i urgently need help to design boeing 747 riveted fuselage model & another model welded by plasma , also how to make stress analysis for both models

i would like to make two diffrent fueslage modeks for boeing 747 , one of them is riveted and another is welded by plasma through using catia

3 Answers

for stress analysis U can use Ansys Workbench

Hi friend, try to model in catia, something like this link:
https://www.researchgate.net/publication/272590001_Fatigue_crack_location_and_fatigue_life_for_riveted_lap_joints_in_aircraft_fuselage

and after that you can make the analysis using ANSYS Software.