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 Download

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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 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

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 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

Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form

Static Longitudinal and Lateral Stability Data from an Exploratory Investigation at Mach Number 4.06 of an Airplane Configuration Having a Wing of Trapezoidal Plan Form PDF Author: Robert W. Dunning
Publisher:
ISBN:
Category :
Languages : en
Pages : 37

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Book Description

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

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.

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

Static Lateral Stability Data from an Exploratory Investigation at a Mach Number of 6.86 of an Airplane Configuration Having a Wing of Trapezoidal Plam Form PDF Author: Herbert W. Ridyard
Publisher:
ISBN:
Category :
Languages : en
Pages : 42

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Book Description

Low-speed Investigation of Static Longitudinal and Lateral Stability Characteristics of an Airplane Configuration with a Highly Tapered Wing and with Several Body and Tail Arrangements

Low-speed Investigation of Static Longitudinal and Lateral Stability Characteristics of an Airplane Configuration with a Highly Tapered Wing and with Several Body and Tail Arrangements PDF Author: Paul G. Fournier
Publisher:
ISBN:
Category : Stability of airplanes, Longitudinal
Languages : en
Pages : 54

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Book Description