Author: Charles T. D'Aiutolo
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
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
Author: Charles T. D'Aiutolo
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
Book Description
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 36
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
Author: Charles T. D'Aiutolo
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 30
Book Description
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback
Author: Frederick C. Grant
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback
Author: Norman F. Smith
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 55
Book Description
A force investigation of a supersonic aircraft configuration and various combinations of its components has been conducted in the Langley 4- by 4-foot supersonic tunnel. The tests were performed at Mach numbers of 1.40 and 1.59 at a Reynolds number of approximately 600,000 based on the wing mean aerodynamic chord and are a part of an extensive investigation of the force and pressure-distribution characteristics of this configuration.
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 55
Book Description
A force investigation of a supersonic aircraft configuration and various combinations of its components has been conducted in the Langley 4- by 4-foot supersonic tunnel. The tests were performed at Mach numbers of 1.40 and 1.59 at a Reynolds number of approximately 600,000 based on the wing mean aerodynamic chord and are a part of an extensive investigation of the force and pressure-distribution characteristics of this configuration.
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
Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 28
Book Description
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Circular-arc Sections and 40 Degree Sweepback
Author: Clyde V. Hamilton
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28
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.
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 28
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 Degree Sweepback - Static Longitudinal and Lateral Stability and Control Characteristics at a Mach Number of 1.89
Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 24
Book Description
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
Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 22
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
Author: Norman F. Smith
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 48
Book Description
An Investigation of a Supersonic Aircraft Configuration Having a Tapered Wing with Curcular-arc Sections and 40 Degrees Sweepback
Author: M. Leroy Spearman
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description
Publisher:
ISBN:
Category :
Languages : en
Pages : 27
Book Description