Static and dynamic FE analysis of piezolaminated composite shells considering electric field nonlinearity under thermo-electro-mechanical loads
DOI10.1007/s00707-018-2284-2zbMath1430.74110OpenAlexW2898484459WikidataQ129032198 ScholiaQ129032198MaRDI QIDQ2296324
Mekala N. Rao, Rüdiger Schmidt, Kai-Uwe Schröder
Publication date: 18 February 2020
Published in: Acta Mechanica (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1007/s00707-018-2284-2
Finite element methods applied to problems in solid mechanics (74S05) Thermal effects in solid mechanics (74F05) Shells (74K25) Electromagnetic effects in solid mechanics (74F15) Random materials and composite materials (74A40)
Related Items (4)
Cites Work
- Active control of geometrically nonlinear transient vibrations of laminated composite cylindrical panels using piezoelectric fiber reinforced composite
- Nonlinear dynamic stability of laminated composite shells integrated with piezoelectric layers in thermal environment
- Efficient modeling of smart piezoelectric composite laminates: a review
- Non-linear shear vibrations of piezoceramic actuators
- An incremental algorithm for static shape control of smart structures with nonlinear piezoelectric actuators
- Finite rotation FE-simulation and active vibration control of smart composite laminated structures
- Mixed variational principles in nonlinear electroelasticity
- A robust non-linear mixed hybrid quadrilateral shell element
- A geometrically non-linear piezoelectric solid shell element based on a mixed multi-field variational formulation
- On a non-linear formulation for curved Timoshenko beam elements considering large displacement/rotation increments
- Finite Elements Based Upon Mindlin Plate Theory With Particular Reference to the Four-Node Bilinear Isoparametric Element
- A simple quadrilateral shell element
- Analysis of piezoelastic structures with laminated piezoelectric triangle shell elements
- Variable structure control and active vibration suppression of flexible spacecraft during attitude maneuver
- A class of mixed assumed strain methods and the method of incompatible modes
This page was built for publication: Static and dynamic FE analysis of piezolaminated composite shells considering electric field nonlinearity under thermo-electro-mechanical loads