Effects of Leading-edge Radius on the Longitudinal Stability Characteristics of Two 60 Degree Sweptback Wings at High Reynolds Numbers PDF Download

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Effects of Leading-edge Radius on the Longitudinal Stability Characteristics of Two 60 Degree Sweptback Wings at High Reynolds Numbers

Effects of Leading-edge Radius on the Longitudinal Stability Characteristics of Two 60 Degree Sweptback Wings at High Reynolds Numbers PDF Author: William C. Schneider
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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Effects of Leading-edge Radius on the Longitudinal Stability Characteristics of Two 60 Degree Sweptback Wings at High Reynolds Numbers

Effects of Leading-edge Radius on the Longitudinal Stability Characteristics of Two 60 Degree Sweptback Wings at High Reynolds Numbers PDF Author: William C. Schneider
Publisher:
ISBN:
Category :
Languages : en
Pages : 46

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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

Effects of Leading-edge Radius on the Longitudinal Stability of Two 45 Degree Sweptback Wings as Influenced by Reynolds Number Up to 8.20 X (10)6 and Mach Numbers Up to 0.303

Effects of Leading-edge Radius on the Longitudinal Stability of Two 45 Degree Sweptback Wings as Influenced by Reynolds Number Up to 8.20 X (10)6 and Mach Numbers Up to 0.303 PDF Author: Gerald V. Foster
Publisher:
ISBN:
Category :
Languages : en
Pages : 65

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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

Aeronautical Engineering Review

Aeronautical Engineering Review PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 844

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Book Description

Aero/space Engineering

Aero/space Engineering PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 1508

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Book Description

Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds

Effects of wing leading-edge radius and Reynolds number on longitudinal aerodynamic characteristics of highly swept wing-body configurations at subsonic speeds PDF Author: William P. Henderson
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 60

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Book Description

Effects of Leading-edge Devices and Trailing-edge Flaps on Longitudinal Characteristics of Two 47.7 Degrees Sweptback Wings of Aspect Ratios 5.1 and 6.0 at a Reynolds Number of 6.0 X (10)6

Effects of Leading-edge Devices and Trailing-edge Flaps on Longitudinal Characteristics of Two 47.7 Degrees Sweptback Wings of Aspect Ratios 5.1 and 6.0 at a Reynolds Number of 6.0 X (10)6 PDF Author: Reino J. Salmi
Publisher:
ISBN:
Category :
Languages : en
Pages : 105

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Effects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4

Effects of Wing-tip Droop on the Longitudinal Characteristics of Two Highly Swept Wing-body Combinations at Mach Numbers from 0.6 to 1.4 PDF Author: Earl D. Knechtel
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Book Description
An investigation was conducted to determine the effects of wing-tip droop on the longitudinal stability characteristics of a 53 and a 63 degree sweptback wing-body combination. Both models were tested with flat and abruptly drooped wing tips. The 63 degree wing was also tested with a curved drooped tip. In addition, the combined effects of wing fences and extended leading-edge flaps were investigated. The results showed that abrupt droop of the outer 40 percent of the basic 53 degree wing improved the stability characteristics of the model. For the 63 degree swept wing, curved droop caused slight beneficial effects on the stability, whereas abrupt droop caused adverse effects. In general, the most favorable stability characteristics were obtained for either flat or abruptly drooped wings with fences and extended leading-edge flaps.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports PDF Author:
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 224

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Book Description