| Nome |
# |
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Numerical and experimental investigation of piezoelectric energy harvester based on flag-flutter, file e3835325-14a7-15e8-e053-a505fe0a3de9
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481
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Dynamic shape reconstruction of a notched beam by proportional observer and multi-resolution analysis, file c27f8984-e308-4846-9938-4443a20a2033
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308
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Aircraft-fuel sloshing ROMs for aeroelastic analyses, file e3835322-425f-15e8-e053-a505fe0a3de9
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281
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Structural damping models for passive aeroelastic control, file e3835322-4265-15e8-e053-a505fe0a3de9
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222
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Structural validation of a realistic wing structure: the RIBES test article, file e3835321-2d63-15e8-e053-a505fe0a3de9
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216
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Mechanical systems virtual sensing by proportional observer and multi-resolution analysis, file e3835327-5a5e-15e8-e053-a505fe0a3de9
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206
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Nonlinear aeroelastic modeling via conformal mapping and vortex method for a flat-plate airfoil in arbitrary motion, file e3835314-438b-15e8-e053-a505fe0a3de9
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203
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OMA analysis of a launcher under operational conditions with time-varying properties, file e383531a-4bec-15e8-e053-a505fe0a3de9
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190
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A normal form analysis in a finite neighborhood of a hopf bifurcation: on the center manifold dimension, file e383531a-2f82-15e8-e053-a505fe0a3de9
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176
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Analysis of a sloshing beam experiment, file e3835322-4afa-15e8-e053-a505fe0a3de9
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162
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Aeroelastics/flight dynamics coupling effects of the semi aeroelastic hinge device, file e3835327-111d-15e8-e053-a505fe0a3de9
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99
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Performance evaluation of a piezoelectric energy harvester based on flag-flutter, file e3835328-3ad5-15e8-e053-a505fe0a3de9
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62
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Nonlinear reduced-order model for vertical sloshing by employing neural networks, file e383532f-467b-15e8-e053-a505fe0a3de9
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22
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Neural network-based reduced-order modeling for nonlinear vertical sloshing with experimental validation, file 2b73ac17-2019-4ac2-9fe4-52bd71d71951
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21
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Linear and nonlinear reduced order models for sloshing for aeroelastic stability and response predictions, file d5074e2e-9a20-430c-9177-7e984581b007
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18
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Multiphysics numerical investigation on the aeroelastic stability of a Le Mans Prototype car, file e383532a-4c27-15e8-e053-a505fe0a3de9
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12
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POD approach for unsteady aerodynamic model updating, file e3835312-9d6f-15e8-e053-a505fe0a3de9
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10
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Analysis of helicopter cabin vibrations due to rotor asymmetry and gust encounter, file e383531b-8626-15e8-e053-a505fe0a3de9
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9
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Sloshing ROMs for fluid-structure interactions in aerospace applications, file e3835324-7888-15e8-e053-a505fe0a3de9
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8
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Hydrofoil vibration induced by a random flow: a stochastic perturbation approach, file e3835311-9ec0-15e8-e053-a505fe0a3de9
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7
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OMA analysis of a launcher under operational conditions with time-varying properties, file e383531a-a017-15e8-e053-a505fe0a3de9
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7
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null, file e383531a-b2ee-15e8-e053-a505fe0a3de9
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7
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Load and deflection estimation of a fast catamaran towingtank model via reduced order modeling and optimal natural observer, file e383531b-d08e-15e8-e053-a505fe0a3de9
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7
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Structural damping models for passive aeroelastic control, file e383532d-01bd-15e8-e053-a505fe0a3de9
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7
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Sensitivity Analysis for the Dynamic Aeroelasticity of a Launch Vehicle, file e3835312-1cc6-15e8-e053-a505fe0a3de9
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6
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Experimental characterisation of sloshing tank dissipative behaviour in vertical harmonic excitation, file e383532e-6d86-15e8-e053-a505fe0a3de9
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6
