| 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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Structural damping models for passive aeroelastic control, file e3835322-4265-15e8-e053-a505fe0a3de9
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225
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Energy harvesting towards self-powered iot devices, file e3835328-2c6a-15e8-e053-a505fe0a3de9
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211
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Effects of variable resistance on smart structures of cubic reconnaissance satellites in various thermal and frequency shocking conditions, file e3835318-7fd6-15e8-e053-a505fe0a3de9
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204
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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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Digital design of medical replicas via desktop systems: shape evaluation of colon parts, file e383531d-e99a-15e8-e053-a505fe0a3de9
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135
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A review on mechanisms for piezoelectric-based energy harvesters, file e3835328-2c3e-15e8-e053-a505fe0a3de9
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86
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Erratum to “Effects of variable resistance on smart structures of cubic reconnaissance satellites in various thermal and frequency shocking conditions”, file e3835321-89fb-15e8-e053-a505fe0a3de9
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83
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Numerical assessment and parametric optimization of a piezoelectric wind energy harvester for IoT-based applications, file e383532c-e3d1-15e8-e053-a505fe0a3de9
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72
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Perturbation methods and proper orthogonal decomposition analysis for nonlinear aeroelastic systems, file e3835315-ce41-15e8-e053-a505fe0a3de9
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71
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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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Study of the surface and dimensional quality of the alsi10mg thin-wall components manufactured by selective laser melting, file e383532c-cc0a-15e8-e053-a505fe0a3de9
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58
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A predictive decision support system for coronavirus disease 2019 response management and medical logistic planning, file bf5ec4b1-8d3f-4ca9-af0b-c95dab659518
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16
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Preliminary design of a mission to triton based on a concurrent engineering approach, file e383531c-dc47-15e8-e053-a505fe0a3de9
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12
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A Geospatial Artificial Intelligence and satellite-based earth observation cognitive system in response to COVID-19, file e383532e-f16a-15e8-e053-a505fe0a3de9
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11
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null, file e383531a-7ce4-15e8-e053-a505fe0a3de9
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9
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Selective laser melting of a 1U cubesat structure. Design for additive manufacturing and assembly, file e383531e-1e93-15e8-e053-a505fe0a3de9
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9
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An additive manufacturing redesign of a military aircraft equipment within a logistic 4.0 framework, file e3835324-79d3-15e8-e053-a505fe0a3de9
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8
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Modeling and design of a piezoelectric nonlinear aeroelastic energy harvester, file e3835328-4901-15e8-e053-a505fe0a3de9
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8
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OMA analysis of a launcher under operational conditions with time-varying properties, file e383531a-a017-15e8-e053-a505fe0a3de9
|
7
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Design and performance evaluation of a piezoelectric aeroelastic energy harvester based on the limit cycle oscillation phenomenon, file e3835320-1c96-15e8-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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Aircraft part substitution via additive manufacturing: design, simulation, fabrication and testing, file e383532b-e2fa-15e8-e053-a505fe0a3de9
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6
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The ECO4CO project among retrospective data, improving of algorithms, predictive hypothesis and future perspectives to tackle health emergencies, file e383532f-12c3-15e8-e053-a505fe0a3de9
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6
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Selective laser melting of a 1U CubeSat structure. Design for additive manufacturing and assembly., file e3835321-be60-15e8-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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An industry 4.0 approach to large scale production of satellite constellations. The case study of composite sandwich panel manufacturing, file e383532d-a42e-15e8-e053-a505fe0a3de9
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5
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An earth observation cognitive system in response to Sars-Covid-19 emergency, file e383532e-641a-15e8-e053-a505fe0a3de9
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5
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Smart manufacturing in the space industry. A cyber-physical system architecture and its implementation to a mait process for mega constellations of satellites, file e383532e-ed3f-15e8-e053-a505fe0a3de9
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5
