Behavior of Airfoil with Control Surface Freeplay for Nonzero Angles of Attack

Behavior of Airfoil with Control Surface Freeplay for Nonzero Angles of Attack

Kholodar and Dowell use a numerical approach to analyze the nonlinear behavior of an aeroelastic wing system with a trailing-edge flap.

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Veröffentlicht in:AIAA journal 1999-05, Vol.37 (5), p.651-653
Hauptverfasser: Kholodar, Denis B, Dowell, Earl H
Format: Artikel
Sprache:eng
Schlagworte:
Aerodynamics
Approximation theory
Degrees of freedom (mechanics)
Equations of motion
Exact sciences and technology
Fundamental areas of phenomenology (including applications)
Integration
Mathematical models
Mechanics
Motion control
Oscillations
Physics
Runge Kutta methods
Solid mechanics
State space methods
Structural and continuum mechanics
Vibration, mechanical wave, dynamic stability (aeroelasticity, vibration control...)
Vibrations and mechanical waves
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Beschreibung
Zusammenfassung:Kholodar and Dowell use a numerical approach to analyze the nonlinear behavior of an aeroelastic wing system with a trailing-edge flap.
ISSN:0001-1452
1533-385X
DOI:10.2514/2.766