Archive for… STRUCTURAL HEALTH MONITORING (SHM)

SAIA

Within the SAIA “Strutture Alari Innovative Aeronautiche” Project, (Program Contract Apulia Region), NOVOTECH has provided a specific contribute to wing design and sizing through the studie

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GROUND VIBRATION TEST (GVT) ON VIATOR AP600

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 EAS

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GRIE.C.AM.

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 subco

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SFIDA

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 Aer

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SCAVIR

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 t

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BOMBARDIER G-7000

BOMBARDIER G-7000: Evaluation of the A/C response to vertical tuned discrete gust and continuous turbulence in compliance EASA CS-25

NOVOTECH has been involved as sub-contractor of DEMA Spa

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MDCD – Control Board

With the support of our customer SICAMB SpA, , NOVOTECH is currently providing the design and the implementation of a Control Board unit , finalized to the functional test of the Main Deck Cargo Do

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SISTER-CHECK

Within the Call “Horizon 2020 – PON I&C 2014-20” issued by Italian Ministry of Economic Development, NOVOTECH is currently working, in partnership with DES Innovation, on the “SISTE

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COGEA

“COGEA” (Composite Certification in General Aviation) is a Project sponsored by Apulia Region. It aims to develop innovative design solutions for composite components of VLA (Very Light Aeropla

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GROUND VIBRATION TEST (GVT) ON BS115 AIRCRAFT

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 funct

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