Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings PDF Download

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Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings

Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings PDF Author: William B. Kemp
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Book Description

Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings

Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35© Sweptback Wings PDF Author: William B. Kemp
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 32

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Book Description

Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35 Degree Sweptback Wings

Damping-in-pitch Characteristics at High Subsonic and Transonic Speeds of Four 35 Degree Sweptback Wings PDF Author: William B. Jr Kemp
Publisher:
ISBN:
Category :
Languages : en
Pages : 21

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Book Description

Effects of Sweep on the Damping-in-roll Characteristics of Three Sweptback Wings Having an Aspect Ratio of 4 at Transonic Speeds

Effects of Sweep on the Damping-in-roll Characteristics of Three Sweptback Wings Having an Aspect Ratio of 4 at Transonic Speeds PDF Author: Vernard E. Lockwood
Publisher:
ISBN:
Category : Aerodynamics, Transonic
Languages : en
Pages : 23

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Book Description
The damping-in-roll characteristics of three wings having an aspect ratio of 4, a taper ratio of 0.6, and NACA 65A006 airfoil section, and sweep angles of 0, 35, and 45 degrees have been determined through a Mach number range from 0.6 to 1.15 and an angle-of-attack range from 0 to approximately 7 degrees. The data were obtained from the Langley 7- by 10-foot tunnel transonic bump by utilizing the twisted-wing technique.

Damping in Pitch of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds

Damping in Pitch of Low-aspect-ratio Wings at Subsonic and Supersonic Speeds PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 116

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Book Description

High-subsonic Damping-in-roll Characteristics of a Wing with the Quarter-chord Line Swept Back 35 Degrees and with Aspect Ratio 3 and Taper Ratio 0.6

High-subsonic Damping-in-roll Characteristics of a Wing with the Quarter-chord Line Swept Back 35 Degrees and with Aspect Ratio 3 and Taper Ratio 0.6 PDF Author: Boyd C. II. Myers
Publisher:
ISBN:
Category :
Languages : en
Pages : 21

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Book Description

The Aerodynamic Damping and Oscillatory Stability in Pitch of Two High-drag Bodies of Revolution at Transonic Speeds

The Aerodynamic Damping and Oscillatory Stability in Pitch of Two High-drag Bodies of Revolution at Transonic Speeds PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 24

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Book Description

Subsonic Roll Damping of a Model with Swept-back and Swept-forward Wings

Subsonic Roll Damping of a Model with Swept-back and Swept-forward Wings PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 40

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Book Description

DESIGN GUIDE FOR PITCH-UP EVALUATION AND INVESTIGATION AT HIGH SUBSONIC SPEEDS OF POSSIBLE LIMITATIONS DUE TO WING-ASPECT-RATIO VARIATIONS

DESIGN GUIDE FOR PITCH-UP EVALUATION AND INVESTIGATION AT HIGH SUBSONIC SPEEDS OF POSSIBLE LIMITATIONS DUE TO WING-ASPECT-RATIO VARIATIONS PDF Author:
Publisher:
ISBN:
Category :
Languages : en
Pages : 44

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Book Description

Damping of Straight and 45 Degrees Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-powered Models

Damping of Straight and 45 Degrees Swept Wings of Various Taper Ratios Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-powered Models PDF Author: E. Claude Jr Sanders
Publisher:
ISBN:
Category :
Languages : en
Pages : 15

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Book Description

Damping in Roll of Models with 45 Degree, 60 Degree, and 70 Degree Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-powered Models

Damping in Roll of Models with 45 Degree, 60 Degree, and 70 Degree Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket-powered Models PDF Author: E. Claude Jr Sanders
Publisher:
ISBN:
Category :
Languages : en
Pages : 18

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Book Description