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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Bibliographische Detailangaben
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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