Pages that link to "Item:Q645329"
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The following pages link to A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel (Q645329):
Displaying 11 items.
- Parametric study on supersonic flutter of angle-ply laminated plates using shear deformable finite element method (Q362962) (← links)
- Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow (Q479623) (← links)
- A parametric study on supersonic/hypersonic flutter behavior of aero-thermo-elastic geometrically imperfect curved skin panel (Q645329) (← links)
- Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow (Q2092914) (← links)
- Aeroelastic characteristics of inflatable reentry vehicle in transonic and supersonic regions (Q2129513) (← links)
- Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model (Q2234966) (← links)
- Aerothermoelastic analysis of panel flutter based on the absolute nodal coordinate formulation (Q2340351) (← links)
- Effect of geometric and fluid flow nonlinearities on cylindrical shells subjected to a supersonic flow (Q2858955) (← links)
- Methods of continuation and their implementation in the COCO software platform with application to delay differential equations (Q6117149) (← links)
- Numerical investigation of aerothermoelastic characteristics of a thin heated panel in high supersonic and hypersonic flow (Q6157757) (← 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)