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Experimental validation of solid rocket motor damping models, file e383531a-26e9-15e8-e053-a505fe0a3de9
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5
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On the control of aeroelastic/flight dynamic integrated stability of maneuvering aircraft, file e383531b-8623-15e8-e053-a505fe0a3de9
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5
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Numerical and experimental investigation of piezoelectric energy harvester based on flag-flutter, file e3835327-3d39-15e8-e053-a505fe0a3de9
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5
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A study of Reduced-Order Models for Gust-Response Analysis of Flexible Wings, file e3835311-bc3f-15e8-e053-a505fe0a3de9
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4
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Multi-disciplinary and multi-objective optimization of an unconventional aircraft concept, file e3835312-a936-15e8-e053-a505fe0a3de9
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4
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Semi-analytical unsteady aerodynamic model of a flexible thin airfoil, file e383531a-214e-15e8-e053-a505fe0a3de9
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4
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Normal form analysis of a forced aeroelastic plate, file e383531b-8142-15e8-e053-a505fe0a3de9
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4
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Finite-Element based modeling for flight dynamics and aeroelasticity of flexible aircraft, file e383531b-8144-15e8-e053-a505fe0a3de9
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4
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On the modal diagonalization of viscoelastic mechanical systems, file e383531b-8dfc-15e8-e053-a505fe0a3de9
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4
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Aeroelastics flight dynamics coupling effects of the semi-aeroelastic hinge device, file e3835327-4c48-15e8-e053-a505fe0a3de9
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4
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Experimental investigation on the damping mechanism in sloshing structures, file e383532b-e7d1-15e8-e053-a505fe0a3de9
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4
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POD Analysis for Aeroelastic Systems in a Neighborhood of a Hopf Bifurcation, file e3835313-5806-15e8-e053-a505fe0a3de9
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3
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A normal form analysis in a finite neighborhood of a hopf bifurcation: on the center manifold dimension, file e383531a-3fb1-15e8-e053-a505fe0a3de9
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3
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Coupled flight dynamics and aeroelasticity of very flexible aircraft based on commercial finite element solvers, file e383531b-87e8-15e8-e053-a505fe0a3de9
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3
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Time- and frequency-domain linear viscoelastic modeling of highly damped aerospace structures, file e383531f-c91a-15e8-e053-a505fe0a3de9
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3
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Multi-objective optimization for the design of an inconventional sun-powered high-altitude-long-endurance unmanned vehicle, file e3835320-034e-15e8-e053-a505fe0a3de9
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3
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Load and deflection estimation of a fast catamaran towingtank model via reduced order modeling and optimal natural observer, file e3835321-7ced-15e8-e053-a505fe0a3de9
|
3
|
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Experimental evaluation of piezoelectric energy harvester based on flag-flutter, file e3835323-9c3d-15e8-e053-a505fe0a3de9
|
3
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A linearized reduced-order model approach for sloshing to be used for aerospace design, file e3835328-e2bc-15e8-e053-a505fe0a3de9
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3
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Quasi-steady aeroelastic analysis of the semi-aeroelastic hinge including geometric nonlinearities, file e383532e-ab15-15e8-e053-a505fe0a3de9
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3
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Sloshing reduced-order model based on neural networks for aeroelastic analyses, file a744c0f0-9e56-403a-8925-4ea87c680f06
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2
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Nonlinear aeroelastic modeling via conformal mappings for typical section in arbitrary motion, file e3835312-aa11-15e8-e053-a505fe0a3de9
|
2
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Nonlinear aeroelastic response of a flat panel. A Normal Form approach., file e3835313-515a-15e8-e053-a505fe0a3de9
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2
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On the modal decoupling of linear mechanical systems with frequency-dependent viscoelastic behavior, file e3835313-c7df-15e8-e053-a505fe0a3de9
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2
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null, file e383531b-8dfe-15e8-e053-a505fe0a3de9
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2
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Semi-analytical unsteady aerodynamic modeling of a flexible thin airfoil in arbitrary motion, file e383531b-b1c6-15e8-e053-a505fe0a3de9
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2