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Revisiting the configuration of small satellites structures in the framework of 3D additive manufacturing, file e383531a-6e25-15e8-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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On the modal diagonalization of viscoelastic mechanical systems, file e383531b-8dfc-15e8-e053-a505fe0a3de9
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4
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Vibration of FG porous three-layered beams equipped by agglomerated nanocomposite patches resting on Vlasov's foundation, file e383532c-b31c-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
|
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
|
3
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null, file e383531e-1338-15e8-e053-a505fe0a3de9
|
3
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null, file e383531e-5cc7-15e8-e053-a505fe0a3de9
|
3
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Time- and frequency-domain linear viscoelastic modeling of highly damped aerospace structures, file e383531f-c91a-15e8-e053-a505fe0a3de9
|
3
|
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A preliminary design of a mission to Triton: a concurrent engineering approach, file e3835322-2ea0-15e8-e053-a505fe0a3de9
|
3
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Experimental evaluation of piezoelectric energy harvester based on flag-flutter, file e3835323-9c3d-15e8-e053-a505fe0a3de9
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3
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Basic technology for smart multifunctional components with embedded electronics using fused filament fabrication, file e3835324-6e91-15e8-e053-a505fe0a3de9
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3
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Investigation of deformation in bimorph piezoelectric actuator: analytical, numerical and experimental approach, file e3835327-efd5-15e8-e053-a505fe0a3de9
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3
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Assessment of smart transformation in the manufacturing process of aerospace components through a data-driven approach, file 1f0b99ca-44fc-457e-8285-43a6022614c3
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2
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Innovative methodology for the preliminary design approach for Low Earth Orbit constellations, file 3ca59391-b07d-4e13-a639-a09aecf61260
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2
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Nonlinear aeroelastic response of a flat panel. A Normal Form approach., file e3835313-515a-15e8-e053-a505fe0a3de9
|
2
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Effects of variable resistance on smart structures of cubic reconnaissance satellites in various thermal and frequency shocking conditions, file e383531d-038f-15e8-e053-a505fe0a3de9
|
2
|
|
Modal parameter estimate of time-varying system using operational modal analysis based on hilbert transform, file e383531d-8f40-15e8-e053-a505fe0a3de9
|
2
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Modal parameter estimate of time-varying system using operational modal analysis based on hilbert transform, file e383531d-8f41-15e8-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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Design and realization of an additive manufactured multifunctional spacecraft structure through a systems and concurrent engineering approach, file e3835328-160c-15e8-e053-a505fe0a3de9
|
2
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A review on applications of piezoelectric materials in aerospace industry, file e3835328-48ff-15e8-e053-a505fe0a3de9
|
2
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Reliability risk analysis for the aeroelastic piezoelectric energy harvesters, file e3835328-5794-15e8-e053-a505fe0a3de9
|
2
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Characterization and implementation of a piezoelectric energy harvester configuration: analytical, numerical and experimental approach, file e3835328-7e3d-15e8-e053-a505fe0a3de9
|
2
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Piezoelectric aeroelastic energy harvesting, file 01b75557-41fc-4310-beff-6cef660504f2
|
1
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A model-based approach for the preliminary design of small satellites constellations based on user needs analysis. The Iride optical sub-constellation case study, file d738d42e-a129-40ae-ac81-77aacf7a91b3
|
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
|
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
|
1
|
|
Design and performance evaluation of an aeroelastic energy harvester based on the limit cycle oscillation phenomenon, file e383531e-1e96-15e8-e053-a505fe0a3de9
|
1
|
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A method for the estimate of modal parameters of time-dependent aerospace structural system using operational data, file e3835321-63dd-15e8-e053-a505fe0a3de9
|
1
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A preliminary design of a mission to Triton: a concurrent engineering approach, file e3835321-c91e-15e8-e053-a505fe0a3de9
|
1
|
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Modeling and design of a nonlinear aeroelastic energy harvester, file e3835321-f747-15e8-e053-a505fe0a3de9
|
1
|
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Response of piezoelectric materials on thermomechanical shocking and electrical shocking for aerospace applications, file e3835322-115f-15e8-e053-a505fe0a3de9
|
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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Design and realization of an additive manufactured multifunctional spacecraft structure through a systems and concurrent engineering approach, file e3835327-f782-15e8-e053-a505fe0a3de9
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1
|
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Smart manufacturing in the framework of space industry. An industry 4.0 approach to large scale production of satellite constellations, file e383532b-fce8-15e8-e053-a505fe0a3de9
|
1
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Analytical, experimental and numerical analysis of stability and degradation of smart structure for cubic reconnaissance satellites, file e383532c-e847-15e8-e053-a505fe0a3de9
|
1
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| Totale |
2.266 |