Effect of Camber and Twist on the Stability Characteristics of Models Having 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds PDF Download

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Effect of Camber and Twist on the Stability Characteristics of Models Having 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds

Effect of Camber and Twist on the Stability Characteristics of Models Having 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds PDF Author: Maurice D. White
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

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Book Description

Effect of Camber and Twist on the Stability Characteristics of Models Having 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds

Effect of Camber and Twist on the Stability Characteristics of Models Having 45 Degree Swept Wing as Determined by the Free-fall Method at Transonic Speeds PDF Author: Maurice D. White
Publisher:
ISBN:
Category :
Languages : en
Pages : 35

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Book Description

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 Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing

Effects of Twist and Camber on the Low-speed Characteristics of a Large-scale 45 Degree Swept-back Wing PDF Author: Lynn W. Hunton
Publisher:
ISBN:
Category :
Languages : en
Pages : 36

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Book Description

Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0

Longitudinal Stability Characteristics at Transonic Speeds of a Rocket-propelled Model of an Airplane Having a 45 Degree Swept Wing of Aspect Ratio 6.0 PDF Author: John C. McFall
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 44

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Book Description

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X (10)6 to 4.8 X (10)6 as Determined by Pressure Distributions, Force Tests, and Calculations

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X (10)6 to 4.8 X (10)6 as Determined by Pressure Distributions, Force Tests, and Calculations PDF Author: George L. Pratt
Publisher:
ISBN:
Category :
Languages : en
Pages : 104

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Book Description

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10(exp 6) to 4.8 X 10(exp 6) as Determined by Pressure Distributions, Force Tests

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 Degree Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10(exp 6) to 4.8 X 10(exp 6) as Determined by Pressure Distributions, Force Tests PDF Author: George L. Pratt
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description

Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds

Determination of Lateral Stability Characteristics from Free-flight Model Tests, with Experimental Results on the Effects of Wing Vertical Position and Dihedral at Transonic Speeds PDF Author: Clarence L. Gillis
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 44

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Book Description

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 O Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10 6 to 4.8 X 10 6 as Determined by Pressure Distributions, Force Tests, and Calculations

Effects of Twist and Camber on the Low-speed Longitudinal Stability Characteristics of a 45 O Sweptback Wing of Aspect Ratio 8 at Reynolds Numbers from 1.5 X 10 6 to 4.8 X 10 6 as Determined by Pressure Distributions, Force Tests, and Calculations PDF Author: George L. Pratt
Publisher:
ISBN:
Category :
Languages : en
Pages :

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Book Description

The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing

The Effects of Mass Distribution on the Low-speed Dynamic Lateral Stability and Control Characteristics of a Model with a 45° Sweptback Wing PDF Author: Donald E. Hewes
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 36

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Book Description
The trends in lateral stability and control produced variations of the mass distribution were determined for a model with a 45 degree sweptback wing. Calculations were made to correlate the trends determined by theory with those determined from tests of a free-flying dynamic model in the Langley free-flight tunnel.

Effect of Wing Camber and Twist at Mach Numbers from 1.4 to 2.1 on the Lift, Drag, and Longitudinal Stability of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces

Effect of Wing Camber and Twist at Mach Numbers from 1.4 to 2.1 on the Lift, Drag, and Longitudinal Stability of a Rocket-powered Model Having a 52.5 Degree Sweptback Wing of Aspect Ratio 3 and Inline Tail Surfaces PDF Author: Warren Gillespie
Publisher:
ISBN:
Category : Aerodynamics, Supersonic
Languages : en
Pages : 29

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Book Description
A free-flight investigation has been made to determine the effect of wing camber and twist at Mach numbers from 1.4 to 2.1 on the lift, drag, and longitudinal stability of a configuration having a 52.5 degree sweptback wing of aspect ratio 3, and inline tail surfaces. The wing was cambered and twisted to have low drag at a wing lift coefficient of 0.3 and at a Mach number of 1.46. The method reported in NACA Report 1226 was used to determine the wing warp. The model was aerodynamically pulsed in pitch throughout the flight of the model alone. Drag polars, normal force, pitching moment, static longitudinal stability, and wash effects at the horizontal tail were obtained. Comparisons are made with data from a similar model that had a flat (untwisted and uncambered) wing.