Pages that link to "Item:Q666580"
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The following pages link to Panel flutter analysis of plate element based on the absolute nodal coordinate formulation (Q666580):
Displaying 4 items.
- Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow (Q479623) (← links)
- Aerothermoelastic analysis of panel flutter based on the absolute nodal coordinate formulation (Q2340351) (← links)
- A thick anisotropic plate element in the framework of an absolute nodal coordinate formulation (Q2435618) (← links)
- A novel plate element based on absolute nodal coordinate formulation with collocation strategy (Q6143780) (← links)