| ∞ 6 mixed plate theories based on the generalized unified formulation. Part I: governing equations L Demasi Composite structures 87 (1), 1-11, 2009 | 263* | 2009 |
| Classical and advanced multilayered plate elements based upon PVD and RMVT. Part 1: Derivation of finite element matrices E Carrera, L Demasi International Journal for Numerical Methods in Engineering 55 (2), 191-231, 2002 | 205 | 2002 |
| ∞ 3 Hierarchy plate theories for thick and thin composite plates: the generalized unified formulation L Demasi Composite Structures 84 (3), 256-270, 2008 | 176 | 2008 |
| Classical and advanced multilayered plate elements based upon PVD and RMVT. Part 2: Numerical implementations E Carrera, L Demasi International Journal for Numerical Methods in Engineering 55 (3), 253-291, 2002 | 160 | 2002 |
| Challenges, ideas, and innovations of joined-wing configurations: a concept from the past, an opportunity for the future R Cavallaro, L Demasi Progress in Aerospace Sciences 87, 1-93, 2016 | 149 | 2016 |
| Refined multilayered plate elements based on Murakami zig–zag functions L Demasi Composite Structures 70 (3), 308-316, 2005 | 130 | 2005 |
| Improved bending analysis of sandwich plates using a zig-zag function S Brischetto, E Carrera, L Demasi Composite Structures 89 (3), 408-415, 2009 | 104 | 2009 |
| Invariant formulation for the minimum induced drag conditions of nonplanar wing systems L Demasi, A Dipace, G Monegato, R Cavallaro AIAA journal 52 (10), 2223-2240, 2014 | 67 | 2014 |
| Three-dimensional closed form solutions and exact thin plate theories for isotropic plates L Demasi Composite Structures 80 (2), 183-195, 2007 | 64 | 2007 |
| Two benchmarks to assess two-dimensional theories of sandwich, composite plates E Carrera, L Demasi AIAA journal 41 (7), 1356-1362, 2003 | 61 | 2003 |
| Dynamic aeroelasticity of structurally nonlinear configurations using linear modally reduced aerodynamic generalized forces L Demasi, E Livne AIAA journal 47 (1), 70-90, 2009 | 55 | 2009 |
| Equivalent Single Layer, Zig-Zag, and Layer Wise theories for variable angle tow composites based on the Generalized Unified Formulation L Demasi, G Biagini, F Vannucci, E Santarpia, R Cavallaro Composite Structures 177, 54-79, 2017 | 54 | 2017 |
| Prandtlplane joined wing: Body freedom flutter, limit cycle oscillation and freeplay studies R Cavallaro, R Bombardieri, L Demasi, A Iannelli Journal of Fluids and Structures 59, 57-84, 2015 | 52 | 2015 |
| 2D, quasi 3D and 3D exact solutions for bending of thick and thin sandwich plates L Demasi Journal of Sandwich Structures & Materials 10 (4), 271-310, 2008 | 51 | 2008 |
| Investigation on the conditions of minimum induced drag of closed wing systems and C-wings L Demasi Journal of Aircraft 44 (1), 81-99, 2007 | 50 | 2007 |
| Vibration analysis of anisotropic simply supported plates by using variable kinematic and Rayleigh-Ritz method E Carrera, FA Fazzolari, L Demasi | 48 | 2011 |
| Multilayered Finite Plate Element based on Reissner Mixed Variational Theorem. Part I: Theory. E Carrera, L Demasi International Journal for Numerical Methods in Engineering 55, 191-231, 2002 | 44 | 2002 |
| Partially layer wise advanced zig zag and HSDT models based on the generalized unified formulation L Demasi Engineering Structures 53, 63-91, 2013 | 43 | 2013 |
| Minimum induced drag theorems for joined wings, closed systems, and generic biwings: Theory L Demasi, G Monegato, A Dipace, R Cavallaro Journal of Optimization Theory and Applications 169, 200-235, 2016 | 42* | 2016 |
| Partially zig-zag advanced higher order shear deformation theories based on the generalized unified formulation L Demasi Composite Structures 94 (2), 363-375, 2012 | 42 | 2012 |
Rauno CavallaroAssociate Professor, Universidad Carlos 3 de Madrid, SpainVerified email at uc3m.es
