Damping In Roll Of Models With 45c 60c And 70c Delta Wings Determined At High Subsonic Transonic And Supersonic Speeds With Rocket Powered Models

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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
Language: en
Pages: 26

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

Authors: E. Claude Sanders
Categories: Airplanes
Type: BOOK - Published: 1952 - Publisher:

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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
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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

Authors: E. Claude Jr Sanders
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Type: BOOK - Published: 1952 - Publisher:

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A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Sting-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings
Language: en
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A Technique Utilizing Rocket-propelled Test Vehicles for the Measurement of the Damping in Roll of Sting-mounted Models and Some Initial Results for Delta and Unswept Tapered Wings

Authors: William M. Bland
Categories: Aerodynamics
Type: BOOK - Published: 1950 - Publisher:

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A free-flight test technique utilizing rocket-propelled test vehicles with which the damping in roll of sting-mounted wings and wing-fuselage combinations can b
Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model
Language: en
Pages: 58

Experimental Determination of the Effects of Frequency and Amplitude of Oscillation on the Roll-stability Derivatives for a 60 Degree Delta-wing Airplane Model

Authors: Lewis R. Fisher
Categories: Vibration
Type: BOOK - Published: 1960 - Publisher:

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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
Language: en
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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

Authors: William M. Bland
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