Pages that link to "Item:Q2927422"
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The following pages link to A fluid-structure coupling algorithm based on finite element method for precise analyses of transonic and supersonic panel flutter (Q2927422):
Displaying 6 items.
- Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow (Q479623) (← links)
- Panel flutter analysis of plate element based on the absolute nodal coordinate formulation (Q666580) (← links)
- A finite volume unstructured mesh approach to dynamic fluid--structure interaction: an assessment of the challenge of predicting the onset of flutter (Q1433329) (← links)
- Nonlinear panel flutter phenomena in transonic flow (Q2751244) (← links)
- Modeling of interaction of a supersonic stream and the deformable panel in a shock tube (Q2932507) (← links)
- Numerical study of fluid-structure interaction in supersonic regimes (Q3433422) (← links)