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Riccardo Vescovini
Riccardo Vescovini
Verified email at polimi.it
Title
Cited by
Cited by
Year
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
1642009
A variable-kinematic model for variable stiffness plates: Vibration and buckling analysis
R Vescovini, L Dozio
Composite Structures 142, 15-26, 2016
902016
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
752011
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
702018
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
692013
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
642018
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
592016
Fast tool for buckling analysis and optimization of stiffened panels
C Bisagni, R Vescovini
Journal of aircraft 46 (6), 2041-2053, 2009
532009
Two-step procedure for fast post-buckling analysis of composite stiffened panels
R Vescovini, C Bisagni
Computers & Structures 128, 38-47, 2013
522013
Buckling analysis and optimization of stiffened composite flat and curved panels
R Vescovini, C Bisagni
AIAA journal 50 (4), 904-915, 2012
512012
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
482012
Exact refined buckling solutions for laminated plates under uniaxial and biaxial loads
R Vescovini, L Dozio
Composite Structures 127, 356-368, 2015
462015
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
342020
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
332022
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
332017
Semi-analytical buckling analysis of omega stiffened panels under multi-axial loads
R Vescovini, C Bisagni
Composite Structures 120, 285-299, 2015
302015
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
272019
Assessment of the damage tolerance of post-buckled hat-stiffened panels using single stringer specimens
C Bisagni, R Vescovini, C Davila
51st AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics, and materials …, 2010
232010
A procedure for the evaluation of damping effects in composite laminated structures
R Vescovini, C Bisagni
Progress in Aerospace Sciences 78, 19-29, 2015
212015
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
202021
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