High Fidelity aero-structural analysis for CNT and FWT configurations

Document reporting the HF aeroelastic analysis of cantilever wing configuration equipped with folding wingtip mechanismCONTRIBUTORSSIEMENS will perform the HIFI aerostructural analyses of the optimized folding wingtip configurations A special care will be devoted to the mechanical simulation of the folding mechanismUNIVBRIS will share the aeroelastic medium fidelity model of the optimized folding wingtip configurations and will support SIEMENSPOLIMI will support SIEMENS to derive the relevant results supporting the definition of the final aeroservoelastic wind tunnel model to be tested at POLIMI