Pages that link to "Item:Q362962"
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The following pages link to Parametric study on supersonic flutter of angle-ply laminated plates using shear deformable finite element method (Q362962):
Displaying 3 items.
- Flutter instability of laminated thick anisotropic plates using BEM (Q1743569) (← links)
- Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow (Q2092914) (← links)
- Analysis of the dynamic behavior, buckling, and aeroelasticity of a thin composite plate with the effect of general and local geometric defects (Q6665029) (← links)