I'm not familiar with Fusion 360 other than reading Autodesk's description of what it can do. I know it can do stress analysis for example, but how are you determining the flight loads to feed into the stress analysis. Having the software work out stresses once you've entered the loads is one thing, but how are you then deciding what are acceptable stress/deflection limits etc. What about flutter analysis? What sort of performance do you expect the aircraft to have? I'm asking because I'm curious, not because I want to come across as critical. You've spent a lot of time and effort to get the external shape looking great, but I'm just wondering about the engineering design behind it.