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
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Category : Aerodynamic load
Languages : en
Pages : 60

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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 : 55

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An investigation has been conducted at the Langley 16-foot transonic tunnel to determine the loading characteristics of flap-down 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, with angles of attack up to about 27 degrees, and at aileron deflections between approximately plus or minus 15 degrees.

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NASA Technical Note PDF Author:
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Category :
Languages : en
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Technical Abstract Bulletin PDF Author: Defense Documentation Center (U.S.)
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Category : Technology
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Category :
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Category : Aeronautics
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Category : Government publications
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