Analytical formulation for local buckling and post-buckling analysis of stiffened laminated panels C Bisagni, R Vescovini Thin-Walled Structures 47 (3), 318-334, 2009 | 167 | 2009 |
A variable-kinematic model for variable stiffness plates: Vibration and buckling analysis R Vescovini, L Dozio Composite Structures 142, 15-26, 2016 | 99 | 2016 |
Single-stringer compression specimen for the assessment of damage tolerance of postbuckled structures C Bisagni, R Vescovini, CG Dávila Journal of Aircraft 48 (2), 495-502, 2011 | 83 | 2011 |
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 | 76 | 2018 |
Failure analysis of composite multi-stringer panels using simplified models R Vescovini, CG Davila, C Bisagni Composites Part B: Engineering 45 (1), 939-951, 2013 | 73 | 2013 |
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 | 69 | 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 | 63 | 2016 |
Two-step procedure for fast post-buckling analysis of composite stiffened panels R Vescovini, C Bisagni Computers & Structures 128, 38-47, 2013 | 55 | 2013 |
Buckling analysis and optimization of stiffened composite flat and curved panels R Vescovini, C Bisagni AIAA journal 50 (4), 904-915, 2012 | 54 | 2012 |
Fast tool for buckling analysis and optimization of stiffened panels C Bisagni, R Vescovini Journal of aircraft 46 (6), 2041-2053, 2009 | 54 | 2009 |
Single-mode solution for post-buckling analysis of composite panels with elastic restraints loaded in compression R Vescovini, C Bisagni Composites Part B: Engineering 43 (3), 1258-1274, 2012 | 48 | 2012 |
A framework based on physics-informed neural networks and extreme learning for the analysis of composite structures CA Yan, R Vescovini, L Dozio Computers & Structures 265, 106761, 2022 | 47 | 2022 |
Exact refined buckling solutions for laminated plates under uniaxial and biaxial loads R Vescovini, L Dozio Composite Structures 127, 356-368, 2015 | 47 | 2015 |
A semi-analytical approach for the analysis of variable-stiffness panels with curvilinear stiffeners R Vescovini, V Oliveri, D Pizzi, L Dozio, PM Weaver International Journal of Solids and Structures 188, 244-260, 2020 | 40 | 2020 |
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 |
Efficient post-buckling analysis of variable-stiffness plates using a perturbation approach R Vescovini, E Spigarolo, EL Jansen, L Dozio Thin-Walled Structures 143, 106211, 2019 | 32 | 2019 |
Semi-analytical buckling analysis of omega stiffened panels under multi-axial loads R Vescovini, C Bisagni Composite Structures 120, 285-299, 2015 | 31 | 2015 |
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 | 25 | 2021 |
Free vibrations of conical shells via Ritz method R Vescovini, N Fantuzzi International Journal of Mechanical Sciences 241, 107925, 2023 | 24 | 2023 |
Thermal buckling behaviour of thin and thick variable-stiffness panels R Vescovini, L Dozio Journal of Composites Science 2 (4), 58, 2018 | 24 | 2018 |