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Nonlinear aeroelastic trim of very flexible aircraft described by detailed models, file e383531f-ec73-15e8-e053-a505fe0a3de9
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2
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Multi‑disciplinary and multi‑objective optimization of an over‑wing‑nacelle aircraft concept, file e3835323-01e7-15e8-e053-a505fe0a3de9
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2
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Damping modelling in aircraft flutter analyses, file e3835324-b554-15e8-e053-a505fe0a3de9
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2
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Damping modelling in aircraft flutter analyses, file e3835325-1837-15e8-e053-a505fe0a3de9
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2
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Sloshing ROMs for fluid-structure interactions in aerospace applications, file e3835327-afc7-15e8-e053-a505fe0a3de9
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2
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Sloshing reduced-order models for aeroelastic analyses of innovative aircraft configurations, file e383532e-37f8-15e8-e053-a505fe0a3de9
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2
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Surrogate finite-element modelling for launch vehicle multidisciplinary optimization, file e383532e-3d90-15e8-e053-a505fe0a3de9
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2
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Correction to: Sloshing wing dynamics - 2nd year project overview, file e383532e-bb91-15e8-e053-a505fe0a3de9
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2
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Sloshing reduced-order model trained with smoothed particle hydrodynamics simulations, file 59b5ec62-2e77-4865-9ed8-78637ee472bf
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1
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POD analysis for free response of linear and nonlinear marginally stable aeroelastic dynamical systems, file e3835312-01eb-15e8-e053-a505fe0a3de9
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1
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Genetic and gradient-based algorithms for the multi-objective optimization of aircraft design with aeroelastic constraints, file e3835312-a934-15e8-e053-a505fe0a3de9
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1
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Linearized Aeroelastic Gust Response Analysis of a Launch Vehicle, file e3835313-2474-15e8-e053-a505fe0a3de9
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1
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Non-linear modelling for Multi-Disciplinary and Multi-Objective Optimization of a complete aircraft, file e3835313-4dd0-15e8-e053-a505fe0a3de9
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1
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Multi-Objective Optimization Strategies for Aircraft Multi-Disciplinary Design, file e3835313-5ad6-15e8-e053-a505fe0a3de9
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1
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Analysis of Pareto-Frontier for Multidisciplinary Design Optimization
of Aircraft, file e3835313-60db-15e8-e053-a505fe0a3de9
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1
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On the control of aeroelastic/flight dynamic integrated stability of maneuvering aircraft, file e383531b-7e07-15e8-e053-a505fe0a3de9
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1
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A FEM-based approach for nonlinear aeroelastic trim of highly flexible aircraft, file e383531b-862d-15e8-e053-a505fe0a3de9
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1
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OMA study on the structural dynamic properties of a launcher vehicle using flight data, file e383531b-87ea-15e8-e053-a505fe0a3de9
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1
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Nonlinear aeroelastic modeling via conformal mappings for typical section in arbitrary motion, file e383531f-e690-15e8-e053-a505fe0a3de9
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1
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Genetic and gradient-based algorithms for the multi-objective optimization of aircraft design with aeroelastic constraints, file e3835320-9316-15e8-e053-a505fe0a3de9
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1
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Estimation of the deflection field over a ship structure model based on pointwise measurements, file e3835323-a834-15e8-e053-a505fe0a3de9
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1
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Experimental study of a flag-flutter energy harvester, file e3835323-e70c-15e8-e053-a505fe0a3de9
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1
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Flutter investigation for piezoelectric aeroelastic energy harvester, file e3835323-e713-15e8-e053-a505fe0a3de9
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1
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Sloshing wing dynamics-2nd year project overview, file e383532e-69a5-15e8-e053-a505fe0a3de9
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1
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Experimental validation of neural-network-based nonlinear reduced-order model for vertical sloshing, file e383532e-bd83-15e8-e053-a505fe0a3de9
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1
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Nonlinear sloshing integrated aeroelastic analyses of a research wing prototype, file e383532e-bd87-15e8-e053-a505fe0a3de9
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1
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| Totale |
2.873 |