Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model

Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model PDF Author: William T. Lauten
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 21

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An analysis of the flight time history of a rocket-propelled model of a 60 degrees delta-wing airplane configuration, fired for the purpose of obtaining zero-lift drag data, indicated wing flutter and subsequent failure at low-supersonic Mach numbers. This flutter occurred during the unpowered decelerating portion of the flight. The behavior of the model during flight is discussed and the mass and stiffness characteristics of a duplicate wing are presented.

Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model

Note on Flutter of a 60 Degree Delta Wing Encountered at Low-supersonic Speeds During the Flight of a Rocket-propelled Model PDF Author: William T. Lauten
Publisher:
ISBN:
Category : Aerofoils
Languages : en
Pages : 21

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Book Description
An analysis of the flight time history of a rocket-propelled model of a 60 degrees delta-wing airplane configuration, fired for the purpose of obtaining zero-lift drag data, indicated wing flutter and subsequent failure at low-supersonic Mach numbers. This flutter occurred during the unpowered decelerating portion of the flight. The behavior of the model during flight is discussed and the mass and stiffness characteristics of a duplicate wing are presented.

Supersonic Flutter of a 60© Delta Wing Encountered During the Flight Test of a Rocket-propelled Model

Supersonic Flutter of a 60© Delta Wing Encountered During the Flight Test of a Rocket-propelled Model PDF Author: William T. Lauten
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 26

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An analysis of the flight time-history records of a record-propelled 60 degree delta-wing airplane configuration indicate that wing flutter started during the accelerating portion of the flight at a Mach number of approximately 1.7 and continued through the peak Mach number of the test (M = 2.08) and during deceleration at least until telemeter failure at M = 1.4 and probably to an even lower speed. CW Doppler velocimeter data indicated that the wings did not fail during the flight.

Flutter of a 60© Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model

Flutter of a 60© Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model PDF Author: Joseph H. Judd
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 30

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Supersonic Flutter of a 60 Degree Delta Wing Encountered During the Flight Test of a Rocket-propelled Model

Supersonic Flutter of a 60 Degree Delta Wing Encountered During the Flight Test of a Rocket-propelled Model PDF Author: William T. Jr Lauten
Publisher:
ISBN:
Category :
Languages : en
Pages : 20

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Flutter of a 60 Degree Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model

Flutter of a 60 Degree Delta Wing (NACA 65A003 Airfoil) Encountered at Supersonic Speeds During the Flight Test of a Rocket-propelled Model PDF Author: Joseph H. Judd
Publisher:
ISBN:
Category :
Languages : en
Pages : 14

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Index of NACA Technical Publications

Index of NACA Technical Publications PDF Author: United States. National Advisory Committee for Aeronautics
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ISBN:
Category : Aeronautics
Languages : en
Pages : 1338

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Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data

Investigation of Methods for Computing Flutter Characteristics of Supersonic Delta Wings and Comparison with Experimental Data PDF Author: Charles Harold Wilts
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ISBN:
Category : Aeroelasticity
Languages : en
Pages : 74

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Some Low-speed Flutter Characteristics of Simple Low-aspect-ratio Delta Wing Models

Some Low-speed Flutter Characteristics of Simple Low-aspect-ratio Delta Wing Models PDF Author: Robert V. Doggett (Jr)
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ISBN:
Category :
Languages : en
Pages : 11

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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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A Preliminary Wind-tunnel Investigation of Flutter Characteristics of Delta Wings

A Preliminary Wind-tunnel Investigation of Flutter Characteristics of Delta Wings PDF Author: Robert W. Herr
Publisher:
ISBN:
Category : Airplanes
Languages : en
Pages : 40

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