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 | 160 | 2016 |
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 | 66 | 2014 |
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 | 57 | 2017 |
PrandtlPlane Joined Wing: Body Freedom Flutter, Limit Cycle Oscillation And Freeplay Studies Journal of Fluids and Structures R Cavallaro, R Bombardieri, L Demasi, A Iannelli Journal of Fluids and Structures, 2015 | 53 | 2015 |
PrandtlPlane Joined Wing: Body Freedom Flutter, Limit Cycle Oscillation and Freeplay Studies R Cavallaro, R Bombardieri, L Demasi, A Iannelli AIAA SciTech > 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015 | 53 | 2015 |
Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Applications L Demasi, G Monegato, E Rizzo, R Cavallaro, A Dipace Journal of Optimization Theory and Applications, 1-26, 2015 | 48* | 2015 |
Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory D Luciano, M Giovanni, D Antonio, C Rauno AIAA SciTech - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015 | 45* | 2015 |
Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory D Luciano, M Giovanni, D Antonio, C Rauno AIAA SciTech - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015 | 44* | 2015 |
Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Results D Luciano, M Giovanni, R Emanuele, C Rauno, D Antonio AIAA SciTech > 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015 | 44* | 2015 |
Minimum Induced Drag Theorems for Joined Wings, Closed Systems, and Generic Biwings: Theory D Luciano, M Giovanni, D Antonio, C Rauno AIAA SciTech > 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015 | 44* | 2015 |
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, 1-36, 2015 | 36 | 2015 |
Minimum Induced Drag Theorems for Multi-Wing Systems L Demasi, G Monegato, R Cavallaro 57th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials …, 2016 | 33 | 2016 |
Generalized Unified Formulation Shell Element for Functionally Graded Variable-Stiffness Composite Laminates and Aeroelastic Applications L Demasi, Y Ashenafi, R Cavallaro, E Santarpia AIAA SciTech > 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015 | 29 | 2015 |
Postcritical analysis of PrandtlPlane joined-wing configurations L Demasi, R Cavallaro, A Márquez Razón AIAA journal 51 (1), 161-177, 2013 | 29 | 2013 |
Nonlinear structural, nonlinear aerodynamic model for static aeroelastic problems E Kantor, DE Raveh, R Cavallaro AIAA Journal 57 (5), 2158-2170, 2019 | 27 | 2019 |
Nonlinear analysis of PrandtlPlane joined wings: Effects of anisotropy R Cavallaro, L Demasi, A Passariello AIAA journal 52 (5), 964-980, 2014 | 24 | 2014 |
Phenomenology of nonlinear aeroelastic responses of highly deformable joined wings R Cavallaro, A Iannelli, L Demasi, AM Razon Advances in aircraft and spacecraft science 2 (2), 125, 2015 | 23 | 2015 |
A hybrid reduced-order model for the aeroelastic analysis of flexible subsonic wings—A parametric assessment M Berci, R Cavallaro Aerospace 5 (3), 76, 2018 | 21 | 2018 |
Minimum induced drag conditions for truss-braced wings L Demasi, G Monegato, R Cavallaro, R Rybarczyk AIAA Journal 56 (12), 4669-4684, 2018 | 19 | 2018 |
Aeroelasticity of the PrandtlPlane: Body freedom flutter, freeplay, and limit cycle oscillation R Cavallaro, R Bombardieri, S Silvani, L Demasi, G Bernardini Variational analysis and aerospace engineering: mathematical challenges for …, 2016 | 17 | 2016 |