Titolo |
Pubblicato in |
Anno |
OMA study on the structural dynamic properties of a launcher vehicle using flight data |
Proceedings of 58th AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 2017 |
2017 |
Preliminary design of a mission to triton based on a concurrent engineering approach |
Proceedings of the XXIV International Conference of the Italian Association of Aeronautics and Astronautics |
2017 |
Effects of variable resistance on smart structures of cubic reconnaissance satellites in various thermal and frequency shocking conditions |
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY |
2017 |
A fused filament fabrication procedure for smart components with embedded electronics |
VIII ECCOMAS Thematic Conference on Smart Structures and Materials SMART 2017 |
2017 |
Modal parameter estimate of time-varying system using operational modal analysis based on hilbert transform |
17th international forum on aeroelasticity and structural dynamics, IFASD 2017 |
2017 |
A method for the estimate of modal parameters of time-dependent aerospace structural system using operational data |
IOMAC 2017 - 7th International operational modal analysis conference. proceedings |
2017 |
Modeling and design of a nonlinear aeroelastic energy harvester |
Proceedings of the International Astronautical Congress, IAC |
2017 |
Analytical, experimental and numerical analysis of stability and degradation of smart structure for cubic reconnaissance satellites |
DeMEASS VIII |
2017 |
Piezoelectric Nonlinear Aeroelastic Energy Harvester |
28th International Conference on Adaptive Structures and Technologies October 8-11th, 2017, Cracow, Poland |
2017 |
A Fused Filament Additive Fabrication Procedure for Smart Components with Embedded Electronics |
ICAST2017: 28th International Conference on Adaptive Structures and Technologies |
2017 |