A unified formulation to assess multilayered theories for piezoelectric plates D Ballhause, M D’Ottavio, B Kröplin, E Carrera Computers & structures 83 (15), 1217-1235, 2005 | 127 | 2005 |
A Sublaminate Generalized Unified Formulation for the analysis of composite structures M D’Ottavio Composite Structures 142, 187-199, 2016 | 81 | 2016 |
On the application of the Ritz method to free vibration and buckling analysis of highly anisotropic plates R Vescovini, L Dozio, M D’Ottavio, O Polit Composite Structures 192, 460-474, 2018 | 74 | 2018 |
Buckling and wrinkling of anisotropic sandwich plates R Vescovini, M D’Ottavio, L Dozio, O Polit International Journal of Engineering Science 130, 136-156, 2018 | 66 | 2018 |
Bending analysis of composite laminated and sandwich structures using sublaminate variable-kinematic Ritz models M D’Ottavio, L Dozio, R Vescovini, O Polit Composite Structures 155, 45-62, 2016 | 62 | 2016 |
Closed-form solutions for the free-vibration problem of multilayered piezoelectric shells M D’Ottavio, D Ballhause, B Kröplin, E Carrera Computers & structures 84 (22), 1506-1518, 2006 | 56 | 2006 |
Variable-kinematics approach for linearized buckling analysis of laminated plates and shells M D'Ottavio, E Carrera AIAA journal 48 (9), 1987-1996, 2010 | 52 | 2010 |
An efficient finite shell element for the static response of piezoelectric laminates P Vidal, M D'Ottavio, M Ben Thaïer, O Polit Journal of Intelligent Material Systems and Structures 22 (7), 671-690, 2011 | 47 | 2011 |
An extension of Reissner mixed variational theorem to piezoelectric laminates M D'Ottavio, B Kröplin Mechanics of advanced materials and structures 13 (2), 139-150, 2006 | 45 | 2006 |
Benchmark solutions and assessment of variable kinematics models for global and local buckling of sandwich struts M D’Ottavio, O Polit, W Ji, AM Waas Composite Structures 156, 125-134, 2016 | 41 | 2016 |
Robust C0 high‐order plate finite element for thin to very thick structures: mechanical and thermo‐mechanical analysis O Polit, P Vidal, M D'Ottavio International Journal for Numerical Methods in Engineering 90 (4), 429-451, 2012 | 40 | 2012 |
Assessment of plate theories for free-edge effects M D’Ottavio, P Vidal, E Valot, O Polit Composites Part B: Engineering 48, 111-121, 2013 | 36 | 2013 |
Thermal buckling response of laminated and sandwich plates using refined 2-D models R Vescovini, M D’Ottavio, L Dozio, O Polit Composite Structures 176, 313-328, 2017 | 35 | 2017 |
High-order plate finite elements for smart structure analysis O Polit, M D’Ottavio, P Vidal Composite Structures 151, 81-90, 2016 | 29 | 2016 |
Bending analysis of laminated and sandwich plates using a layer-wise stress model ND Thai, M D’Ottavio, JF Caron Composite Structures 96, 135-142, 2013 | 28 | 2013 |
Considerations on higher-order finite elements for multilayered plates based on a unified formulation M D’Ottavio, D Ballhause, T Wallmersperger, B Kröplin Computers & structures 84 (19-20), 1222-1235, 2006 | 28 | 2006 |
Multiscale Modeling of Polymer Gels—Chemo-Electric Model versus Discrete Element Model T Wallmersperger, FK Wittel, M D'Ottavio, B Kröplin Mechanics of Advanced Materials and Structures 15 (3-4), 228-234, 2008 | 24 | 2008 |
Dynamic response of viscoelastic multiple-core sandwich structures M D’Ottavio, A Krasnobrizha, E Valot, O Polit, R Vescovini, L Dozio Journal of Sound and Vibration 491, 115753, 2021 | 23 | 2021 |
Linearized global and local buckling analysis of sandwich struts with a refined quasi-3D model M D’Ottavio, O Polit Acta Mechanica 226 (1), 81-101, 2015 | 22 | 2015 |
Benchmark of wrinkling formulae and methods for pre-sizing of aircraft lightweight sandwich structures M Ginot, M D'Ottavio, O Polit, C Bouvet, B Castanié Composite Structures 273, 114387, 2021 | 18 | 2021 |