Pages that link to "Item:Q2414632"

The following pages link to Computation of aerothermoelastic properties and active flutter control of CNT reinforced functionally graded composite panels in supersonic airflow (Q2414632):

Displaying 21 items.

• On the nonlinear dynamic responses of FG-CNTRC beams exposed to aerothermal loads using third-order piston theory (Q725192) (← links)
• Elastodynamic analysis of regular polygonal CNT-reinforced composite plates via FSDT element-free method (Q1655277) (← links)
• Vibrational analysis of functionally graded carbon nanotube-reinforced composite spherical shells resting on elastic foundation using the variational differential quadrature method (Q1658277) (← links)
• Thermoelastic nonlinear frequency analysis of CNT reinforced functionally graded sandwich structure (Q1658705) (← links)
• In-plane and shear buckling analysis of FG-CNTRC annular sector plates based on the third-order shear deformation theory using a numerical approach (Q1732329) (← links)
• Aeroelastic characteristics of functionally graded carbon nanotube-reinforced composite plates under a supersonic flow (Q1798593) (← links)
• Meshless numerical approach to flutter analysis of rotating pre-twisted nanocomposite blades subjected to supersonic airflow (Q1980179) (← links)
• Compressive instability of open section nanocomposite struts using a layerwise theory (Q1988252) (← links)
• Free vibration of functionally graded carbon nanotube reinforced composite plates integrated with piezoelectric layers (Q2012713) (← links)
• Thermal buckling strength of smart nanotube-reinforced doubly curved hybrid composite panels (Q2019593) (← links)
• An efficient solver for fully coupled solution of interaction between incompressible fluid flow and nanocomposite truncated conical shells (Q2173596) (← links)
• Modeling of dynamic responses of CNT-reinforced composite cylindrical shells under impact loads (Q2308781) (← links)
• Computationally efficient model for flow-induced instability of CNT reinforced functionally graded truncated conical curved panels subjected to axial compression (Q2309800) (← links)
• Modeling aerothermoelastic properties and active flutter control of nanocomposite cylindrical shells in supersonic airflow under thermal environments (Q2310026) (← links)
• Postbuckling analysis of smart FG-CNTRC annular sector plates with surface-bonded piezoelectric layers using generalized differential quadrature method (Q2310038) (← links)
• On the snap-through instability of post-buckled FG-CNTRC rectangular plates with integrated piezoelectric layers (Q2310695) (← links)
• Vibration of functionally graded CNTs-reinforced skewed cylindrical panels using a transformed differential quadrature method (Q2400384) (← links)
• Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes (Q2421973) (← links)
• Modeling of hyperelastic polymer gels under blunt ballistic impact with three-dimensional flexibilities (Q6099232) (← links)
• Vibration and dynamic instability analyses of functionally graded porous doubly curved panels with piezoelectric layers in supersonic airflow (Q6184193) (← links)
• Dynamic instability of functionally graded carbon nanotubes-reinforced composite joined conical-cylindrical shell (Q6499537) (← links)