Pages that link to "Item:Q2517521"
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The following pages link to Aeroelastic analysis and active flutter control of nonlinear lattice sandwich beams (Q2517521):
Displaying 9 items.
- Aerothermoelastic analysis of lattice sandwich composite panels in supersonic airflow (Q296080) (← links)
- Elimination of the flutter phenomenon in a forced and self-excited nonlinear beam using an improved saturation controller algorithm (Q2066875) (← links)
- A new method for suppressing nonlinear flutter and thermal buckling of composite lattice sandwich beams (Q2115390) (← links)
- An efficient solver for fully coupled solution of interaction between incompressible fluid flow and nanocomposite truncated conical shells (Q2173596) (← links)
- Nonlinear primary resonances of lattice sandwich beams with pyramidal truss core and viscoelastic surfaces (Q2296339) (← links)
- Nonlinear flutter and limit-cycle oscillations of damaged highly flexible composite wings (Q2296959) (← links)
- Computationally efficient model for flow-induced instability of CNT reinforced functionally graded truncated conical curved panels subjected to axial compression (Q2309800) (← links)
- Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow (Q2414632) (← links)
- Aerothermoelastic analysis of GPL-reinforced composite lattice sandwich beams based on a refined equivalent model (Q6044001) (← links)