The Influence of a Nonzero Angle of Attack and Gust Loads on the Nonlinear Response of a Typical Airfoil Section with a Control Surface Freeplay (Q4503835)
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scientific article; zbMATH DE number 1507068
| Language | Label | Description | Also known as |
|---|---|---|---|
| English | The Influence of a Nonzero Angle of Attack and Gust Loads on the Nonlinear Response of a Typical Airfoil Section with a Control Surface Freeplay |
scientific article; zbMATH DE number 1507068 |
Statements
The Influence of a Nonzero Angle of Attack and Gust Loads on the Nonlinear Response of a Typical Airfoil Section with a Control Surface Freeplay (English)
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21 November 2000
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control surface freeplay
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aeroelastic wing
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nonlinear dynamics
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angle of attack
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harmonic gust excitation
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Theodorsen aerodynamics
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Jones' approximation
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structural damping
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gust generator
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Wagner function
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Duhamel's superposition integral
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Schwarz's solution
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pressure distribution
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NACA 0012 rectangular wing model
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low speed wind tunnel
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quenching effect
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three-degree-of-freedom airfoil section
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