| 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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Detection of low-velocity impact-induced delaminations in composite laminates using Auto-Regressive models, file e3835314-ab80-15e8-e053-a505fe0a3de9
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207
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Finite element modeling of dielectric elastomer actuators for space applications, file e3835315-c8f2-15e8-e053-a505fe0a3de9
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120
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Green sandwich structures under impact. Experimental vs numerical analysis, file e3835323-2c3e-15e8-e053-a505fe0a3de9
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111
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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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Dynamic response of green sandwich structures, file e3835328-22de-15e8-e053-a505fe0a3de9
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47
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Thermomechanical buckling analysis of the e&p-fgm beams integrated by nanocomposite supports immersed in a hygrothermal environment, file 750a49f1-a22a-427a-9556-6968ebe05895
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9
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null, file e383531a-7ce4-15e8-e053-a505fe0a3de9
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9
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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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DAMAGE TOLERANCE OF HEMP FIBRE REINFORCED BIO-BASED EPOXY LAMINATES SUBJECTED TO LOW-VELOCITY IMPACT, file e3835312-d610-15e8-e053-a505fe0a3de9
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6
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Revisiting the shapes of spacecraft structures according to 3d additive manufacturing, file e3835316-48c1-15e8-e053-a505fe0a3de9
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6
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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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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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Low-velocity impact behaviour of hemp fibre reinforced bio-based epoxy laminates, file e3835314-b515-15e8-e053-a505fe0a3de9
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4
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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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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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Smart thermal protection leading edges, file e3835311-528d-15e8-e053-a505fe0a3de9
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3
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Finite element models of piezoelectric actuators for active flow control, file e3835311-f59a-15e8-e053-a505fe0a3de9
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3
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Effects of a High Fidelity Filter on the attitude stabilization of a flexible spacecraft, file e383531b-28e9-15e8-e053-a505fe0a3de9
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3
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Monitoring of a controlled space flexible multibody by means of embedded piezoelectric sensors and cameras synergy, file e383531b-beb0-15e8-e053-a505fe0a3de9
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3
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Finite element models of piezoelectric actuation for active flow control, file e383531d-5de8-15e8-e053-a505fe0a3de9
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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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Magneto-electro-elastic vibration analysis of modified couple stress-based three-layered micro rectangular plates exposed to multi-physical fields considering the flexoelectricity effects, file e3835328-6eab-15e8-e053-a505fe0a3de9
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3
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Coupled electro-aeroelastic energy harvester model based on piezoelectric transducers, VIV-galloping interaction and nonlinear switching circuits, file 8dccd85d-144b-4d2b-ae9f-e3a934aa2e3e
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2
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Numerical Simulation of the Behaviour of Inflatable Structures for Space, file e3835311-96ce-15e8-e053-a505fe0a3de9
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2
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Damage tolerance of carbon/flax hybrid composites subjected to low velocity impact, file e3835314-b517-15e8-e053-a505fe0a3de9
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2
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Low velocity impact response of basalt-aluminium fibre metal laminates, file e3835314-b519-15e8-e053-a505fe0a3de9
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2
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Sparse sensing detection of impact-induced delaminations in composite laminates, file e3835315-5e34-15e8-e053-a505fe0a3de9
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2
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High velocity impact behaviour of hybrid basalt-carbon/epoxy composites, file e3835316-dae9-15e8-e053-a505fe0a3de9
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2
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Innovative composite material component with embedded self-powered wireless sensor device for structural monitoring, file e383531b-879d-15e8-e053-a505fe0a3de9
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2
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Thermo-elastic buckling of honeycomb micro plates integrated with FG-GNPs reinforced epoxy skins with stretching effect, file e383532c-2fb2-15e8-e053-a505fe0a3de9
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2
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Effect of ZnO-decorated electrospun veils on the damage tolerance of CFRP laminates, file b9e5f98f-63ea-4748-8c0a-746e5be22407
|
1
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Smart Thermal Protection Systems (Smart TPS), file e3835311-a505-15e8-e053-a505fe0a3de9
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1
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Aeroheating reduction by active thermal protection structures for a re-entry vehicle, file e3835311-a85b-15e8-e053-a505fe0a3de9
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1
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Finite element analysis of a solid booster flexible bearing joint for thrust vector control, file e3835312-2991-15e8-e053-a505fe0a3de9
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1
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Drop-weight impact behaviour of woven hybrid basalt-carbon/epoxy composites, file e3835312-2992-15e8-e053-a505fe0a3de9
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1
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Composite structure of a cubesat satellite with embedded sensors for structural monitoring experiment, file e3835315-a23f-15e8-e053-a505fe0a3de9
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1
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Attitude stabilization of a flexible spacecraft using combined PZT/optical sensors, file e383531b-86ae-15e8-e053-a505fe0a3de9
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1
|
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Analysis of damage in composite laminates with embedded piezoelectric patches subjected to bending action, file e383531b-a008-15e8-e053-a505fe0a3de9
|
1
|
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Variable curvature concepts for smart thermal protection systems (smart TPS), file e383531d-4494-15e8-e053-a505fe0a3de9
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1
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Numerical simulation of the behavior of inflatable structures for space, file e383531d-4c4f-15e8-e053-a505fe0a3de9
|
1
|
|
Static and dynamic characterization of agglomerated cork and related sandwich structures, file e383531e-8104-15e8-e053-a505fe0a3de9
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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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Analysis of damage in hybrid composites subjected to ballistic impact. An integrated non-destructive approach, file e3835323-32f3-15e8-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
|
1
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Flutter investigation for piezoelectric aeroelastic energy harvester, file e3835323-e713-15e8-e053-a505fe0a3de9
|
1
|
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Impact and post-impact properties of multiscale carbon fiber composites interleaved with carbon nanotube sheets, file e3835324-0a72-15e8-e053-a505fe0a3de9
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1
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Impact behavior of sandwich structures made of flax/epoxy face sheets and agglomerated cork, file e3835324-90fc-15e8-e053-a505fe0a3de9
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1
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Effect of basalt fibre hybridization on high velocity impact behaviour of carbon/epoxy composites, file e3835328-420c-15e8-e053-a505fe0a3de9
|
1
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Falling-weight impact and post-impact flexural performance of hybrid flax/carbon laminates, file e3835328-487d-15e8-e053-a505fe0a3de9
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1
|
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Effect of temperature and MWCNTs on low velocity impact response of CFRP laminates, file e383532b-e79b-15e8-e053-a505fe0a3de9
|
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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Low-velocity impact response of MWCNTs toughened CFRP composites. Stacking sequence and temperature effects, file e383532e-8e12-15e8-e053-a505fe0a3de9
|
1
|
| Totale |
1.152 |