Fea on aircraft fuselage using ansys discovery

I'm looking for someone to complete a FEA on an aircraft fuselage using Ansys Discovery. The specific type of analysis needed is structural analysis. I have some specific requirements and constraints in regards to the analysis, particularly boundary conditions. This project is critical to the success of our project and I am looking for a freelancer with experience in the written specified software and analysis processes. If you feel confident that you can meet this requirement, please let me know and I will provide you with further project details. Thank you for your interest!