A nonlinear aeroelastic model for a rigid flat plate in 2D incompressible potential flow is presented as a special case of a more general formulation, based on time-dependent conformal mapping and discrete vortex shedding. The model captures large-amplitude motions and free-wake dynamics, enabling investigation of flutter onset and large oscillations. Numerical simulations highlight strong nonlinear behaviors and complex vortex patterns. An excess energy formulation is introduced to analyze fluid-structure energy exchange, offering insights into instability mechanisms beyond classical linear theories.

Analytical investigation of the energetic exchange involved in the aeroelastic behavior of a thickless plate in a 2D flow / Eugeni, M., Riccardi, G.. - (2025). (EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES Roma ).

Analytical investigation of the energetic exchange involved in the aeroelastic behavior of a thickless plate in a 2D flow

Marco Eugeni
Conceptualization
;
Giorgio Riccardi
Methodology
2025

Abstract

A nonlinear aeroelastic model for a rigid flat plate in 2D incompressible potential flow is presented as a special case of a more general formulation, based on time-dependent conformal mapping and discrete vortex shedding. The model captures large-amplitude motions and free-wake dynamics, enabling investigation of flutter onset and large oscillations. Numerical simulations highlight strong nonlinear behaviors and complex vortex patterns. An excess energy formulation is introduced to analyze fluid-structure energy exchange, offering insights into instability mechanisms beyond classical linear theories.
2025
EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES
Fluid-structure interaction, incompressible and planar flows, conformal mapping, analytical methods
04 Pubblicazione in atti di convegno::04b Atto di convegno in volume
Analytical investigation of the energetic exchange involved in the aeroelastic behavior of a thickless plate in a 2D flow / Eugeni, M., Riccardi, G.. - (2025). (EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES Roma ).
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11573/1777708
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