Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback PDF Download

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Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback

Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback PDF Author: Charles T. D'Aiutolo
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36

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Book Description

Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback

Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40© Sweepback PDF Author: Charles T. D'Aiutolo
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36

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Book Description

Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback

Preliminary Results of the Flight Investigation Between Mach Numbers of 0.80 and 1.36 of a Rocket-powered Model of a Supersonic Airplane Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback PDF Author: Charles T. D'Aiutolo
Publisher:
ISBN:
Category :
Languages : en
Pages : 30

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An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback PDF Author: Frederick C. Grant
Publisher:
ISBN:
Category :
Languages : en
Pages : 27

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Book Description

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback - Static Lateral Stability Characteristics at Mach Numbers of 1.40 and 1.59

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback - Static Lateral Stability Characteristics at Mach Numbers of 1.40 and 1.59 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 28

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Book Description

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback PDF Author: Clyde V. Hamilton
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28

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Book Description
An investigation has been conducted in the Langley 4- by 4-foot supersonic pressure tunnel at a Mach number of 1.61 to determine the stability of control characteristics of a supersonic aircraft configuration with a 40 percent sweptback wing and equipped with spoiler lateral control devices. Some effects of various types of spoilers, spoiler span, projection, and chordwise location were investigated, as well as the hinge-moment characteristics for a plain spoiler.

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback - Static Longitudinal Stability and Control Characteristics at a Mach Number of 1.59

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degrees Sweepback - Static Longitudinal Stability and Control Characteristics at a Mach Number of 1.59 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 22

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Book Description

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback - Static Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.89

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback - Static Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.89 PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Section and 40 Degrees Sweepback - a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.40

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Section and 40 Degrees Sweepback - a Pressure-distribution Study of the Aerodynamic Characteristics of the Wing at Mach Number 1.40 PDF Author: Norman F. Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 48

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Book Description

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Curcular-arc Sections and 40 Degrees Sweepback

An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Curcular-arc Sections and 40 Degrees Sweepback PDF Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 27

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Book Description

Sonic-boom Characteristics in the Extreme Near Field of a Complex Airplane Model at Mach Numbers of 1.5, 1.8, and 2.5

Sonic-boom Characteristics in the Extreme Near Field of a Complex Airplane Model at Mach Numbers of 1.5, 1.8, and 2.5 PDF Author: Odell A. Morris
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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Book Description