Development of the new empennage FE model.
Sizings, Static structural justification of the empennages and boom.
Thermal analysis (Avionics), Static structural analysis of the UAS body, load application, FEA , Certification Reports
Seminario: FATIGUE AND DAMAGE TOLERANCE - Practical Computational Aspects
About 8 months ago from AirWorks's Twitter via Twitter Web Client
@AIRWORKS_Srl , è Capofila del progetto ABE (Abbattimento delle emissioni vibroacustiche e chimiche in ambito naval… twitter.com/i/web/status/1…
Please give a look to Airwork proprietary software StructCode performing Fatigue and Damage Tolerance FEM based anal…lnkd.in/eEyN8uc
About 4 years ago from AirWorks's Twitter via LinkedIn
Succesfully passed Static Test on the Clamp Band Tool for the OPTSAT-3000 program.
About 4 years ago from AirWorks's Twitter via Twitter Web Client
Successfully passed the CDR with the Clamp Band Tool and Dummy Satellite for the OPTSAT-3000 program.