Aeroelastic characteristics of functionally graded carbon nanotube-reinforced composite plates under a supersonic flow

DOI10.1016/j.cma.2014.11.042zbMath1423.76191OpenAlexW2039663689MaRDI QIDQ1798593

S. Pouresmaeeli, S. Ahmad Fazelzadeh, Esmaeal Ghavanloo

Publication date: 23 October 2018

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.cma.2014.11.042

zbMATH Keywords

supersonic flownanocompositeaeroelastic characteristicfunctionally graded carbon nanotube-reinforced composite

Mathematics Subject Classification ID

Fluid-solid interactions (including aero- and hydro-elasticity, porosity, etc.) (74F10) Composite and mixture properties (74E30) Supersonic flows (76J20)

Related Items (5)

A naturally stabilized nodal integration meshfree formulation for carbon nanotube-reinforced composite plate analysis ⋮ Aerothermoelastic flutter analysis of pre-twisted thin-walled rotating blades reinforced with functionally graded carbon nanotubes ⋮ Modeling geometrically nonlinear large deformation behaviors of matrix cracked hybrid composite deep shells containing CNTRC layers ⋮ Size-dependent analysis of FG-CNTRC microplates based on modified strain gradient elasticity theory ⋮ Dynamic stability of fluid-conveying thin-walled rotating pipes reinforced with functionally graded carbon nanotubes

Cites Work

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• Large deflection analysis of functionally graded carbon nanotube-reinforced composite plates by the element-free \(kp\)-Ritz method
• Postbuckling of carbon nanotube-reinforced functionally graded cylindrical panels under axial compression using a meshless approach
• CHAOTIC AND BIFURCATION DYNAMIC BEHAVIOR OF FUNCTIONALLY GRADED CURVED PANELS UNDER AERO-THERMAL LOADS
• Nonlinear Vibrations and Stability of Shells and Plates
• Theoretical considerations of panel flutter at high supersonic Mach numbers.

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