Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane PDF Download

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Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 150

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Book Description

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X-15 Research Airplane PDF Author: Jim A. Penland
Publisher:
ISBN:
Category : Aerodynamic measurements
Languages : en
Pages : 150

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Book Description

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X- 15 Research Airplane

Static Longitudinal, Directional, and Lateral Stability and Control Data at a Mach Number of 6.83 of the Final Configuration of the X- 15 Research Airplane PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 78

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Book Description

Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configuration

Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configuration PDF Author: David E. Fetterman
Publisher:
ISBN:
Category :
Languages : en
Pages : 87

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Book Description

Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configurations

Static Longitudinal, Directional, and Lateral Stability and Control Data from an Investigation at a Mach Number of 6.83 of Two Developmental X-15 Airplane Configurations PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 92

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Book Description

Stability and Control Characteristics of a 0.0667-scale Model of the Final Version of the North American X-15 Research Airplane (configuration 3) at Transonic Speeds

Stability and Control Characteristics of a 0.0667-scale Model of the Final Version of the North American X-15 Research Airplane (configuration 3) at Transonic Speeds PDF Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 112

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Book Description

Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Static Longitudinal and Lateral Stability and Control Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form PDF Author: David E. Jr Fetterman
Publisher:
ISBN:
Category :
Languages : en
Pages : 103

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Book Description

Stability and Control Derivative Characteristics of the X-15 Airplane

Stability and Control Derivative Characteristics of the X-15 Airplane PDF Author: Harold J. Walker
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Book Description

Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration

Static Lateral Characteristics at High Subsonic Speeds of a Complete Airplane Model with a Highly Tapered Wing Having the 0.80 Chord Line Unswept and with Several Tail Configuration PDF Author: Kenneth W. Goodson
Publisher:
ISBN:
Category : Stability of airplanes, Lateral
Languages : en
Pages : 102

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Book Description
An investigation was made at high subsonic speeds of a complete model having a highly tapered wing and several tail configurations. The aspect-ratio-3.50 wing had a taper of 0.067 and an unswept 0.80 chord line. The complete model was tested with a wing-chord-plane tail, a T-tail, and a biplane tail (combined T-tail and wing-chord-plane tail). The model was tested in the Langley high-speed 7- by 10-foot tunnel at Mach numbers from 0.60 to 0.92 over a range of angle of attack of about ±20° and a range of sideslip of -15° to 13°. Some data were obtained with the horizontal stabilizer deflected. A few tests were also made with the wing tips clipped to an aspect ratio of 3.00.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 996

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Book Description
Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3.11 of Square and Circular Plan-form Reentry Vehicles, with Some Effects of Controls and Leading-edge Extensions

Static Longitudinal and Lateral Stability Characteristics at a Mach Number of 3.11 of Square and Circular Plan-form Reentry Vehicles, with Some Effects of Controls and Leading-edge Extensions PDF Author: Byron M. Jaquet
Publisher:
ISBN:
Category : Leading edges (Aerodynamics)
Languages : en
Pages : 26

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Book Description