Pages that link to "Item:Q479623"

The following pages link to Aeroelastic flutter analysis for 2D Kirchhoff and Mindlin panels with different boundary conditions in supersonic airflow (Q479623):

Displaying 16 items.

• Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow (Q296080) (← links)
• Dynamics and stability of an axially moving plate interacting with surrounding airflow (Q333655) (← links)
• Panel flutter analysis of plate element based on the absolute nodal coordinate formulation (Q666580) (← links)
• Nonlinear aero-thermal flutter postponement of supersonic laminated composite beams with shape memory alloys (Q1658026) (← links)
• Flutter instability of laminated thick anisotropic plates using BEM (Q1743569) (← links)
• An energy flow model for high-frequency vibration analysis of two-dimensional panels in supersonic airflow (Q1985224) (← links)
• Aerothermoelastic analysis of curvilinear fiber variable stiffness laminated panels in supersonic flow (Q2092914) (← links)
• An efficient solver for fully coupled solution of interaction between incompressible fluid flow and nanocomposite truncated conical shells (Q2173596) (← links)
• Aeroelastic analysis of rectangular plates coupled to sloshing fluid (Q2194386) (← links)
• Aeroelastic stability analysis of a flexible panel subjected to an oblique shock based on an analytical model (Q2234966) (← links)
• Computationally efficient model for flow-induced instability of CNT reinforced functionally graded truncated conical curved panels subjected to axial compression (Q2309800) (← links)
• A fluid-structure coupling algorithm based on finite element method for precise analyses of transonic and supersonic panel flutter (Q2927422) (← links)
• Wave propagation in one-dimensional multi-bay periodically supported panels under supersonic fluid flow (Q4520000) (← links)
• Supersonic flutter analysis of wings using an unsteady 3D panel method (Q5929811) (← links)
• Vibration and dynamic instability analyses of functionally graded porous doubly curved panels with piezoelectric layers in supersonic airflow (Q6184193) (← links)
• Supersonic aeroelasticity and dynamic instability of functionally graded porous cylindrical shells using a unified solution formulation (Q6491607) (← links)