Pages that link to "Item:Q396306"
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The following pages link to On the aeroelastic stability and bifurcation structure of subsonic nonlinear thin panels subjected to external excitation (Q396306):
Displaying 14 items.
- On double stable limit cycle flutter of a plate with motion constraints in subsonic flow (Q293592) (← links)
- Melnikov's method for chaos of a two-dimensional thin panel in subsonic flow with external excitation (Q366788) (← links)
- Nonlinear dynamics analysis of a two-dimensional thin panel with an external forcing in incompressible subsonic flow (Q437427) (← links)
- Stability analysis and active control of a nonlinear composite laminated plate with piezoelectric material in subsonic airflow (Q521210) (← links)
- Bifurcations and subharmonic resonances in multi-degree-of-freedom panel models (Q676946) (← links)
- Coherent structures and their influence on the dynamics of aeroelastic panels (Q873362) (← links)
- Chaotic analysis of nonlinear viscoelastic panel flutter in supersonic flow (Q1418910) (← links)
- The instability of a plate fixed at both ends in an axial flow revisited: an application of the DQ-BE method (Q1989221) (← links)
- Aeroelastic instability of an inverted cantilevered plate with cracks in axial subsonic airflow (Q2109580) (← links)
- Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model (Q2234966) (← links)
- Nonlinear flutter behavior of a plate with motion constraints in subsonic flow (Q2258195) (← links)
- Asymptotic Analysis of Passive Nonlinear Suppression of Aeroelastic Instabilities of a Rigid Wing in Subsonic Flow (Q3053174) (← links)
- Bifurcation structure and scaling properties of a subsonic periodically driven panel with geometric nonlinearity (Q3195026) (← links)
- On the aeroelastic bifurcation of a flexible panel subjected to cavity pressure and inviscid oblique shock (Q6541835) (← links)