05/2016-09/2017 AerospaceCockpit Static analysis (certification reports and detail FE model ) and Bird Strike Analysis on AW609 TiltRotor (FE model in ABAQUS Explicit)11/2015-05/2016Static and Crash analysis on AW169, Static Analysis for ThalesAlenia Space01/2011-11/2015 AerospaceAs an external supplier, resident AgustaWestland now Leonardo Helicopters in Cascina Costa (VA) ItalyStatic, and Crash analysis on AW169 new twin-engine helicopter Program:Static analysis : Engine mount, Cabin Upper Deck Structure, Cabin Floor Structure, Thermoplastic Tail Structure, Canopy Structure, Forward Cowling StructureBird Strike analysis using Abaqus Explicit: Forward Cowling and Canopy StructureFull Scale Static Test: Design and calculation of Rear to Tail equipment for FSSTExperimental activities: Airframe Temperature Survey on first and third prototype, and structural analysis of the interested are with a possible “disbonding” of the Honeycomb panel facings and the “decay” of the laminates; Airframe Structure strain gauge data comparison and checking between flight data and theoretical FEM results data; Strain gauge data comparison and checking between Fatigue Test of Anti-Torque Beam data and theoretical FEM results data.Fatigue analysis AW189 Program:AW189 Rescue Hoist Backup Structure Preliminary Fatigue and Damage Tolerance Analysis12/2010-01/2011 AerospaceAs an external supplier, resident in AssystemUK in Bristol UKStatic analysis, Rib 16-21 Airbus A320 EFT Using Airbus software10/2010-11/2010 AerospaceStatic analysis Airbus A320&A321 Spoiler

07/2010 – 10/2010 RailwayStatic and fatigue analysis of a part of a carrying frame for a local train (Customer Alstom)Static and fatigue analysis of a wheel arrangement for a street-rail vehicle (Customer Prode)04/2007-06/2010 AerospaceAs an external supplier, resident in Alenia Aermacchi:- Static and fatigue analysis of the Engine Nacelle for the Airbus A380 program.- Alenia Aermacchi M346 Program:Comparision of strain gauge data obtained for selected flights with Magali acquisition data software with data obtained from global FEM loaded with the same load conditions.Global F.E.M. management in order to introduce structure redesign and materials update.Preliminary analysis in case of a fire event in a engine bay in order to check the structure integrity and landing capability.Static analysis and certification reports for several parts: front fuselage radar installation, noose doors, windshield and canopy structure, metallic rear lower skin, rear upper longerons.11/2005-04/2007 AerospaceStatic and fatigue analysis of the Engine Nacelle for the Airbus A380 program02/2005 – 10/2005 Railway and mechanicsDemo and test case preparation with Adina software.Static and fatigue analysis for several railway customers.

Static and crash analysis. Development of numerical model of road safety barriers and improvement of numerical model of vehicles using the multibody software Madyac. Road safety barrier omologation reports as request in the European Norm EN1317-1 e EN1317-2

Collaboration with the Aerospace department for different activities:- Development of F.E. Geo Metro model in the within of a project carried on with the cooperation of several Universities and Safety Research Centres.- Side impact using an optimised model of a Hybrid III dummy. The injuries caused by the impact against the lateral window were considered – referring to the Head Injury Criterion (HIC)- Realisation and optimisation of the model of a helicopter seat and related seat-belts. The effects of a prescribed deceleration on the occupant were investigated using a optimised model of a Hybrid III dummy.FEM code LsDyna960, Patran, Ls-Pre-Post