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Rauno Cavallaro
Rauno Cavallaro
Associate Professor, Universidad Carlos 3 de Madrid, Spain
Verified email at uc3m.es
Title
Cited by
Cited by
Year
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
1512016
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
672014
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
552017
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
522015
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
522015
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
47*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
D Luciano, M Giovanni, D Antonio, C Rauno
AIAA SciTech - 56th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and …, 2015
43*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
43*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
43*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
352015
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
322016
Postcritical analysis of PrandtlPlane joined-wing configurations
L Demasi, R Cavallaro, A Márquez Razón
AIAA journal 51 (1), 161-177, 2013
302013
Nonlinear structural, nonlinear aerodynamic model for static aeroelastic problems
E Kantor, DE Raveh, R Cavallaro
AIAA Journal 57 (5), 2158-2170, 2019
262019
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
262015
Nonlinear analysis of PrandtlPlane joined wings: Effects of anisotropy
R Cavallaro, L Demasi, A Passariello
AIAA journal 52 (5), 964-980, 2014
242014
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
222015
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
202018
Minimum induced drag conditions for truss-braced wings
L Demasi, G Monegato, R Cavallaro, R Rybarczyk
AIAA Journal 56 (12), 4669-4684, 2018
192018
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
172016
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