Capabilities Novotech because of the long period of activity, most of 25 years, has gained over time the specific expertise in various engineering aerospace and other high-tech fields. Starting from the initial activity in the field of GVT and Aeroelasticity, it has gradually expanded its expertise in the fields of various kinds of simulations, analysis…
NOVOTECH completed a GVT survey on the Vulcanair A – Viator AP600 Aircraft in order to identify its structural dynamic characteristics, and to demonstrate the aircraft’s conformity with the EASA CS-23 norms par. 23.629 “Flutter”. The modal parameters (natural frequencies, damping and mode-shapes) were determined for both stick-free and stick-fixed conditions. NOVOTECH proceeded to test…
This Project is related to the Italian nuclear decommissioning of the power plant site of Garigliano (ITALY) managed by Sogin, the Italian State-owned company responsible. NOVOTECH, by subcontract of the GRIE.C.AM Company, has performed these main different activities: a) Statistical analysis of historical wind data recorded by the wind measurement station; b) Definition of FE Model…
Within PON SFIDA Project, NOVOTECH performed several activities as follows: • Define and evaluate an optimized tone noise/vibration control measures, applied to the cabin of the Alenia Aermacchi NTP Regional A/C. • Develop a passive device (Dynamic Vibration Absorber – DVA) to reduce the fuselage fundamental vibration frequency. Design, manufacture and test in laboratory about…
Starting from results obtained within SFIDA Project, the SCAVIR (Advanced Configurations Studies for an Innovative Regional Aircraft) activities were still aimed to improve the comfort level into the Regional aircraft cabin through the control of the propeller tonal noise and related vibrations generated by the propeller blades rotation. For these activities have been investigated Innovative…
We are engaged in the development and prototype manufacturing of
THE MARIN – AIR VEHICLE FOR THE MILLENNIAL GENERATION
Novotech performed a GVT on BS115 Aircraft, to define the modal parameters to be used as in the up-grade process of the dynamic aircraft F.E.M. model. The evaluation of the frequency response functions in several points of the structure correlating each one to the fixed excitation points in order to perform a Multi Input Multi…
