Pages that link to "Item:Q2310026"
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The following pages link to Modeling aerothermoelastic properties and active flutter control of nanocomposite cylindrical shells in supersonic airflow under thermal environments (Q2310026):
Displaying 7 items.
- Nonlinear aero-thermal flutter postponement of supersonic laminated composite beams with shape memory alloys (Q1658026) (← links)
- Aeroelastic characteristics of functionally graded carbon nanotube-reinforced composite plates under a supersonic flow (Q1798593) (← links)
- A unified adaptive approach for membrane structures: form finding and large deflection isogeometric analysis (Q2236180) (← links)
- Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow (Q2414632) (← links)
- Adaptive fault-tolerant flutter control based on dynamic output feedback (Q2680287) (← links)
- Solving post-buckling characteristic of thermal-resistance films attached to Glass façade via an optimization method (Q6493272) (← links)
- Dynamic instability of functionally graded carbon nanotubes-reinforced composite joined conical-cylindrical shell (Q6499537) (← links)