The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96 PDF Download

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The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96

The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96 PDF Author: Robert I. Sammonds
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 64

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Book Description
An investigation has been conducted to determine the effect of conical camber on the drag due to lift and on the static longitudinal, lateral, and directional stability characteristics of an aspect-ratio-3, 45 degree sweptback wing in combination with a streamline body. Tests were made at Mach numbers up to 0.96 at a Reynolds number of 1.5 million and at a Reynolds number up to 8 million at a Mach number of 0.22, both with and without roughness strips near the leading edge of both the upper and lower surfaces of the wing.

The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96

The Effect of Conical Camber on the Static Longitudinal, Lateral, and Directional Characteristics of a 45-degree Sweptback Wing at Mach Numbers Up to 0.96 PDF Author: Robert I. Sammonds
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 64

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Book Description
An investigation has been conducted to determine the effect of conical camber on the drag due to lift and on the static longitudinal, lateral, and directional stability characteristics of an aspect-ratio-3, 45 degree sweptback wing in combination with a streamline body. Tests were made at Mach numbers up to 0.96 at a Reynolds number of 1.5 million and at a Reynolds number up to 8 million at a Mach number of 0.22, both with and without roughness strips near the leading edge of both the upper and lower surfaces of the wing.

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45© Swept-back Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 106 to 4.8 X 10 as Determined by Pressure Distributions, Force Tests, and Calculations PDF Author: George L. Pratt
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 110

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Book Description

Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5

Effects of Deflected Wing Tips on the Aerodynamic Characteristics of a Canard Configuration at Mach Numbers from 0.7 to 3.5 PDF Author: Victor L. Peterson
Publisher:
ISBN:
Category : Aerodynamics
Languages : en
Pages : 180

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Book Description

The Static Longitudinal Characteristics of a Twisted and Cambered 45 O Sweptback Wing at Mach Numbers Up to 0.96

The Static Longitudinal Characteristics of a Twisted and Cambered 45 O Sweptback Wing at Mach Numbers Up to 0.96 PDF Author: Robert I. Sammonds
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75°

Stability and Control Characteristics at Mach Numbers of 2.50, 3.00, and 3.71 of a Variable- Wing-sweep Configuration with Outboard Wing Panels Swept Back 75° PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 38

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Book Description

The Static Longitudinal Characteristics of a Twisted and Cambered 45 Degree Sweptback Wing at Mach Numbers Up to 0.96

The Static Longitudinal Characteristics of a Twisted and Cambered 45 Degree Sweptback Wing at Mach Numbers Up to 0.96 PDF Author: Robert I. Sammonds
Publisher:
ISBN:
Category :
Languages : en
Pages : 26

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Book Description

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces

Effect of Horizontal-tail Location on Low-speed Static Longitudinal Stability and Damping in Pitch of a Model Having 45° Sweptback Wing and Tail Surfaces PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 34

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Book Description
Wind-tunnel results are presented to show the effect of changes in horizontal-tail location on the low-speed static longitudinal stability and steady-state rotary damping in pitch for a complete model with wing and tail surfaces having the quarter-chord lines swept back 45 degrees.

Effects of Wing Elevation, Incidence, and Camber on the Aerodynamic Characteristics of a Representative Hypersonic Cruise Configuration at Mach Numbers from 0.65 to 10.70

Effects of Wing Elevation, Incidence, and Camber on the Aerodynamic Characteristics of a Representative Hypersonic Cruise Configuration at Mach Numbers from 0.65 to 10.70 PDF Author: Walter P. Nelms
Publisher:
ISBN:
Category : Aerodynamics, Hypersonic
Languages : en
Pages : 82

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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

Effects of Leading-edge Radius on the Longitudinal Stability of Two 45 Degrees Sweptback Wings Incorporating Leading-edge Camber as Influenced by Reynolds Numbers Up to 8.00 X 10 6 and Mach Numbers Up to 0.290

Effects of Leading-edge Radius on the Longitudinal Stability of Two 45 Degrees Sweptback Wings Incorporating Leading-edge Camber as Influenced by Reynolds Numbers Up to 8.00 X 10 6 and Mach Numbers Up to 0.290 PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Book Description