guidance on fuselage design & analysis using ANSYS + PyAnsy
Hi everyone,
I’m currently working on a project where I need to design and analyze an aircraft fuselage section using ANSYS, and I’d like to integrate Python (PyAnsys) into the workflow.
I’m still a beginner with PyAnsys, so I’m looking for guidance on how to get started properly — especially:
- Setting up geometry and meshing with scripts
- Running structural analysis using Python
- Best practices or tutorials for aerospace applications
If anyone has experience with this or can share resources, example scripts, or advice, I’d really appreciate it.
Thanks in advance! 🙏