The Effects of High-lift Devices on the Low-speed Stability Characteristics of a Tapered 37.5 Degrees Sweptback Wing of Aspect Ratio 3 in Straight and Rolling Flow PDF Download

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The Effects of High-lift Devices on the Low-speed Stability Characteristics of a Tapered 37.5 Degrees Sweptback Wing of Aspect Ratio 3 in Straight and Rolling Flow

The Effects of High-lift Devices on the Low-speed Stability Characteristics of a Tapered 37.5 Degrees Sweptback Wing of Aspect Ratio 3 in Straight and Rolling Flow PDF Author: M.J. Queijo
Publisher:
ISBN:
Category :
Languages : en
Pages : 27

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The Effects of High-lift Devices on the Low-speed Stability Characteristics of a Tapered 37.5 Degrees Sweptback Wing of Aspect Ratio 3 in Straight and Rolling Flow

The Effects of High-lift Devices on the Low-speed Stability Characteristics of a Tapered 37.5 Degrees Sweptback Wing of Aspect Ratio 3 in Straight and Rolling Flow PDF Author: M.J. Queijo
Publisher:
ISBN:
Category :
Languages : en
Pages : 27

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Book Description

Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds

Aerodynamic Load Measurements and Opening Characteristics of Automatic Leading-edge Slats on a 45 Degree Sweptback Wing at Transonic Speeds PDF Author: Donald D. Arabian
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 54

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Effect of High-lift Devices on the Low-speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Degree Sweptback Wing

Effect of High-lift Devices on the Low-speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Degree Sweptback Wing PDF Author: Jacob H. Lichenstein
Publisher:
ISBN:
Category :
Languages : en
Pages : 21

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Effect of High-lift Devices on the Low Speed Characteristics of a Sweptback Wing

Effect of High-lift Devices on the Low Speed Characteristics of a Sweptback Wing PDF Author: Donald Dwight Seath
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 104

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Effect of High-lift Devices on the Low-speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 [degrees] Sweptback Wing

Effect of High-lift Devices on the Low-speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 [degrees] Sweptback Wing PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence

An Analysis of the Effects of Wing Aspect Ratio and Tail Location on Static Longitudinal Stability Below the Mach Number of Lift Divergence PDF Author: John A. Axelson
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 20

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Book Description
An analysis is presented of the influence of wing aspect ratio and tail location on the effects of compressibility upon static longitudinal stability. The investigation showed that the use of reduced wing aspect ratios or short tail lengths leads to serious reductions in high-speed stability and the possibility of high-speed instability.

Effect of High-lift Devices on the Static-lateral-stability Derivatives of a 45 [degrees] Sweptback Wing of Aspect Ratio 4.0 and Taper Ratio 0.6 in Combination with a Body

Effect of High-lift Devices on the Static-lateral-stability Derivatives of a 45 [degrees] Sweptback Wing of Aspect Ratio 4.0 and Taper Ratio 0.6 in Combination with a Body PDF Author: Jacob H. Lichtenstein
Publisher:
ISBN:
Category :
Languages : en
Pages : 50

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Book Description

Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio

Lift, Pitching Moment, and Span Load Characteristics of Wings at Low Speed as Affected by Variations of Sweep and Aspect Ratio PDF Author: Edward J. Hopkins
Publisher:
ISBN:
Category : Aerodynamic load
Languages : en
Pages : 40

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Book Description
Lift, pitching-moment, and pressure distribution were measured on a wing which was swept -40, -30, 0, 35, and 45 degrees. The wing span was decreased to give aspect ratios 6.8, 5.3, 4.2, 3.4, and 2.8. The effects of independent variations of sweep and aspect ratio on the lift, pitching-moment, and span-load characteristics of the wings are compared with the effects estimated by use of the Weissinger method.

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

Effect of High-Lift Devices on the Low-Speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Deg Sweptback Wing

Effect of High-Lift Devices on the Low-Speed Static Lateral and Yawing Stability Characteristics of an Untapered 45 Deg Sweptback Wing PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 0

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Book Description