

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Book Description

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 286

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Book Description

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degree Swepptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 282

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Book Description

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-Percent-Thick 30 Deg Sweptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-Percent-Thick 30 Deg Sweptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30° Sweptback Wing at Transonic Speeds

An Investigation of Wing and Aileron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30° Sweptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 282

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Book Description

An Investigation of Wing and Alleron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degrees Sweptback Wing at Transonic Speeds

An Investigation of Wing and Alleron Loads Due to Deflected Inboard and Outboard Ailerons on a 4-percent-thick 30 Degrees Sweptback Wing at Transonic Speeds PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 282

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Book Description

Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron

Normal-force and Hinge-moment Characteristics at Transonic Speeds of Flap-type Ailerons at Three Spanwise Locations on a 4-percent-thick Sweptback-wing-body Model and Pressure-distribution Measurements on an Inboard Aileron PDF Author: Jack F. Runckel
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 60

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Book Description

A Wind-tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds

A Wind-tunnel Investigation of the Wing Loads Due to Deflected Inboard Ailerons on a 45 Degree Sweptback Wing at Transonic Speeds PDF Author: Astwood R. Jr Heath
Publisher:
ISBN:
Category :
Languages : en
Pages : 100

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Book Description

Loads on Wings Due to Spoilers at Subsonic and Transonic Speeds

Loads on Wings Due to Spoilers at Subsonic and Transonic Speeds PDF Author: Alexander D. Hammond
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 18

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Book Description

Loads on Thin Wings at Transonic Speeds

Loads on Thin Wings at Transonic Speeds PDF Author: Don D. Davis (Jr.)
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 22

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Book Description

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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Book Description
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.