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 Download

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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

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

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

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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Research Abstracts

Research Abstracts PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 568

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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

Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds

Investigation of a 42.7 Degree Sweptback Wing Model to Determine the Effects of Trailing-edge Thickness on the Aileron Hinge-moment and Flutter Characteristics at Transonic Speeds PDF Author: Robert F. Thompson
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 42

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Book Description
An investigation was made in the Langley high-speed 7- by 10-foot tunnel of 42.7 degrees sweptback wing model to determine the effects of aileron trailing-edge thickness on aileron hinge moments and one-degree-of-freedom aileron flutter. The wing had an aspect ratio of 4.0, a taper ratio of 0.5, and was tested over a Mach number range of 0.60 to 1.175. The half-span, 20-percent-chord ailerons were flat sided and located outboard.

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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Book Description
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.

Research Abstracts and Reclassification Notice

Research Abstracts and Reclassification Notice PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category :
Languages : en
Pages : 596

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Book Description

Effectiveness at Transonic Speeds of Flap-type Ailerons for Several Spanwise Locations on a 4-percent Thick Swept-back-wing-fuselage Model with and Without Tails

Effectiveness at Transonic Speeds of Flap-type Ailerons for Several Spanwise Locations on a 4-percent Thick Swept-back-wing-fuselage Model with and Without Tails PDF Author: Gerald Hieser
Publisher:
ISBN:
Category : Ailerons
Languages : en
Pages : 34

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Book Description
A transonic investigation has been made in the Langley 16-foot transonic tunnel to determine the effects of spanwise location of a flap-type aileron on the lateral characteristics of a 4-percent-thick sweptback wing-fuselage model. Some effects of the model tail on the lateral characteristics are also included. The inboard, midspan, and outboard ailerons have a span of 40 percent of the wing semispan and a chord of 30 percent of the wing chord. The tests covered Mach numbers from 0.80 to 1.03 and angles of attack up to 27 degrees.

Aerodynamic Characteristics at Subsonic and Transonic Speeds of a 42.7 Degrees Sweptback Wing Model Having an Aileron with Finite Trailing-edge Thickness

Aerodynamic Characteristics at Subsonic and Transonic Speeds of a 42.7 Degrees Sweptback Wing Model Having an Aileron with Finite Trailing-edge Thickness PDF Author: Thomas R. Turner
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description