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 Download

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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

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

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° 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 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 : 0

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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

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

Technical Abstract Bulletin

Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
Publisher:
ISBN:
Category : Technology
Languages : en
Pages : 1116

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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 :
Languages : en
Pages : 1

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Book Description
An investigation was conducted at the Langley 16-foot transonic tunnel to determine the loading characteristics of flap-type ailerons located at inboard, midspan, and outboard positions on a 45 degree sweptback-wing-body combination. Aileron normal-force and hinge-moment data have been obtained at Mach numbers from 0.80 to 1.03, at angles of attack up to about 27 degrees, and at aileron deflections between approximately -15 degrees and 15 degrees. Results of the investigation indicate that the loading over the ailerons was established by the wing-flow characteristics, and the loading shapes were irregular in the transonic speed range. The spanwise location of the aileron had little effect on the values of the slope of the curves of hinge-moment coefficient against aileron deflection, but the inboard aileron had the greatest value of the slope of curves of hinge-moment coefficient against angle of attack and the outboard aileron had the least. Hinge-moment and aileron normal-force data taken with strain-gage instrumentation are compared with data obtained with pressure measurements. (Author).

Transonic Characteristics of Outboard Ailerons on a 4-percent-thick 30 Degree Sweptback Wing, Including Some Effects of Aileron Trailing-edge Thickness and Aerodynamic Balance

Transonic Characteristics of Outboard Ailerons on a 4-percent-thick 30 Degree Sweptback Wing, Including Some Effects of Aileron Trailing-edge Thickness and Aerodynamic Balance PDF Author: Charles F. Whitcomb
Publisher:
ISBN:
Category :
Languages : en
Pages : 70

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Book Description