Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models PDF Download

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Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models

Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models PDF Author: William M. Bland
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models

Effect of Wing Flexibility on the Damping in Roll of a Notched Delta Wing Body Combination Between Mach Numbers 0.6 and Approximately 2.2 as Determined with Rocket-propelled Models PDF Author: William M. Bland
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Book Description

Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
Publisher:
ISBN:
Category : Aeronautics
Languages : en
Pages : 580

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A Selected Listing of NASA Scientific and Technical Reports for ...

A Selected Listing of NASA Scientific and Technical Reports for ... PDF Author:
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ISBN:
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Damping in Roll of Models with 45©, 60©, and 70© Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket -powered Models

Damping in Roll of Models with 45©, 60©, and 70© Delta Wings Determined at High Subsonic, Transonic, and Supersonic Speeds with Rocket -powered Models PDF Author: E. Claude Sanders
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ISBN:
Category : Airplanes
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Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model PDF Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Vibration
Languages : en
Pages : 58

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Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket-propelled Vehicles

Effect of Fuselage Interference on the Damping in Roll of Delta Wings of Aspect Ratio 4 in the Mach Number Range Between 0.6 and 1.6 as Determined with Rocket-propelled Vehicles PDF Author: William M. Bland
Publisher:
ISBN:
Category :
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A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0

A Note on the Drag Due to Lift of Delta Wings at Mach Numbers Up to 2.0 PDF Author: Robert S. Osborne
Publisher:
ISBN:
Category : Aerodynamics
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Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60© Delta-wing Airplane Model

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60© Delta-wing Airplane Model PDF Author: Lewis R. Fisher
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 54

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Book Description