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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

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.

Investigation at Transonic Speeds of the Loading Over a 40 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 40 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 : Aerodynamics
Languages : en
Pages : 98

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Book Description

A Method for Calculating Aerodynamic Loadings on Thin Wings at a Mach Number of 1

A Method for Calculating Aerodynamic Loadings on Thin Wings at a Mach Number of 1 PDF Author: John L. Crigler
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 34

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Flight Tests at Transonic and Supersonic Speeds of an Airplane-like Configuration with a Thin Straight Sharp-edge Wings and Tail Surfaces

Flight Tests at Transonic and Supersonic Speeds of an Airplane-like Configuration with a Thin Straight Sharp-edge Wings and Tail Surfaces PDF Author: Clarence L. Gillis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Flight Measurements of Lifting Pressures for a Thin Low-aspect-ratio Wing at Subsonic, Transonic, and Low Supersonic Speeds

Flight Measurements of Lifting Pressures for a Thin Low-aspect-ratio Wing at Subsonic, Transonic, and Low Supersonic Speeds PDF Author: Thomas A. Byrdsong
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 128

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Book Description

A Study of the Aerodynamic Loads on Sweptback Wings at Transonic Speeds

A Study of the Aerodynamic Loads on Sweptback Wings at Transonic Speeds PDF Author: Claude V. Williams
Publisher:
ISBN:
Category :
Languages : en
Pages : 14

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Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds

Aerodynamic Properties of Cruciform-wing and Body Combinations at Subsonic, Transonic, and Supersonic Speeds PDF Author: John R. Spreiter
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 646

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Book Description
The aerodynamic forces and moments exerted on pitched and yawed wing-body combinations consisting of a slender body of revolution and a cruciform arrangement of thin wings have been investigated by two theoretical methods. One method, an extension of the slender wing-body theory of NACA TN No. 1662, makes possible the determination of simple closed expressions for the load distribution, of simple closed expressions for the load distribution, the forces, and the moments for slender cruciform-wing and body combinations in which the wings may be dissimilar plan form. The second method treats cruciform-wing and body combinations consisting of a body of revolution and identical wings of arbitrary aspect ratio and plan form. The results are valid at subsonic, transonic, and supersonic 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

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

Calculation of Aerodynamic Loading and Twist Characteristics of a Flexible Wing at Mach Numbers Approaching 1.0 and Comparison with Experiment

Calculation of Aerodynamic Loading and Twist Characteristics of a Flexible Wing at Mach Numbers Approaching 1.0 and Comparison with Experiment PDF Author: John P.. Mugler
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40

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Book Description